Flight Planning [870 q] -

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JAA Test Prep033 - Flight PlanningEdition 2008

033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS1© 2008AVIATIONEXAM.com1129 (A) 1171 (D) 12526 (C) 25049 (B) 25050 (C) 25051 (D) 25070 (B) 25173 (D)28335 (D) 28336 (A) 28337 (A) 28338 (A)033-01-01 Navigation plan1129. (all)How many feet you have to climb to reach FL75? Given:Departure aerodrome elevation: 1.500 ftQNH: 1023 hPaTemperature: ISA1 hPa: 30 ft#A) 6.300 ftB) 6.000 ftC) 6.600 ftD) 7.800 ft1171. (all)VFR flights shall not be flown over the congested areas of

cities at a height less than:A) the heighest obstacle.B) 2.000 ft above the heighest obstacle within a radius of 600ft from the aircraft.C) 500 ft above the heighest obstacle.#D) 1.000 ft above the heighest obstacle within a radius of 600m from the aircraft.12526. (all)(Refer to figures 033-73)The measured course 042° TThe variation in the area is 6° W and the wind is calmThe deviation is 4° WIn order to follow this course, the pilot must fly a compass

heading of:A) 040°B) 044°#C) 052°D) 058°25049. (all)(Refer to Jeppesen Manual chart ED-6)What is the lowest ICAO VFR level for a flight from TRA(N47°42 E008°26) to KPT (N47°45 E010°21) ensuring thatyou are at least at minimum grid area altitude with QNH1013?A) FL070#B) FL095

C) FL075D) FL09025050. (all)On a flight from (47°10N 010°00E) to (49°10N 010°00E) ata TAS of 140 kts with a 20 kts headwind component, howmany nautical air miles do you fly?A) 100B) 120#C) 140D) 70



25051. (all)Given CAS/RAS of 130 kts, OAT 0 °C at 10.000 ft, trip distanceof 240 NGM, track 275° (T) and W/V 030/30 kts. Whatis your true heading and time enroute?A) 287° and 103 minutes.B) 287° and 95 minutes.C) 285° and 95 minutes.#D) 285° and 88 minutes.25070. (all)(Refer to figure 033-06)What is the fuel, time and distance to climb from an aerodromeat sea level up to FL100 where the outside air temperatureis 0 °C?A) 13 USG, 24 min, 45 NM.#B) 9 USG, 16 min, 28 NM.C) 9 USG, 14 min, 27 NM.D) 5 USG, 10 min, 16 NM.25173. (all)Given:True course: 017°W/V: 340°/30TAS: 420 ktsFind:1) the wind correction angle (WCA)

2) the ground speed (G/S)A) (1) +2°; (2) 416 kts.B) (1) +2°; (2) 396 kts.C) (1) -2°; (2) 426 kts.#D) (1) -2°; (2) 396 kts.28335. (AIR: atpl, cpl; HELI: atpl, cpl)The average true course from C (62°N 020°W) to B (58°N004°E) is:A) 120°B) 119°C) 099°#D) 109°28336. (AIR: atpl, cpl; HELI: atpl, cpl)

The initial magnetic course from C (62°N 020°W) to B (58°N004°E) is:#A) 116°B) 080°C) 098°D) 113°28337. (AIR: atpl, cpl; HELI: atpl, cpl)The initial true course from C (62°N 020°W) to B (58°N004°E) is:#A) 098°B) 116°C) 080°D) 278°

28338. (AIR: atpl, cpl; HELI: atpl, cpl)The distance (NM) from A (64°N 006°E) to C (62°N 020°W)is:#A) 720B) 690C) 1590D) 1440

033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS2



© 2008AVIATIONEXAM.com28339 (A) 28340 (C) 28341 (D) 28342 (A) 28343 (D) 1112 (B) 1115 (D) 1121 (B)1135 (A) 1138 (D)28339. (AIR: atpl, cpl; HELI: atpl, cpl)The average magnetic course from A (64°N 006°E) to C(62°N 020°W) is:#A) 271°B) 259°C) 247°D) 279°28340. (AIR: atpl, cpl; HELI: atpl, cpl)The average true course from A (64°N 006°E) to C (62°N020°W) is:A) 271°B) 247°#C) 259°D) 079°28341. (AIR: atpl, cpl; HELI: atpl, cpl)The initial magnetic course from A (64°N 006°E) to C (62°N020°W) is:A) 262°B) 267°C) 271°

#D) 275°28342. (AIR: atpl, cpl; HELI: atpl, cpl)The initial true course from A (64°N 006°E) to C (62°N 020°W)is:#A) 271°B) 275°C) 267°D) 246°28343. (AIR: atpl, cpl; HELI: atpl, cpl)The distance (NM) from C (62°N 020°W ) to B (58°N 004°E)is:A) 775B) 725

C) 700#D) 760033-01-02 Fuel plan1112. (all)(Refer to figure 033-05)For a flight departing from MSL at 3.663 lbs, cruising atFL80 at 2.300 RPM, 20 °C lean of peak EGT, in 40 kts headwind,calculate endurance:A) 4,75 hrs#B) 5,3 hrsC) 6,1 hrsD) 6,55 hrs1115. (all)

Given:Dry operating mass (DOM): 33.510 kgLoad: 7.600 kgFinal reserve fuel: 983 kgAlternate fuel: 1.100 kgContingency fuel: 102 kgThe estimated landing mass at alternate should be:A) 42.312 kgB) 42.093 kgC) 42.210 kg



#D) 42.195 kg1121. (all)A multi engine piston aeroplane is on an IFR flight. The fuelplan gives a trip fuel of 65 US gallons. The alternate fuel,final reserve included, is 17 US gallons. Contingency fuelis 5% of the trip fuel. The usable fuel at departure is 93 USgallons. At a certain moment the fuel consumed accordingto the fuel gauges is 40 US gallons and the distance flownis half of the total distance. Assume that fuel consumptiondoes not change. Which statement is right?A) At the destination there will still be 30 US gallons in thetanks.#B) The remaining fuel is not sufficient to reach the destinationwith reserves intact.C) At departure the reserve fuel was 28 US gallons.D) At destination the required reserves remain intact.1135. (all)(Refer to figure 033-05)Given:Cruising: FL75Mixture: leanFull throttle: 2.300 RPMTakeoff fuel: 444 lbsTakeoff from: MSL

Find endurance in hours:#A) 5 hrs 12 mins.B) 5 hrs 20 mins.C) 4 hrs 42 mins.D) 5 hrs 23 mins.1138. (all)For a planned flight the calculated fuel is as follows:Flight time: 2:42Taxi fuel: 9 kgBlock fuel: 136 kgThe reserve fuel, at any time, should not be less than 30%of the remaining trip fuel.How much fuel should remain after 2 hours flight time?

A) 33 kg trip fuel and no reserve fuel.B) 33 kg trip fuel and 10 kg reserve fuel.C) 23 kg trip fuel and 10 kg reserve fuel.#D) 25 kg trip fuel and 8 kg reserve fuel.

033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS3© 2008AVIATIONEXAM.com1146 (A) 1155 (A) 1159 (A) 1164 (C) 1173 (A) 1275 (B) 1277 (A)1146. (all)(Refer to figure 033-02)A flight has to be made with the SEP1. For the fuel calculation

allow:- 10 lbs fuel for start up and taxi- 3 mins and 1 gallon of additional fuel to allow for theclimb- 10 mins and no fuel correction for the descent- Planned flight time (overhead to overhead) is 3 hrs 12mins- Reserve fuel 30% of the trip fuel- Power setting is 25HG (or full throttle) 2100 RPM, 20 °Clean



- FL70 and OAT is 11 °CThe minimum block fuel is:#A) 283 lbsB) 268 lbsC) 215 kgD) 252 kg1155. (all)During an IFR flight in a Beech Bonanza the fuel indicatorsshow that the remaining amount of fuel is 100 lbs after 38minutes. The total amount of fuel at departure was 160 lbs.For the alternate fuel, 30 lbs is necessary. The planned fuelfor taxi was 13 lbs. Final reserve fuel is estimated at 50 lbs.If the fuel flow remains the same, how many minutes can beflown to the destination with the remaining fuel?#A) 12 minutes.B) 63 minutes.C) 44 minutes.D) 4 minutes.1159. (all)(Refer to figure 033-08)A flight has to be made with a multi engine piston aeroplane.For the fuel calculations take 5 US gallons for thetaxi, and an additional 13 minutes at cruise condition toaccount for climb and descent. Calculated time overhead

to overhead is 2 hrs 37 min.Power setting is 65%, 2.500 RPMCalculated reserve fuel is 30% of the trip fuelFL120, Temperature 1 °CFind the minimum block fuel:#A) 91 US gallons.B) 86 US gallons.C) 76 US gallons.D) 118 US gallons.1164. (all)For a planned flight the calculated fuel is as follows:Flight time: 3:06Taxi fuel: 8 kg

Block fuel: 118 kgThe reserve fuel, at any time, should not be less than 30%of the remaining trip fuelHow much fuel should remain after 2 hours flight time?A) 27 kg trip fuel and 12 kg reserve fuel.B) 39 kg trip fuel and 12 kg reserve fuel.#C) 30 kg trip fuel and 9 kg reserve fuel.D) 39 kg trip fuel and no reserve fuel.1173. (all)(Refer to figure 033-04)Using the following information, calculate the range.Given:Aeroplane mass at start up: 3.663 lbs

Fuel load (density 6lbs/gal): 74 galTakeoff altitude: sea levelHeadwind: 40 ktsCruise altitude: 8.000 ftPower setting: full throttle 2.300 RPM 20 °C lean of peak#A) 633 NMB) 844 NMC) 730 NMD) 547,5 NM1275. (all)



(Refer to figure 033-10)Given the following data:FL75Lean mixtureEconomy Power settingFind the endurance with no reserve:A) 06:12#B) 05:01C) 06:06D) 05:111277. (all)(Refer to figure 033-02)A flight has to be made with the single engine sample aeroplane.For the fuel calculation allow:- 10 lbs fuel for start up and taxi- 3 minutes and 1 gallon of additional fuel to allow for theclimb- 10 minutes and no fuel correction for the descent- Planned flight time (overhead to overhead) is 03 hoursand 12 minutes- Reserve fuel 30% of the trip fuelPower setting is 25 inHg (or full throttle), 2.100 RPM, 20 °CleanFlight level is 70 and the OAT 11 °C

The minimum block fuel is:#A) 283 lbsB) 268 lbsC) 252 lbsD) 215 lbs

033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS4© 2008AVIATIONEXAM.com1284 (D) 1298 (A) 2298 (C) 12241 (A) 24772 (B) 25034 (D) 25055 (A) 25060 (D)25067 (A)1284. (all)

(Refer to figure 033-03)A flight has to be made with the single engine sample aeroplane.For the fuel calculation allow:- 10 lbs fuel for start up and taxi- 3 minutes and 1 gallon of additional fuel to allow for theclimb- 10 minutes and no fuel correction for the descent- Planned flight time (overhead to overhead) is 02 hoursand 37 minutes- Reserve fuel 30% of the trip fuel- Power setting is 23 inHg (or full throttle), 2.300 RPM, 20°C lean- Flight level is 50 and the OAT -5 °C

The minimum block fuel is:A) 250 lbsB) 208 lbsC) 270 lbs#D) 265 lbs1298. (all)(Refer to figure 033-07)A flight is to be made in a multi engine piston aeroplane(MEP1). The cruising level will be 11.000 ft. The outside airtemperature at FL is -15 °C. The usable fuel is 123 US gallons.



The power is set to economic cruise. Find the rangein NM with 45 min reserve fuel at 45% power.#A) 752 NMB) 852 NMC) 610 NMD) 602 NM2298. (all)Using the following data, determine the maximum fuelload:DOM: 2.800 kgTrip: 300 kgPayload: 400 kgMTOM: 4.200 kgMLM: 3.700 kgA) 700 kgB) 1.000 kg#C) 800 kgD) 500 kg12241. (all)(Refer to figure 033-08)A flight has to be made with a multi engine piston aeroplane(MEP 1). For the fuel calculations take 5 US gallonsfor the taxi, and an additional 13 min at cruise condition toaccount for climb and descent. Calculated time from overhead

to overhead is 1 hrs 47 min.Powersetting is 45%, 2.600 RPMCalculated reserve fuel is 30% of the trip fuelFL100, Temperature -5 °CFind the minimum block fuel:#A) 47 US gallonsB) 37 US gallonsC) 60 US gallonsD) 470 US gallons24772. (all)Given:DOM: 33.510 kgTraffic load: 7.600 kg

Trip fuel: 2.040 kgFinal reserve: 983 kgAlternate fuel: 1.100 kgContingency: 5% of trip fuelWhich of the following is correct?A) Landing mass at destination is 43.193 kg.#B) Landing mass at destination is 43.295 kg.C) Takeoff mass is 43.295 kg.D) Takeoff mass is 45.233 kg.25034. (all)(Refer to figure 033-04)At 6.000 ft what is the range of the aircraft at full throttlewith 2.500 RPM set?

A) 840 NAMB) 872 NAMC) 914 NAM#D) 756 NAM25055. (AIR: all)A jet aircraft is due to fly to an isolated aerodrome. Theaircraft fuel burn in the cruise is 7.500 kg/hrs and 5.000 kg/hrs in the hold. What is the absolute minimum additionalfuel it should carry?#A) 15.000 kg



B) 10.000 kgC) 3.750 kgD) 5.625 kg25060. (all)You are required to uplift 40 US Gallons of AVGAS with sp.gravity of 0,72. How many litres and kilograms is this?A) 109 litres, 151 kg.B) 182 litres, 131 kg.C) 182 litres, 289 kg.#D) 151 litres, 109 kg.25067. (all)(Refer to figure 033-03)On a standard day what is the TAS and fuel flow in USG at10.000 ft?#A) 157 kts, 11,0 GPH.B) 137 kts, 66,2 GPH.C) 157 kts, 20,7 GPH.D) 157 kts, 11,4 GPH.

033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS5© 2008AVIATIONEXAM.com25166 (A) 25168 (C) 25186 (B) 1116 (B) 1131 (B) 1132 (B) 1169 (C) 1202 (C)

1301 (B)25166. (all)(Refer to figure 033-03)Given:Lean mixture23,0 inHg (or full throttle) at 2.300 RPMFL75OAT +10 °CFind TAS and fuel flow in gallons per hour:#A) 160 kts, 11,6 GPH.B) 143 kts, 71,1 GPH.C) 160 kts, 68,5 GPH.D) 143 kts, 11,6 GPH.

25168. (all)Given:Dry Operating Mass: 33.000 kgLoad: 8.110 kgFinal reserve fuel: 983 kgAlternate fuel: 1.100 kgContingency: 102 kgThe estimated landing mass at the alternate aerodrome is:A) 42.210 kgB) 42.312 kg#C) 42.195 kgD) 41.110k g25186. (all)

For a planned flight the calculated fuel is as follows:Flight time: 2 hrs 42 minBlock fuel: 136 kgTaxi fuel: 9 kgThe reserve fuel, at any time, should be not less than 30%of trip fuel remaining.How many kg of fuel should remain after 2 hrs of flight?A) 33 kg trip and 10 kg reserve.#B) 25 kg trip and 8 kg reserve.C) 23 kg trip and 10 kg reserve.



D) 33 kg trip and no reserve.033-01-03 Flight monitoring and in-flight replanning1116. (all)After flying for 16 min at 100 kts TAS with a 20 kts tail windcomponent, you have to return to the airfield of departure.You will arrive after:A) 20 min.#B) 24 min.C) 10 min 40 sec.D) 16 min.1131. (all)ATC require a descent from FL270 to FL160 to be level 6NM before a VOR. If rate of descent is 800 feet per minute,mean groundspeed is 256 kts, how far out from the VORmust descent be started?A) 59 NM#B) 65 NMC) 144 NMD) 150 NM1132. (all)In the cruise at FL155 at 260 kts TAS, the pilot plans for a500 ft/min descent in order to fly overhead MAN VOR at2.000 feet (QNH 1.030). TAS will remain constant during descent,wind is negligible, temperature is standard. The pilot

must start the descent at a distance from MAN of:A) 140 NM#B) 120 NMC) 110 NMD) 130 NM1169. (all)A VFR flight in Piper SENECA III. At a fuel check you have60 US gallons (USG) of usable fuel remaining. Alternate fuelrequired is 12 USG. The flight time remaining is 1 hrs 35min. What is the highest consumption rate acceptable?A) 33,0 USG/hrsB) 37,9 USG/hrs#C) 30,3 USG/hrs

D) 21,3 USG/hrs1202. (all)An aircraft flying at 7.500 ft is cleared to descend to be levelat 1.000 ft, 6 NM before reaching a beacon. If ground speedis 156 kts and Rate of Descent is 800 ft/min, how manymiles before the beacon should descent begin?A) 15,0B) 30,2#C) 27,1D) 11,11301. (all)A descent is planned from 7.500 ft MSL so as to arrive at1.000 ft MSL 6 NM from a VORTAC. With a GS of 156 kts

and a rate of descent of 800 ft/min. The distance from theVORTAC when descent is started is:A) 15,0 NM#B) 27,1 NMC) 11,7 NMD) 30,2 NM

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AVIATIONEXAM.com1313 (C) 24740 (D) 24744 (D) 24746 (C) 25053 (A) 25054 (C) 25058 (D) 25104 (A)25105 (D) 1120 (C) 1192 (A)1313. (all)Minimum planned takeoff fuel is 160 kg (30% total reservefuel is included). Assume the groundspeed on this trip isconstant. When the aeroplane has done half the distancethe remaining fuel is 70 kg. Is diversion to a nearby alternatenecessary?A) Diversion to a nearby alternate is not necessary, becauseit is allowed to calculate without reserve fuel.B) Diversion to a nearby alternate is not necessary, becausethe reserve fuel has not been used completely.#C) Diversion to a nearby alternate is necessary, because theremaining fuel is not sufficient.D) Diversion to a nearby alternate is necessary, unless thecaptain decides to continue on his own responsability.24740. (all)An aircraft is in cruising flight at FL095, IAS 155 kts. Thepilot intends to descend at 500 ft/min to arrive overheadthe MAN VOR at 2.000 ft (QNH 1.030 hPa). The TAS remainsconstant in the descent, wind is negligible, temperaturestandard. At which distance from MAN should the pilotcommence the descent?

A) 42 NMB) 40 NMC) 45 NM#D) 48 NM24744. (all)The still air distance in the climb is 189 NAM and time 30min. What ground distance would be covered in a 30 ktsheadwind?A) 193 NMB) 203 NMC) 188 NM#D) 174 NM24746. (all)

An aircraft climbs from an airfield, elevation 1.500 ft, QNH1.023 mb, to FL75. What height does the aircraft have toclimb? (Assume 1 mb = 30 ft)A) 6.600 ftB) 7.800 ft#C) 6.300 ftD) 6.000 ft25053. (all)An aircraft is flying at an indicated pressure altitude of5.000 ft where the OAT is -10 °C. What is the aircrafts truealtitude?#A) 4.750 ftB) 5.260 ft

C) 5.120 ftD) 4.600 ft25054. (all)A mountain 6.011 ft AMSL lies along an aircrafts track of356° (T), variation 10°W, HDG 355° (M). What is the lowestVFR ICAO level the aircraft may fly to miss the mountain byat least 2.000 ft, QNH 990 hPa (assume 1 hPa = 30 ft)?A) FL075B) FL090#C) FL095



D) FL08525058. (all)An aircraft takes 14 minutes to climb to FL290 covering71 NAM, what is the ground distanced covered in a 30 ktsheadwind?A) 71 NGMB) 57 NGMC) 78 NGM#D) 64 NGM25104. (all)Given:Variation 15°EDeviation 6°WHeading 080° (T)Determine aircrafts compass and magnetic headings:#A) 071, 065B) 065, 071C) 086, 095D) 095, 08625105. (all)Given:Variation 12°WDeviation 3°EHeading 180° (T)

Determine aircrafts compass and magnetic headings:A) 168, 171B) 168, 165C) 192, 189#D) 189, 192033-01-04 Radio communication and navigation aids1120. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-01)What navigation or communications facilities are at 48°55N009°20E?A) NDBB) TACAN#C) VOR/DME

D) VOR1192. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-02)Give the frequency of ZURICH Volmet.#A) 127,2 MHzB) 127,2 kHzC) 128,525 MHzD) 118,1 MHz

033-01 FLIGHT PLANS FOR CROSS-COUNTRY FLIGHTS7© 2008AVIATIONEXAM.com

1205 (A) 12239 (C) 12242 (D) 12243 (D) 12244 (C) 12245 (B)1205. (all)(Refer to Jeppesen Manual ED-6 or figures ED6-04 andED6-06)Give the frequency of the GRENCHEN VOR at 47°11N007°25E.#A) 108,65 MHz.B) 326 kHz.C) channel 23.D) 120,1 MHz.



12239. (all)During a flight at night a position has to be reported toATC. The aeroplane is at a distance of 750 NM from thegroundstation and at flight level 350. The frequency to beused is:A) 17.286 kHzB) 123,9 MHz#C) 5.649 kHzD) 1.136 kHz12242. (all)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-26)The radio navigation aid serving STRASBOURG (48°30N007°34E) is a:A) VOR only, frequency 115,6 MHz.B) DME only, channel 115,6.C) TACAN only, frequency 115,6 MHz.#D) VOR/TACAN, frequency 115,6 MHz.12243. (all)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-27)The radio navigation aid at ST DIZIER (48°38N 004°53E)is a:A) VOR, frequency 114,0 MHz, and TACAN channel 87.

B) TACAN, channel 114,0 MHz.C) TACAN, channel 87, and NDB frequency 114,0 kHz.#D) TACAN, channel 87, frequency 114,0 MHz.12244. (all)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-28)The radio navigation aid on airway UG4 at LUXEUIL (47°41N006°18E) is a:A) VOR/DME and NDB, identifier LXI.B) VOR/DME only, identifier LUL.#C) VOR only, identifier LUL.D) VOR, identifier LUL, frequency paired with TACAN identi-fier LXI.

12245. (all)(Refer to Route Manual chart E (LO)1 or figure LO-12)The radio navigation aid at BELFAST CITY (54°37N 005°53W)is:A) an NDB, frequency 420 kHz, continuous operation.#B) an NDB, frequency 420 kHz, NOT continuous operation.C) a TACAN, channel 420.D) a fan marker, frequency 420 kHz.

033-02 ICAO ATC FLIGHT PLAN8© 2008AVIATIONEXAM.com

1234 (B) 1237 (D) 1245 (C) 1250 (B) 25030 (C) 1211 (D) 1212 (D) 1213 (D)1216 (A) 1217 (B)033-02-01 Types of flight plan1234. (all)From the options given below select those flights whichrequire flight plan notification:1) Any Public Transport flight.2) Any IFR flight.3) Any flight which is to be carried out in regions which aredesignated to ease the provision of the Alerting Service or



the operations of Search and Rescue.4) Any cross-border flights.5) Any flight which involves overflying water.A) 1, 5#B) 2, 4C) 1, 2, 3D) 3, 4, 51237. (all)A current flight plan is a:A) flight plan in the course of which radio communicationshould be practised between aeroplane and ATC.B) filed flight plan.C) flight plan with the correct time of departure.#D) filed flight plan with amendments and clearance included.1245. (all)For which flights are Flight Plans required?1) IFR flights.2) IFR and VFR flights.3) Flights crossing national boundaries.4) Flights over water.5) Public transport flights.A) 2, 3, 4B) 1, 3, 5#C) 1, 3

D) 2, 3, 4, 51250. (all)For a repetitive flight plan (RPL) to be used, flights musttake place on a regular basis on at least:A) 20 occasions.#B) 10 occasions.C) 30 occasions.D) 50 occasions.25030. (all)Repetitive flight plans may be used for ___ flights with ahigh degree of stability over the same days of consecutiveweeks on at least ___ occasions.A) IFR; 7

B) VFR; 10#C) IFR; 10D) VFR; 7033-02-02 Completing the flight plan1211. (all)When completing an ATS flight plan for a European destination,clock times are to be expressed in:A) central European time.B) local mean time.C) local standard time.#D) UTC.1212. (all)In an ATS flight plan an aircraft will be classified as (L) if its

MTOM is:A) 27.000 kgB) 10.000 kgC) 57.000 kg#D) 7.000 kg1213. (all)(Refer to figure 033-61)In the ATS flight plan Item 15, a cruising speed of 470 ktswill be entered as:A) N470



B) KN470C) 0470K#D) N04701216. (all)In the ATS flight plan item 15, when entering a route forwhich standard departure (SID) and standard arrival (STAR)procedures exist:#A) both should be entered in the ATS plan where appropriate.B) SIDs should be entered but not STARs.C) STARS should be entered but not SIDs.D) neither SID nor STAR should be entered.1217. (all)When submitting a flight plan before flight, departure timeis?A) Overhead the first reporting point.#B) At which the aircraft leaves the parking area.C) Of takeoff.D) At which flight plan is filed.

033-02 ICAO ATC FLIGHT PLAN9© 2008AVIATIONEXAM.com1221 (D) 1222 (C) 1224 (C) 1226 (B) 1228 (D) 1229 (B) 1230 (A) 1232 (B)

1233 (C) 1235 (B) 1236 (A) 1239 (A) 1240 (D)1221. (all)An aircraft has a maximum certificated takeoff mass of137.000 kg but is operating at takeoff mass 135.000 kg. InItem 9 of the ATS flight plan its wake turbulence categoryis:A) medium plus (M+).B) heavy/medium (H/M).C) medium (M).#D) heavy (H).1222. (all)The navigation plan reads:Trip fuel: 136 kg

Flight time: 2 hrs 45 minCalculated reserve fuel: 30% of trip fuelFuel in tank is minimum (no extra fuel on board)Taxi fuel: 3 kgThe endurance on the ICAO flight plan should read:A) 2 hrs 49 minB) 2 hrs 45 min#C) 3 hrs 34 minD) 3 hrs 38 min1224. (all)In the appropriate box of a flight plan form, correspondingto the estimated time of departure, the time indicated is thatat which the aircraft intends to:

A) start-up.B) takeoff.#C) go off blocks.D) pass the departure beacon.1226. (all)(Refer to figure 033-61)In an ATS flight plan, item 15 (route), a cruising pressurealtitude of 32.000 feet would be entered as:A) FL320#B) F320



C) S3200D) 320001228. (all)An aeroplane is flying from an airport to another. In cruise,the calibrated airspeed is 150 kts, true airspeed 180 kts,average ground speed 210 kts, the speed box on the filedflight plan shall be filled as follows:A) K0150B) K0210C) K0180#D) N01801229. (all)When completing an ATS flight plan, an elapsed time (item16) of 1 hrs 55 min should be entered as:A) 0115#B) 0155C) 115MD) 1H551230. (all)In the ATS flight plan item 13, in a flight plan submitted beforedeparture, the departure time entered is the:#A) estimated off-block time.B) estimated time over the first point enroute.C) estimated takeoff time.

D) allocated slot time.1232. (all)For the purposes of item 9 (wake turbulence category) ofthe ATS flight plan, an aircraft with a maximum certificatedtakeoff mass of 62.000 kg is:A) light (L).#B) medium (M).C) heavy (H).D) unclassified (U).1233. (all)An aircraft plans to depart London at 1000 UTC and arriveat Munich (EDDM) at 1215 UTC. In the ATS flight plan item16 (destination / EET) should be entered with:

A) EDDM 1215.B) EDDM 1415.#C) EDDM 0215.D) EDDM 2H15.1235. (all)In the ATS flight plan item 19, if the number of passengersto be carried is not known when the plan is ready for filing:A) the plan should be filed with the relevant box blank.#B) TBN (to be notified) may be entered in the relevant box.C) an estimate may be entered but that number may not subsequentlybe exceeded.D) the plan may not be filed until the information is available.1236. (all)

In the ATS flight plan, for a non-scheduled flight which ofthe following letters should be entered in item 8 (type offlight):#A) NB) N/SC) GD) X1239. (all)In the appropriate box of a flight plan, for endurance, onemust indicate the time corresponding to:



#A) the total usable fuel on board.B) the required fuel for the flight.C) the required fuel for the flight plus the alternate and 45minutes.D) the total usable fuel on board minus reserve fuel.1240. (all)When completing an ATS flight plan for a flight commencingunder IFR but possibly changing to VFR, the letters enteredin item 8 (flight rules) would be:A) XB) N/SC) G#D) Y

033-02 ICAO ATC FLIGHT PLAN10© 2008AVIATIONEXAM.com1243 (C) 1244 (D) 1246 (B) 1249 (B) 1251 (A) 1253 (B) 1257 (C) 1259 (B)1261 (B) 1262 (D) 1264 (C) 1265 (C) 1347 (C)1243. (all)The cruising speed to write in the appropriate box of a flightplan is:A) ground speed.

B) indicated air speed.#C) true air speed.D) calibrated air speed.1244. (all)On a flight plan you are required to indicate in the boxmarked SPEED the planned speed for the first part of thecruise or for the entire cruise. This speed is:A) the estimated ground speed.B) the equivalent airspeed.C) the indicated airspeed.#D) the true airspeed.1246. (all)In the ATS flight plan Item 15 (cruising speed), when not

expressed as a Mach number, cruising speed is expressedas:A) IAS#B) TASC) CASD) ground speed1249. (all)The navigation plan reads:Trip fuel: 100 kgFlight time: 1 hrs 35 minTaxi fuel: 3 kgBlock fuel: 181 kgThe endurance on the ICAO flight plan should read:

A) 1 hrs 35 min#B) 2 hrs 49 minC) 2 hrs 04 minD) 2 hrs 52 min1251. (all)The maximum permissible takeoff mass of an aircraft forthe L wake turbulence category on a flight plan is:#A) 7.000 kgB) 2.700 kgC) 5.700 kg



D) 10.000 kg1253. (all)In the ATS flight plan item 10 (equipment), the letter to indicatethe carriage of a serviceable transponder - mode A (4digits-4096 codes) and mode C, is:A) B#B) CC) AD) P1257. (all)In an ATS flight plan item 15, in order to define a positionas a bearing and distance from a VOR, the group of figuresshould consist of:A) VOR ident, magnetic bearing and distance in kilometres.B) VOR ident, true bearing and distance in kilometres.#C) VOR ident, magnetic bearing and distance in nauticalmiles.D) full name of VOR, true bearing and distance in kilometres.1259. (all)When filling in a flight plan, wake turbulence category is afunction of?A) Maximum certified landing mass.#B) Maximum certified takeoff mass.C) Estimated landing mass.

D) Estimated takeoff mass.1261. (all)When an ATS flight plan is submitted for a flight outsidedesignated ATS routes, points included in item 15 (route)should not normally be at intervals of more than:A) 20 minutes flying time or 150 km.#B) 30 minutes flying time or 370 km.C) 15 minutes flying time or 100 km.D) 1 hour flying time or 500 km.1262. (all)When a pilot fills in a flight plan, he must indicate the waketurbulence category. This category is a function of whichmass?

A) Actual takeoff mass.B) Estimated takeoff mass.C) Maximum certified landing mass.#D) Maximum certified takeoff mass.1264. (all)In the appropriate box of a flight plan form, concerningequipment, the letter to be used to indicate that the aircraftis equipped with a mode A 4096 codes transponder withaltitude reporting capability is:A) SB) P#C) CD) A

1265. (all)(Refer to figure 033-61)In an ATS flight plan item 15 (route), in terms of latitude andlongitude, a significant point at 41°35N 4°15E should beentered as:A) N04135E0415B) 41°35 N 04° 15E#C) 4135N00415ED) N4135 E004151347. (all)



An aircraft in the cruise has a calibrated airspeed of 150kts, a true airspeed of 180 kts and an average ground speedof 210 kts. The speed box of the flight plan must be filledas follows:A) K0210B) N0150#C) N0180D) K0180

033-02 ICAO ATC FLIGHT PLAN11© 2008AVIATIONEXAM.com4306 (A) 4314 (A) 4315 (B) 4316 (B) 4326 (C) 4328 (A) 4332 (B) 4337 (C)4339 (D) 4343 (A) 4346 (A) 4360 (A)4306. (all)On an ATC flight plan, an aircraft indicated as H forHEAVY:#A) is of the highest wake turbulence category.B) has a certified landing mass greater than or equal to136.000 kg.C) has a certified takeoff mass greater than or equal to140.000 kg.D) requires a runway length of at least 2.000 m at maximum

certified takeoff mass.4314. (all)On a VFR flight plan, the total estimated time is:#A) the estimated time from takeoff to overhead the destinationairport.B) the estimated time from takeoff to overhead the destinationairport, plus 15 minutes.C) the estimated time from takeoff to landing at the alternateairport.D) the estimated time from engine start to landing at the destinationairport.4315. (all)Total elapsed time for an IFR flight, when filling in the ICAO

flight plan at box 16, is the time elapsed from:A) takeoff until landing.#B) takeoff until reaching the IAF (Initial Approach Fix) of thedestination aerodrome.C) taxi-out prior to takeoff until taxiing after landing.D) taxiing until the IAF (Initial Approach Fix) of the destinationaerodrome.4316. (all)Given the following flight plan information:Trip fuel: 136 kgFlight time: 2,75 hrsReserve fuel: 30% of tripFuel in tanks: minimum

Taxi fuel: 3 kgState how endurance should be completed on the ICAOflight plan:A) 0338#B) 0334C) 0245D) 02494326. (all)The navigation plan reads:Trip fuel: 100 kg





landing.

033-02 ICAO ATC FLIGHT PLAN12© 2008AVIATIONEXAM.com4361 (B) 4364 (D) 4366 (C) 4368 (C) 4369 (B) 12524 (B) 12529 (A) 12530 (A)12531 (C) 12532 (B) 14186 (A) 22882 (A) 24765 (A)4361. (all)On an ATC flight plan, to indicate that you will overfly thewaypoint TANGO at 350 kts at flight level 280, you write:A) TANGO / K0350 FL280#B) TANGO / N0350 F280C) TANGO / FL280 N0350D) TANGO / KT350 F2804364. (all)If the destination airport has no ICAO indicator, in box 16 ofyour ATS flight plan, you write:A) ////B) AAAAC) XXXX#D) ZZZZ4366. (all)(Refer to figure 033-61)

Item 7 of the flight plan in accordance with PANS-RAC(DOC 4444) should always include, for an aircraft equippedwith a radio:A) aircraft initialisation.B) aircraft type.#C) aircraft callsign.D) aircraft operator.4368. (all)Reference the ICAO flight plan, in item 15 (speed) thisspeed refers to:A) indicated airspeed.B) equivalent airspeed.#C) initial cruising true airspeed.

D) calculated ground speed.4369. (all)(Refer to figure 033-61)When filling in item 9 of the flight plan and there is no aircraftdesignator listed, what should the entry be?A) None.#B) ZZZZ followed by an entry at item 18.C) XXXX followed by an entry at item 18.D) A descriptive abbreviation of the aircraft type.12524. (all)(Refer to figure 033-61)Prior to an IFR fligt, when filling in the ICAO flight plan, thetime information which should be entered in box 13 (time)

is:A) the time of flight plan filing.#B) estimated off-block time.C) planned takeoff time.D) planned engine start time.12529. (all)(Refer to figure 033-61)In the ATS flight plan item 10 (standard equipment) is consideredto be:#A) VHF RTF, ADF, VOR and ILS.



B) VHF RTF, ADF, VOR and transponder.C) VHF RTF, VOR and transponder.D) VHF RTF, VOR, ILS and transponder.12530. (all)(Refer to figure 033-61)In the ATS flight plan Item 15, for a flight along a designatedroute, where the departure aerodrome is not on orconnected, to that route:#A) the letters DCT should be entered, followed by the pointof joining the ATS route.B) it is necessary only to give the first reporting point on thatroute.C) the words AS CLEARED should be entered.D) it is not necessary to indicate the point of joining that routeas it will be obvious to the ATS unit.12531. (all)(Refer to figure 033-61)In the ATS flight plan item 19, emergency and survivalequipment carried on the flight should be indicated by:A) placing a tick in the relevant box.B) listing the items carried on the REMARKS line.#C) crossing out the box relevant to any equipment not carried.D) circling the relevant box.12532. (all)

(Refer to figure 033-61)Item 9 of the ATS flight plan includes NUMBER AND TYPEOF AIRCRAFT. In this case, the NUMBER means:A) the ICAO type designator number as set out in ICAO Doc8643.#B) the number of aircraft flying in a group.C) the registration number of the aircraft.D) the number of aircraft which will separately be using a repetitiveflight plan (RPL).14186. (all)An aircraft has:Maximum Certificated Takeoff Mass: 137.000 kgActual Takeoff Mass: 135.000 kg

Which wake turbulence category should be entered initem 9?#A) Heavy (H).B) Medium (M).C) Medium/Heavy (M/H).D) Heavy/Medium (H/M).22882. (all)For a flight plan filed before the flight, the indicated time ofdeparture is:#A) the estimated off-block time.B) the time at which the flight plan is filed.C) the time of takeoff.D) the time overhead the first reporting point after takeoff.

24765. (all)What is the maximum estimated elapsed time or distancebetween points on track mentioned in Item15 of the flightplan, for flights outside designated ATS routes?#A) 30 min / 200 NM.B) 60 min / 370 NM.C) 90 min / 370 km.D) 120 min / 370 NM.

033-02 ICAO ATC FLIGHT PLAN



13© 2008AVIATIONEXAM.com24766 (B) 25044 (C) 25045 (B) 25175 (B) 28346 (D) 1209 (C) 1231 (D) 1256 (B)1263 (D) 1267 (D) 24902 (D)24766. (all)Given:Trip fuel: 100 kgPlanned flight time: 1 hrs 30 minTaxi fuel: 3 kgBlock fuel: 181 kgHow should endurance be shown on the flight plan?A) 0204#B) 0240C) 0249D) 025225044. (all)Your aircraft has a maximum certified takeoff mass of140.000 kg. Today your calculated takeoff mass is 130.000kg. What letter should appear in the wake turbulence categoryon the flight plan form?A) Leave blankB) L#C) H

D) M25045. (all)Your initial cruising speed and level are 300 kts and flightlevel 250 at position STP on airway B3 you plan to climb toflight level 330 and increase speed to 350 kts. How shouldthis change be shown in box 15 on the flight plan form?A) N0300 F250 from STP N0350 F330 B3.#B) STP/N0350F330 B3.C) STP/N0330F350 B3.D) STP/N0350F33025175. (all)The cruising speed in item 15 of an ATS flight plan is:A) Indicated Air Speed.

#B) True Air Speed.C) Ground Speed.D) Calibrated Air Speed.28346. (AIR: atpl)Your aircraft is approved for MNPS and RVSM. What do youhave to insert in item 10 of the ATC flight plan?A) WB) YC) X#D) W, X033-02-03 Filing the flight plan1209. (all)It is possible, in flight, to:

1) File an IFR flight plan2) Modify an active IFR or VFR flight plan3) Cancel an active VFR flight plan4) Close an active VFR flight planWhich of the following combinations contains all of thecorrect statements?A) 1, 2, 4B) 1, 2, 3#C) 1, 2, 3, 4D) 2, 3, 4



1231. (all)Which of the following statements regarding filing a flightplan is correct?A) A flying college can file repetitive flight plan for VFRflights.B) Any flight plan should be filed at least 10 minutes beforedeparture.C) A flight plan should be filed when a national FIR boundarywill be crossed.#D) In case of ATFM (Air Traffic Flow Management) the flightplan should be filed at least three hours in advance of theEOBT.1256. (all)How many hours in advance of departure time should aflight plan be filed in the case of flights into areas subjectto air traffic flow management (ATFM)?A) 1:00 hour.#B) 3:00 hours.C) 0:30 hours.D) 0:10 hours.1263. (all)The planned departure time from the parking area is 1815UTC. The estimated takeoff time is 1825 UTC. The IFR flightplan must be filed with ATC at the latest at:

A) 1755 UTCB) 1725 UTCC) 1745 UTC#D) 1715 UTC1267. (all)A repetitive flight plan (RPL) is filed for a scheduled flight:Paris Orly to Angouleme, Paris Orly as alternate. Followingheavy snow falls, Angouleme airport will be closed at theexpected time of arrival. The airline decides before departureto plan a re-routing of that flight to Limoges.A) The pilot-in-command must advise ATC of his intention todivert to Limoges at least 15 minutes before the plannedtime of arrival.

B) The airlines Operations Department has to tansmit achange in the RPL at the ATC office, at least half an hourbefore the planned time of departure.C) It is not possible to plan another destination and the fIighthas to be simply cancelled that day (scheduled flight andnot chartered).#D) The RPL must be cancelled for that day and a specificflight plan has to be filed.24902. (AIR: all)For an intercontinental flight routed via the North Atlanticsystem, how long before start up is requested should yourflight plan have been filed?A) 30 min

B) 6 hrsC) 60 min#D) 3 hrs

033-02 ICAO ATC FLIGHT PLAN14© 2008AVIATIONEXAM.com25056 (B) 1219 (C) 1238 (B) 1254 (A) 1210 (C) 1214 (D) 1248 (B) 1255 (C)1258 (C) 1260 (B)



25056. (all)An aircraft has a flight time of 2 hrs 30 min, a contingencyfuel of 30% is carried. What is the total endurance?A) 1 hr 55 min#B) 3 hrs 15 minC) 3 hrsD) 2 hrs 30 min1254. (all)An aeroplane is on an IFR flight. The flight is to be changedfrom IFR to VFR. Is it possible?A) Yes, the pilot in command must inform ATC using thephrase cancelling my IFR flight.B) No, you have to remain IFR in accordance to the filed flightplan.#C) No, only ATC can order you to do this.D) Yes, but only with permission from ATC.033-02-04 Closing the flight plan1219. (all)You make a diversion from the route given in the flight planand land at an uncontrolled airfield. Within what time afterlanding should you inform ATC?A) 10 min#B) 20 minC) 30 min

D) 45 min1238. (all)If a pilot lands at an aerodrome other than the destinationaerodrome specified in the flight plan, he must ensure thatthe ATS unit at the destination aerodrome is informed withina certain number of minutes of his planned ETA at destination.This number of minutes is:#A) 10B) 30C) 15D) 45033-02-05 Adherence to flight plan1210. (all)

During an IFR flight TAS and time appear to deviate fromthe data in the flight plan. The minimum deviations, thatshould be reported to ATC in order to conform to PANSRAC,are:A) TAS 5 kts and time 5 minutes.B) TAS 3% and time 3 minutes.#C) TAS 5% and time 3 minutes.D) TAS 10 kts and time 2 minutes.1214. (all)When an ATS flight plan has been submitted for a controlledflight, the flight plan should be amended or cancelled in theevent of the off-block time being delayed by:A) 90 minutes or more.

B) 45 minutes or more.C) 60 minutes or more.#D) 30 minutes or more.1248. (all)If a pilot lands at an aerodrome other than the destinationaerodrome specified in the ICAO flight plan, he must ensurethat the ATS unit at the destination is informed withina specified time of his planned ETA at destination. The timeis:A) 45 min



#B) 30 minC) 15 minD) 10 min1255. (all)In the ATS flight plan item 15, it is necessary to enter anypoint at which a change of cruising speed takes place. Forthis purpose a CHANGE OF SPEED is defined as:A) 20 km/h or Mach 0,1 or more.B) 10% TAS or Mach 0,05 or more.#C) 5% TAS or Mach 0,01 or more.D) 20 kts or Mach 0,05 or more.1258. (all)You have filed a flight plan for an uncontrolled flight andsuffer a delay prior to departure. After how long a delaymust you restate your OBT?A) 30 minB) 40 min#C) 60 minD) 90 min1260. (all)In flight, it is possible to:1) File an IFR flight plan.2) Modify an active flight plan.3) Cancel aVFR flight plan.

4) Close a VFR flight plan.A) 1, 3#B) 1, 2, 3, 4C) 2, 3, 4D) 1, 4

033-02 ICAO ATC FLIGHT PLAN15© 2008AVIATIONEXAM.com1266 (A) 24764 (C)1266. (all)You have a flight plan IFR from Amsterdam to London.

In the flight plan it is noted that you will deviate from theATS route passing the FIR boundary Amsterdam/London.The airway clearance reads Cleared to London via flightplanned route. Which of the following statements is correct?#A) The route according to the flight plan is accepted.B) The filed deviation is not accepted.C) You will get a separate clearance for the deviation.D) It is not allowed to file such a flight plan.24764. (all)If your speed, in flight, changes from that given in the flightplan, you should notify ATC for changes of more than:A) 5% TAS / ETA 5 min.B) 3% TAS / ETA 3 min.

#C) 5% TAS / ETA 3 min.D) 3% TAS / ETA 5 min.

033-03 PRACTICAL FLIGHT PLANNING16© 2008AVIATIONEXAM.com1167 (C) 1181 (D) 1185 (B) 1191 (D) 1252 (B) 1276 (C) 1286 (B) 4340 (D)12270 (C) 12271 (A) 12272 (D) 23750 (A)033-03-01 Chart preparation



1167. (all)(Refer to Jeppesen Manual ED-6 or fugure ED6-03)Flying VFR from VILLINGEN (48°03,5N, 008°27,0E) toFREUDENSTADT (48°28,0N, 008°24,0E), determine thedistance:A) 54 NMB) 29 km#C) 24 NMD) 33 NM1181. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-04)The GRENCHEN LSZG aerodrome (47°11N 007°25E) has atower frequency of 120,10 MHz. The (V) after the frequencyindicates:A) available on request.B) only to be used during daylight.C) available for VFR flight only.#D) VDF available.1185. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-05)What navigation or communications facilities are at 48°23N008°39E?A) NDB#B) VOR

C) VOR/DMED) VORTAC1191. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-07)An aeroplane is flying VFR and approaching position TANGO(48°37N 009°16E) at FL55 and on a magnetic track of090. The distance from TANGO is 20 NM. The navigation aidand frequency at TANGO is:A) VORTAC 112,50 kHz.B) DME 112,50 MHz.C) VOR 112,50 with no DME.#D) VORTAC 112,50 MHz.1252. (all)

(Refer to Jeppesen Manual ED-6 or figure ED6-08)Flying VFR from PEITING (47°48N 010°55,5E) to IMMENSTADT(47°33,5N 010°13,0E) determine the magneticcourse.A) 077#B) 243C) 257D) 0631276. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-09)Flying from position ERBACH (48°21N 009°55E) to POLTRINGENairport (48°33N 008°57E). Find the magneticcourse and distance.

A) 108° / 60 NM.B) 252° / 41 NM.#C) 287° / 41 NM.D) 287° / 60 NM.1286. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-10)Flying from position SIGMARINGEN (48°05N 009°13E) toBIBERACH airport (48°07N 009°46E). Find the magneticcourse and distance.A) 093° / 41 NM.



#B) 086° / 22 NM.C) 267° / 22 NM.D) 086° / 32 NM.4340. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-03)Flying VFR from VILLINGEN (48°03,5N 008°27,0E) toFREUDENSTADT (48°28,0N 008°24,0E), determine themagnetic course:A) 176°B) 004°C) 185°#D) 356°12270. (all)(Refer to Route Manual VFR+GPS chart ED-6 or figureED6-03)Flying VFR from VILLINGEN (48°03,5N 008°27,0E) toFREUDENSTADT (48°28,0N 008°24,0E). Determine theminimum altitude within a corridor 5 NM left and 5 NM rightof the courseline in order to stay 1.000 ft clear of obstacles.A) 4.200 ftB) 1.500 ft#C) 3.900 ftD) 2.900 ft12271. (all)

(Refer to Route Manual VFR+GPS chart ED-6 or figureED6-08)Flying VFR from PEITING (47°48,0N 010°55,5E) to IMMENSTADT(47°33,5N 010°13,0E). Determine the distance.#A) 32 NMB) 46 NMC) 58 NMD) 36 NM12272. (all)(Refer to Route Manual VFR+GPS chart ED-6 or figureED6-08)Flying VFR from PEITING (47°48,0N 010°55,5E) to IMMENSTADT(47°33,5N 010°13,0E). Determine the minimum altitude

within a corridor 5 NM left and 5 NM right of the courselinein order to stay 1.000 ft clear of obstacles.A) 5.500 ftB) 6.600 ftC) 5.300 ft#D) 6.900 ft23750. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon)Approach chart (29-1) or figure VFR-10)What is the variation shown on the chart?#A) 3°EB) 3°WC) 5°E

D) 5°W

033-03 PRACTICAL FLIGHT PLANNING17© 2008AVIATIONEXAM.com23751 (B) 23753 (B) 23754 (A) 23755 (C) 23756 (D) 23757 (C) 23758 (C) 23759 (C)23760 (A) 23761 (A) 23762 (D)23751. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM (VFR), Aberdeen



(Dyce) Area chart (10-1V) or figure VFR-1)What is the elevation of the highest ground within theboundary of Aberdeen Control Zone?A) 1.245 ft#B) 1.733 ftC) 2.105 ftD) 2.025 ft23753. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)What is elevation of LSZH ZURICH KLOTHEN airport(47°28N, 008°33E)?A) 1.000 m#B) 1.416 ftC) 1.421 ftD) 1.572 ft23754. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Flying from EDPJ LAICHINGEN airport (48°30N 009°38E)to EDSZ ROTTWEIL ZEPFENHAN (48°12N 008°44E). Findmagnetic course and the distance.#A) Magnetic course 243°, distance 41 NM.B) Magnetic course 063°, distance 41 NM.

C) Magnetic course 063°, distance 62 NM.D) Magnetic course 243°, distance 62 NM.23755. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Flying from EDPJ LAICHINGEN airport (48°30N 009°38E)to EDTM MELGEN airport (48°03N 009°22E). Find magneticcourse and the distance.A) Magnetic course 022°, distance 44 NM.B) Magnetic course 022°, distance 28 NM.#C) Magnetic course 202°, distance 28 NM.D) Magnetic course 202°, distance 44 NM.23756. (all)

(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Flying from EDSZ ROTTWEIL ZEPFENHAN (48°12N008°44E) to EDPJ LAICHINGEN airport (48°30N 009°38E).Determine the highest obstacle within a corridor 5NM leftand right from track.A) 2.852 ftB) 3.612 ftC) 3.278 ft#D) 3.760 ft23757. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)

Flying from EDSZ ROTTWEIL ZEPFENHAN (48°12N008°44E) to EDPJ LAICHINGEN airport (48°30N 009°38E).Find magnetic course and the distance.A) Magnetic course 063°, distance 62 NM.B) Magnetic course 243°, distance 41 NM.#C) Magnetic course 063°, distance 41 NM.D) Magnetic course 243°, distance 62 NM.23758. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)



Flying from EDSZ ROTTWEIL ZEPFENHAN (48°12N008°44E) to EDTM MENGEN airport (48°03N 009°22E). Determinethe highest obstacle within a corridor 5NM left and5 NM right of track.A) 2.920 ftB) 3.331 ft#C) 3.760 ftD) 2.605 ft23759. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Flying from EDSZ ROTTWEIL ZEPFENHAN (48°12N008°44E) to EDTM MENGEN airport (48°03N 009°22E).Find magnetic course and the distance.A) Magnetic course 108°, distance 40 NM.B) Magnetic course 288°, distance 27 NM.#C) Magnetic course 108°, distance 27 NM.D) Magnetic course 288°, distance 40 NM.23760. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Flying from EDTM MELGEN airport (48°03N 009°22E) toEDSZ ROTTWEIL ZEPFENHAN (48°12N 008°44E). Findmagnetic course and the distance.

#A) Magnetic course 288°, distance 27 NM.B) Magnetic course 108°, distance 27 NM.C) Magnetic course 108°, distance 40 NM.D) Magnetic course 288°, distance 40 NM.23761. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Flying from EDTM MENGEN airport (48°03N 009°22E) toEDPJ LAICHINGEN airport (48°30N 009°38E). Determinethe highest obstacle within a corridor 5NM left and 5 NMright from track.#A) 2.870 ftB) 2.838 ft

C) 2.507 ftD) 2.120 ft23762. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Flying from EDTM MENGEN airport (48°03N 009°22E) toEDPJ LAICHINGEN airport (48°30N 009°38E). Find magneticcourse and the distance.A) Magnetic course 202°, distance 44 NM.B) Magnetic course 202°, distance 28 NM.C) Magnetic course 022°, distance 44 NM.#D) Magnetic course 022°, distance 28 NM.

033-03 PRACTICAL FLIGHT PLANNING18© 2008AVIATIONEXAM.com23763 (C) 23764 (B) 23765 (B) 23767 (B) 23802 (A) 23803 (A) 23804 (B) 23805 (C)23806 (D) 23807 (B) 23808 (B) 23809 (A)23763. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Name the frequency of TANGO VORTAC (48°37N



009°16E):A) 118,60 MHzB) 422 kHz#C) 112,50 MHzD) 118,80 MHz23764. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)What minimum grid area altitude is applicable for EDPJLAICHINGEN airport (48°30N 009°38E)?A) 46#B) 43C) 2.434 ftD) 402 m23765. (all)(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)What minimum grid area altitude is applicable for EDTMMENGEN airport (48°03N, 009°22E)?A) 43#B) 46C) 1819 ft.D) 1120 m.23767. (all)

(Refer to Jeppesen Student Route Manual VFR+GPS chartED-6)Which navigation aid is located in position 48°55N009°20E?A) NDB#B) VOR/DMEC) TACAND) VOR23802. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Sabadell Areachart (19-1) or figure VFR-12)What is the published frequency for Barcelona ATIS?#A) 118,65 MHz

B) 119,10 MHzC) 124,70 MHzD) 120,80 MHz23803. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Sabadell Aerodromechart (19-2) or figure VFR-13)What is the published initial VFR arrival procedure for helicopters?#A) From the southwest.B) From reporting point N or E.C) From Sant Cugat del Vallis.D) From reporting point MARTORELL or MOLLET.23804. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Barcelona Area

chart (10-1V) or figure VFR-16)If routeing along the Barcelona VFR corridors from ReusREP to SAN CELONI, what is the maximum altitude availablewithout changing?A) 3.000 ft#B) 2.000 ftC) 4.500 ftD) 3.500 ft23805. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon)



Approach chart (29-1) or figure VFR-10)What is the published frequency to use for start up?A) Approach 119,10.B) Tower 118,10.#C) Ground 121,70.D) ATIS 123,40.23806. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon)Approach chart (29-1) or figure VFR-10)What is the frequency and ident of the DVOR/DME shown atthe northern end of Hellinikon airfield?A) 294 HNB) 357 KVRC) 275 HK#D) 114,40 ATH23807. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon)Approach chart (29-1) or figure VFR-10)What is the total distance when following the VFR routeingfrom Abeam Patroklos to Hellinikon?A) 19 km#B) 19 NMC) 14 NMD) 16 NM

23808. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon)Area chart (29-1) or figure VFR-10)What is the maximum permitted altitude if routeing inboundfrom Abeam Patroklos to Hellinikon?A) 1.500 ft#B) 300 ftC) 4.000 ftD) 322 ft23809. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon)Landing Chart (29-2) or figure VFR-11)What is the position of the Aerodrome Reference Point?

#A) 37°53,8N 23°43,7EB) 37°54,2N 23°44,3EC) 37°53,2N 23°43,3ED) 37°54,8N 23°44,7E

033-03 PRACTICAL FLIGHT PLANNING19© 2008AVIATIONEXAM.com23810 (D) 23813 (D) 23814 (D) 23815 (B) 23816 (A) 23817 (A) 23818 (A) 23819 (D)23820 (A) 23821 (B) 23822 (C) 23823 (A)23810. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Athinai (Hellinikon)

Aerodrome chart (29-2) or figure VFR-11)What are the available outbound tracks for helicoptersfrom the helicopter landing point at approximately 37°54N23°44E?A) 215° or 035°.B) 245° or 035°.C) 065° or 245°.#D) 065° or 215°.23813. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce)



Information Page (19-6) or figure VFR-2)Which of the Helicopter Routes in the Aberdeen CTR is thedesignated low visibility/bad weather route?A) H4B) H1C) H2#D) H623814. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, De Kooy Aerodromechart (19-2) or figure VFR-8)How many Helicopter landing points are shown on the chartfor De Kooy Aerodrome?A) Fifteen (15)B) Four (4)C) Two (2)#D) Six (6)23815. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, De Kooy Areachart (19-1) or figure VFR-7)What is (i) the frequency and (ii) QDM of the ILS at De KooyAerodrome?A) (i) 123,30; (ii) 220° (M)#B) (i) 109,70; (ii) 216° (M)C) (i) 109,70; (ii) 214° (T)

D) (i) 123,30; (ii) 220° (T)23816. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, De Kooy Areachart (19-1) or figure VFR-7)What is the minimum altitude over the Quiet Zone in thevicinity of De Kooy?#A) 1.500 ftB) 3.500 ftC) 3.000 ftD) 32.800 ft23817. (HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce)Information Page (19-6) or figure VFR-2)

According to the Helicopter Local Flying Regulations,approaches to the Helistrip 23 aiming point should be ona heading of:#A) 218° (M)B) 230° (M)C) 228° (M)D) 218° (T)23818. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce)Information Page (19-6) or figure VFR-2)What are the designated departure routes when using (i)Rwy 34 and (ii) Rwy 05?#A) (i) H2; (ii) H4

B) (i) H6; (ii) H2C) (i) H1; (ii) H3D) (i) H5; (ii) H123819. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce)Information Page (19-6) or figure VFR-2)What is the designated departure route when using Runway23 in bad weather and/or low visibility?A) H5B) H3



#C) H1D) H623820. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce)Information Page (19-6) or figure VFR-2)What is the minimum flight visibility required when landingat Aberdeen (Dyce) Airport other than when using RouteH6?#A) 2 kmB) 3 kmC) 4 kmD) 5 km23821. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce)Area chart (19-5) or figure VFR-3)What ATIS frequency(ies) is/are available when on theground?A) 121,85 only.#B) 114,30 or 121,85.C) 121,70 only.D) 121,70 or 121,85.23822. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen (Dyce)Area chart (19-5) or figure VFR-3)

What is the ATIS frequency that may not be used when inflight?A) 121,70B) 114,30#C) 121,85D) 118,1023823. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen InformationPage (19-3) or figure VFR-4)The East Apron and Eastern Twy have restricted access.The maximum permitted wingspan:#A) is 20 m.B) is the same as a Beech 200.

C) is 20 ft.D) does not apply to helicopters.

033-03 PRACTICAL FLIGHT PLANNING20© 2008AVIATIONEXAM.com23824 (A) 23825 (C) 23826 (A) 23827 (B) 23828 (B) 24742 (D) 24748 (C) 24896 (B)25046 (A) 25562 (C) 25563 (B) 25564 (D) 25565 (C)23824. (HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Aberdeen Aerodromechart (19-2) or figure VFR-5)How many runways are available for use by helicopters?

#A) Seven (7)B) Five (5)C) Six (6)D) Two (2)23825. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM (VFR) , Aberdeen(Dyce) Area chart (10-1V) or figure VFR-1)What is the elevation of the highest obstacle within theboundary of Aberdeen Control Area?A) 2.025 ft



B) 1.245 ft#C) 2.105 ftD) 1.733 ft23826. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM (VFR), Aberdeen(Dyce) Area chart (10-1V) or figure VFR-1)Which of the following frequencies is listed as available forcontact with Aberdeen ATSU?#A) 135,17B) 126,25C) 119,87D) 114,3023827. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM (VFR), Aberdeen(Dyce) Area chart (10-1V) or figure VFR-1)What is the correct frequency to contact Scottish Informationwhen overhead reporting point BANCHORY to thesouthwest of Aberdeen Airport?A) 126,25#B) 119,87C) 134,10D) 135,1723828. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM (VFR), Aberdeen

(Dyce) Area chart (10-1V) or figure VFR-1)What is the elevation of the highest ground within theboundary of Aberdeen Control Area?A) 2.105 ft.#B) 2.025 ft.C) 1.733 ft.D) 1.245 ft.24742. (all)(Refer to Jeppesen Manual ED-6)What is the navaid at 48°30N 007°34E?A) VORTAC/NDBB) NDBC) TACAN

#D) VOR/DME24748. (all)(Refer to Jeppesen Manual - chart ED-6)You are at position 47°59N 010°15E. Which Flight InformationService should you contact?A) Memmingen 117,20 Mhz.B) Memmingem 135,60 Mhz.#C) Munchen 126,95 Mhz.D) Munchen 131,22 MHz.24896. (all)(Refer to Jeppesen Manual chart ED-6)STUTTGART airport (48°41N 009°11E) is within what sortof airspace:

A) class E.#B) class D.C) class A.D) class G.25046. (all)(Refer to Jeppesen Student Manual - chart ED-6)What is the main true track and distance from TRA (47°42N008°26E) to KPT (47°45N 010°21E)?#A) 087° / 143 kmB) 267° / 78 NM



C) 087° / 88 NMD) 091° / 76 NM25562. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Esbjerg Aerodromechart (19-2) or figure VFR-15)What are the dimensions of runway 08/26 at Esbjerg?A) 8.530 ft x 45 ftB) 8.530 m x 45 m#C) 2.600 m x 45 mD) 2.600 ft x 148 ft25563. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Esbjerg Aerodromechart (19-2) or figure VFR-15)What is the position of the Aerodrome Reference Point atEsbjerg?A) 55°31,6N 008°33,1W#B) 55°31,6N 008°33,1EC) 55°32,2N 008°34,9ED) 55°32,2N 008°34,9W25564. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Esbjerg Areachart (19-1) or figure VFR-14)What is the course and distance from Locator HP to thethreshold of Runway 08?

A) 080° (T) / 4,2 km.B) 080° (T) / 4,2 NM.C) 080° (M) / 4,2 km.#D) 080° (M) / 4,2 NM.25565. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, Esbjerg Areachart (19-1) or figure VFR-14).What is the track and distance shown on the chart fromVOR/DME SKR (55°13,8N 009°12,9E to overhead Esbjerg(55°31,6N 008°33,2E)?A) 308° (T) / 29 NM.B) 308° (M) / 29 km.#C) 308° (M) / 29 NM.

D) 308° (T) / 29 km.

033-03 PRACTICAL FLIGHT PLANNING21© 2008AVIATIONEXAM.com25566 (B) 25567 (A) 4348 (A) 12268 (D) 14444 (A) 25012 (B) 1126 (C) 1127 (D)12525 (D) 12528 (B)25566. (AIR: atpl, cpl; HELI: atpl, cpl)(Refer to Jeppesen Student Manual - TRM, The NetherlandsAerodrome Directory (7-3) or figure VFR-6)What is the local time (LT) in the Netherlands in (i) Winterand (ii) Summer?

A) (i) LT - 2 Hours = UTC; (ii) LT - 1 Hour = UTC#B) (i) LT - 1 Hour = UTC; (ii) LT - 2 Hours = UTCC) (i) LT = UTC + 2 Hours; (ii) LT = UTC + 1 HourD) (i) LT = UTC - 1 Hour; (ii) LT = UTC - 2 Hours25567. (AIR: atpl, cpl; HELI: atpl, cpl)Refer to Jeppesen Student Manual - TRM, Greece AerodromeDirectory (7-3) or figure VFR-9)What is the local time (LT) in Greece in (i) Winter and (ii)Summer?#A) (i) LT = UTC + 2 Hours; (ii) LT = UTC + 3 Hours



B) (i) LT = UTC - 2 Hours; (ii) LT = UTC - 3 HoursC) (i) LT + 2 Hours = UTC; (ii) LT + 3 Hours = UTCD) (i) LT - 3 Hours = UTC; (ii) LT - 2 Hours = UTC033-03-02 Navigation plans4348. (all)What is Total Elapsed Time on a VFR flight plan?#A) From takeoff to overhead destination.B) From takeoff to overhead destination + 15 mins.C) From takeoff to landing.D) From taxi to arrival on the gate.12268. (all)(Refer to Route Manual VFR+GPS chart ED-6 or figureED6-12)Flying from SAULGAU airport (48°02N 009°31E) to ALTENSTADTairport (47°50N 010°53E). Find magnetic courseand the distance.A) Magnetic course 282°, distance 56 NM.B) Magnetic course 102°, distance 82 NM.C) Magnetic course 078°, distance 82 NM.#D) Magnetic course 102°, distance 56 NM.14444. (all)An aircraft flight planning chart states that the time to reachFL190 at a given gross mass is 22 minutes with a still airdistance of 66 NM. The ground distance travelled when the

average headwind component is 35 kts will be:#A) 53 NMB) 61 NMC) 79 NMD) 85 NM25012. (AIR: all)At 1000 UTC Shanwick Oceanic clear you to enter the Oceaniccontrol Area at 47°00N 008°W, 220 track miles fromyour current position, at time 1033 UTC. At FL200, ISA conditionsand with TAS 430 kts, headwind 30 kts, FMS beingunavailable, what is the required Mach number to complywith this instruction?A) M 0,75

#B) M 0,70C) M 0,60D) M 0,80033-03-03 Simple fuel plans1126. (AIR: all)In a flight plan when the destination aerodrome is A and thealternate aerodrome is B, the final reserve fuel for a turbojetengine aeroplane corresponds to:A) 15 minutes holding 2.000 feet above aerodrome A.B) 30 minutes holding 2.000 feet above aerodrome B.#C) 30 minutes holding 1.500 feet above aerodrome B.D) 30 minutes holding 1.500 feeI above aerodrome A.1127. (AIR: atpl, cpl; HELI: atpl, cpl)

Given:Dry operating mass (DOM): 33.000 kgLoad: 8.110 kgFinal reserve fuel: 983 kgAlternate fuel: 1.100 kgContingency fuel: 102 kgThe estimated landing mass at alternate should be:A) 42.312 kgB) 41.110 kgC) 42.210 kg



#D) 42.195 kg12525. (all)A helicopter is on a 150 NM leg to an off-shore oil rig. ItsTAS is 130 kts with a 20 kts tailwind, its endurance is 3hrs 30 min without reserve. Upon reaching destination, itis asked to proceed outbound to locate a ship in distress,on a track which gives a 15 kts tailwind. Maintaining zeroreserve on return to the oil rig, the helicopter can fly outboundfor distance of:A) 224,5 NMB) 158,6 NMC) 222,1 NM##D) 160,3 NM12528. (all)You are to determine the maximum fuel load which can becarried in the following conditions:- dry operating mass: 2.800 kgtrip fuel: 300 kgpayload: 400 kgmaximum takeoff mass: 4.200 kgmaximum landing mass: 3.700 kgA) 500 kg#B) 800 kgC) 1.000 kg

D) 700 kg033-03 PRACTICAL FLIGHT PLANNING22© 2008AVIATIONEXAM.com24752 (B) 1165 (A) 12267 (B) 12269 (D)24752. (all)(Refer to figure 033-08)Given:Trip time 2 hrs 37 min from departure to destination at 2.500RPM, 65% power. For the climb and descent add 13 minof cruise fuel. Reserve = 30% of trip fuel. Taxy fuel is 5 US

gal.What is the min Ramp Fuel?A) 88 gal#B) 93 galC) 120 galD) 115 gal033-03-04 Radio planning practice1165. (all)(Refer to Jeppesen Manual ED-6 or figure ED6-02)What is the frequency for Stuttgart ATIS?#A) 126,125 MHzB) 135,775 MHzC) 112,250 MHZ

D) 126,12 kHz12267. (all)(Refer to Route Manual VFR+GPS chart ED-6 or figureED6-02)Give the name and frequency of the Flight Information Servicefor an aeroplane in position (47°59N, 010°14E).A) MEMMINGEN INFORMATION 122,1 MHz.#B) MUNCHEN INFORMATION 126,95 MHz.C) MUNCHEN INFORMATION 120,65 MHz.D) FRANKFURT INFORMATION 128,95 MHz.



12269. (all)(Refer to Route Manual VFR+GPS chart ED-6 or figureED6-11)Which navigation aid is located in position 48°30N007°34E?A) NDBB) VORC) TACAN#D) VOR/DME

033-04 IFR (AIRWAYS) FLIGHT PLANNING23© 2008AVIATIONEXAM.com2194 (C) 2199 (D) 2208 (D) 2222 (C) 2226 (A) 2234 (C)033-04-01 Meteorological considerations2194. (AIR: atpl, ir; HELI: atpl, ir)Given the following TAF / METAR:What are the lowest cloud conditions (oktas/feet) forecastfor JOHANNESBURG/JAN SMUTS at 0300 UTC?JOHANNESBURG/JAN SMUTSFAJS/JNBFT0900 120900Z 121212 36010KT 9999 FEW030CB FEW035PROB40 TEMPO 1318 VRB15KT 3000 TSRA SCT030CB

BKN080 FM2000 03005KT CAVOK BECMG 0204 SCT008SCT100 PROB30 0305 3000 BCFG BKN004 FM0800 34012KT9999 SCT025 T25/12Z T15/03Z T27/12Z=A) 5 to 7 at 800.B) 3 to 4 at 800.#C) 5 to 7 at 400.D) 3 to 4 at 400.2199. (AIR: atpl, ir; HELI: atpl, ir)Given the following TAF / METAR:Which best describes the weather, if any, at Lyon / Satolasat 1330 UTC?LYONS/SATOLAS LFLL/LYS SA1330 121330Z 14007KT9000 -TSRA FEW020CB SCT033TCU BKN046 09/07 Q1003

NOSIG=FC1100r 121100Z 121221 VRB03KT 9999 FEW010 SCT020BKN040 BECMG 1821 33006KT TEMPO 1221 VRB15G20KT4000 SHRA SCT008 BKN015=FT1000 121000Z 121812 33004KT 9999 SCT025 BKN060BECMG 2224 VRB02KT 8000 SCT010 SCT020 BECMG 02041500 BR BKN003 TEMPO 0407 0800 FG OVC002 BECMG0810 33006KT 9999 SCT015 BKN030=A) Nil.B) Frequent rain showers.C) Fog.#D) Light rain associated with thunderstorms.2208. (AIR: atpl, ir; HELI: atpl, ir)

Refer to weather information for Birmingham.What is the total time for which the weather is forecast?BIRMINGHAM EGBB/BHXSA0850 280850 18014kt 9999 SCT024 BKN030 BKN04512/08 Q1011=FC0600 280600Z 280816 190015G27kt 9999 BKN025 TEMPO0812 5000 - DZ BKN012 BECMG 1214 19022G37=FT0400 280434Z 281212 19022G37 9999 BKN025 TEMPO1902 5000 RA BKN010 BECMG 2201 25007ktA) 9 hours.



B) 18 hours.C) 24 hours.#D) 28 hours.2222. (AIR: atpl, ir; HELI: atpl, ir)Given the following TAF / METAR:What maximum windspeed (kts) is forecast for BORDEAUX/ MERIGNAC AT 1600 UTC?Bordeaux / MerignacLFBD / BODSA1330 121330Z 21005KT 9000 FEW030TCU FEW 033CBSCT040 BKN100 09/08 Q1005 TEMPO 25015G25KT 3000TSRA SCT005 BKN015CB=FC1100r 121100Z 121221 28010KT 9999 -RA SCT020FEW025CB SCT040 TEMPO 1218 25015G25KT 6000SHRA SCT008 SCT020CB BKN033 PROB30 TEMPO 121828020G30KT 3000 TSRA SCT005 BKN015CB BECMG 182122004KT 8000 NSW FEW006 BKN030=FT1000 121000Z 121812 30010KT 9999 SCT020 FEW025CBBKN040 BECMG 1822 22004KT 8000 FEW006 BKN030 BECMG0306 24005KT 6000 SCT007 SCT015 BKN090 BECMG1012 -RA=A) 10B) 5#C) 30

D) 252226. (AIR: atpl, ir; HELI: atpl, ir)A METAR reads:SA1430 35002KY 7000 SKC 21/03 QI024 =Which of the following information is contained in thisMETAR?#A) Temperature/dewpoint.B) Runway in use.C) Day/month.D) Period of validity.2234. (AIR: atpl, ir; HELI: atpl, ir)Refer to the TAF below:What are the lowest cloud conditions forecast for 1900 UTC

at HAMBURG (EDDH)?TAF EDDH ISSUED ATEDDH 0624 21010KT CAVOKBECMG 0810 9999 SCT025 SCT040PROB30 TEMPO 1218 7000 -RADZ BKN012BECMG 1620 7000 BKN020TEMPO 1824 4000 RADZ BKN005A) 5 to 7 at 1.200 ft.B) 3 to 4 at 500 ft.#C) 5 to 7 at 500 ft.D) 5 to 7 at 2.000 ft.

033-04 IFR (AIRWAYS) FLIGHT PLANNING

24© 2008AVIATIONEXAM.com2243 (B) 2250 (C) 2258 (C) 2903 (C) 4304 (A) 4307 (A) 4318 (C) 4320 (C)4330 (A) 4331 (A) 4335 (D)2243. (AIR: atpl, ir; HELI: atpl, ir)Refer to weather information for Birmingham.What is the lowest visibility forecast at 280800Z?BIRMINGHAM EGBB/BHXSA0850 280850 18014kt 9999 SCT024 BKN030 BKN045



12/08 Q1011=FC0600 280600Z 280816 190015G27kt 9999 BKN025 TEMPO0812 5000 - DZBKN012 BECMG 1214 19022G37=FT0400 280434Z 281212 19022G37 9999 BKN025 TEMPO1902 5000 RABKN010 BECMG 2201 25007ktA) 50 km#B) 5.000 mC) 10 km or moreD) 2.500 m2250. (AIR: atpl, ir; HELI: atpl, ir)Given the following TAF/ METAR:What is the earliest time (UTC), if any, that thunderstormsare forecast for Tunis/Carthage?TUNIS/CARTHAGEDTTA/TUNSA1330 121330Z 24008KT 9999 FEW023 BKN200 24/08Q1007=FC1200 121200Z 121322 28012KT 9999 FEW030 SCT200BECMG 1518 30014KT SCT026 BKN200 TEMPO 172232014G25KT 6000 -SHRA FEW023CB=FT1020 121020Z 121212 26012KT 9999 FEW030 SCT200BECMG 1619 30014KT 8000 SCT020 BKN100 TEMPO 1802

32014G25KT 6000 SHRA OR -TSSHRA FEW023CB BECMG0406 28019KT 6000 BECMG 0810 8000 SCT020 SCT026TEMPO 5000 -SHRA FEW026CB=A) 0800B) 1300#C) 1800D) nil2258. (AIR: atpl, ir; HELI: atpl, ir)A METAR reads:SA 1430 35002KT 7000 SKC 21/03 Q1024Which of the following information is contained in this report?A) Day, month.B) Runway in use.

#C) Temperature, dewpoint.D) Period of validity.2903. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)Which best describes be maximum intensity of icing, if any,at FL150 in the vicinity of BUCHAREST (45°N 026°E)?A) SevereB) Nil#C) ModerateD) Light4304. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)Which describes the maximum intensity of icing, if any, at

FL180 in the vicinity of Casablanca (33°N 008°W)?#A) SevereB) ModerateC) LightD) Nil4307. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)What is the temperature deviation (°C) from ISA over 60°N000°E?#A) -9



B) -55C) +2D) +94318. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)What is the maximum wind speed over Italy?A) 100 kts at FL380.B) 110 kts at FL380 but the maximum not shown on thechart.#C) 110 kts at FL380.D) 130 kts at FL340.4320. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)What mean temperature (°C) is likely on a course 360° (T)from 40°N to 50°N at 020°E?A) -47B) -46#C) -49D) -504330. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)The approximate mean wind component (kt) along the truecourse 180 from 50°N to 40°N at 020°E is:#A) 55 kts tailwind.

B) 40 kts tailwind.C) 70 kts tailwind.D) 55 kts headwind.4331. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)At position 38°N 15°E what is the worst hazard which couldbe expected?#A) Engine flame-out and windscreen damage.B) Turbulence.C) Reduced visibilty.D) Nil.4335. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)

What is the wind associated with Munich (50°N 010°E)?A) Maximum wind of 160 kts from 360°(T).B) Maximum wind of 120 kts from 260° (M).C) Maximum wind of 100 kts from 360° (T).#D) Maximum wind of 140 kts from 290° (T).

033-04 IFR (AIRWAYS) FLIGHT PLANNING25© 2008AVIATIONEXAM.com4336 (D) 4350 (D) 4351 (D) 4353 (D) 4355 (B) 4359 (C) 12289 (C) 12290 (A)12291 (D) 12293 (A) 12294 (C) 12295 (A) 12296 (D) 12297 (C)4336. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to figures 033-75)Which of the following flight levels, if any, is forecast to beclear of significant cloud, icing and CAT along the markedroute from SHANNON (53°N 10°W) to BERLIN (53°N 13°E)?A) NoneB) FL290C) FL210#D) FL2504350. (AIR: atpl, ir)(Refer to figure 033-79)



The approximate mean wind component at Mach 0,78 alongthe true course 270° at 50°N from 000° to 010°W is?A) 25 kts tailwind component.B) 55 kts headwind component.C) 35 kts tailwind component.#D) 40 kts headwind component.4351. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)In the vicinity of WARSAW (52°N 020°E) the tropopause isat approximate:A) FL400B) FL370C) FL350#D) FL3304353. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)The surface system over London (51°N 000°E) is a / an:A) cold front moving west.B) warm front moving north.C) stationary occluded front.#D) occluded front moving east.4355. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)In the vicinity of Paris (49°N 003°E), the tropopause is at

approximately:A) FL340#B) FL400C) FL350D) FL3804359. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)Over PRAGUE (50N 014E) the lowest FL listed which is unaffectedby CAT is:A) 350B) 300#C) 270D) 400

12289. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)The surface weather system over England (53°N 002°W)is:A) a warm front moving southeast.B) a cold front moving east.#C) an occluded front moving east.D) a depression moving north.12290. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)Which best describes the significant cloud, if any, forecastfor the area southwest of BODO (67°N 014°E)?#A) 5 to 7 oktas CU and CB base below FL100, tops FL180.

B) 5 to 7 oktas CU and CB base FL100, tops FL180.C) 3 to 7 oktas CU and CB base below FL100, tops FL180.D) Nil.12291. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)Which best describes the maximum intensity of CAT, if any,forecast for FL330 over BENGHAZI (32°N 020°E)?A) LightB) ModerateC) Severe



#D) Nil12293. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)The wind velocity over ITALY is:#A) a maximum of 110 kts at FL380.B) 130 kts at FL380 maximum velocity not shown on chart.C) a maximum of 160 kts at FL380.D) 110 kts at FL380 maximum velocity not shown on chart.12294. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)The wind direction and velocity (° / kts) at 50°N 040°E is:A) 200/70B) 020/80#C) 020/70D) 350/7012295. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)The wind direction and velocity (° / kts) at 60°N 015°W is:#A) 290/155B) 320/155C) 110/155D) 290/18512296. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)

What is the mean temperature deviation (°C) from the ISAover 50°N 10°W?A) +2B) +9C) +13#D) -212297. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)The wind direction and velocity (° / kts) at 40°N 040°E is:A) 150/75B) 300/75#C) 330/75D) 330/85

033-04 IFR (AIRWAYS) FLIGHT PLANNING26© 2008AVIATIONEXAM.com12298 (D) 12299 (C) 12300 (C) 12301 (C) 12533 (D) 12534 (D) 12535 (B) 12536 (B)12537 (A) 12538 (A) 12539 (B) 12540 (A) 12541 (A) 12542 (B)12298. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-70)What minimum visibility (m) is forecast for 0600 UTC atLONDON LHR (EGLL)?A) 2.200B) 5.000

C) 10.000#D) 1.50012299. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-70)Which affects the visibility for 1330 UTC at TUNIS (DTTA)?A) HazeB) Mist#C) SmokeD) Dust12300. (AIR: atpl, ir; HELI: atpl, ir)



(Refer to figures 033-70)What is the earliest time (UTC), if any, that thunderstormsare forecast for DUBAI (OMDB)?A) 1000B) 1200#C) 1400D) Nil forecast12301. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)What mean temperature (°C) is likely on a course of 360° (T)from 40°N to 50°N at 040°E?A) -49B) -50#C) -47D) -4612533. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)The W/V (°/kts) at 50°N 015°W is:A) 100/75B) 175/90C) 310/85#D) 355/9012534. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)

What mean temperature (°C) is likely on a true course of270° from 025°E to 010°E at 45°N?A) -48B) -52C) -54#D) -5012535. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-79)The W/V (°/kts) at 40°N 020°W is:A) 185/65#B) 005/65C) 185/60D) 005/60

12536. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-82)What is the temperature deviation (°C) from ISA over 50°N010°E?A) +10#B) -10C) -55D) +212537. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-80)The W/V (°/kts) at 60°N 15°W is:#A) 290/40B) 110/40

C) 280/20D) 100/2012538. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-77)Which best describes the significant cloud forecast for thearea over WARSAW (52°N 021°E)?#A) 5 to 7 oktas CU and AC base below FL100 tops FL120.B) 3 to 4 oktas CU and AC base below FL100 tops FL120.C) 5 to 7 oktas CU and AC base FL100 tops FL120.D) 3 to 4 oktas CU and AC base FL100 tops FL120.



12539. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-77)Which best describes the maximum intensity of icing, ifany, at FL100 overhead WARSAW (52°N 021°E)?A) Severe#B) ModerateC) LightD) Nil12540. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)Which describes the intensity of icing, if any, at FL180 inthe vicinity of the CANARY ISLANDS (29°N 015°W)?#A) Moderate or severe.B) Moderate.C) Light.D) Nil.12541. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-77)The surface system over ZURICH (48°N 008°E) is:#A) occluded front moving east.B) quasi-stationary front moving east.C) quasi-stationary front moving south.D) occluded front moving north-east.12542. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to figure 033-77)In the vicinity of PARIS (49°N 002°E) the tropopause is atabout:A) FL340#B) FL350C) FL400D) FL450

033-04 IFR (AIRWAYS) FLIGHT PLANNING27© 2008AVIATIONEXAM.com12543 (A) 12544 (D) 12545 (C) 12546 (B) 12547 (A) 12548 (C) 12549 (A) 12550 (B)

12551 (B) 12552 (C) 22898 (C) 23747 (C) 23748 (C) 23749 (A)12543. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-77)Which best describes the significant cloud forecast overZURICH (48°N 008°E)?#A) Broken AC/CU base below FL100 tops FL190, embeddedisolated CB base below FL100 tops FL300.B) Well separated CB base FL100 tops to FL300.C) Isolated CB embedded in layer cloud, surface to FL300.D) 5 to 7 oktas CU and AC base below FL100 tops to FL300.12544. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)Which describes the maximum intensity of turbulence, if

any, at FL210 in the vicinity of the CANARY ISLANDS (29°N015°W)?A) NilB) LightC) Moderate#D) Severe12545. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-77)The maximum wind velocity (°/kts) over ATHENS (37°N024°E) is:



A) 300/90B) 270/320#C) 250/110D) 270/9012546. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-77)Over LONDON (51°N 000°E/W), the lowest FL listed which isunaffected by CAT is:A) 360#B) 230C) 280D) 31012547. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-69)The forecast period covered by the PARIS/CHARLES-DEGAULLETAFs totals (hours):#A) 27B) 9C) 18D) 2012548. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-69)The lowest cloud conditions (oktas/ft) at BORDEAUX/MERIGNACat 1230 UTC were:

A) 3 to 4 at 2.000.B) 3 to 4 at 800.#C) 1 to 2 at 3.000.D) 1 to 4 at 3.000.12549. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-69)The surface wind velocity (°/kts) at PARIS/CHARLES-DEGAULLEat 1330 UTC was:#A) 270/04B) 300/05C) 270/08D) 180/1212550. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to figures 033-69)Which is the heaviest type of precipitation, if any, forecastfor BORDEAUX/MERIGNAC at 1000 UTC?A) Nil.#B) Light rain.C) Rain showers.D) Heavy rain associated with thunderstorms.12551. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-69)What minimum visibility is forecast for PARIS/CHARLESDE-GAULLE at 2100 UTC?A) 2.000 m#B) 6.000 m

C) 10 kmD) 8.000 m12552. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-70)Which best describes the weather, if any, forecast for JOHANNESBURG/JAN SMUTS at 0400 UTC?A) CAVOK.B) Mist and/or fog.#C) Patches of fog.D) Rain associated with thunderstorms.



22898. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-70)What affects the visibility forecast for TUNIS (DTTN)?A) HazeB) Mist#C) SmokeD) Dust23747. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-78)The maximum wind velocity (°/kts) immediately north ofTUNIS (36°N 010°E) is:A) 250/85B) 180/105#C) 190/95D) 280/11023748. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-78)Which describes the maximum intensity of turbulence, ifany, forecast for FL260 over TOULOUSE (44°N 001°E)?A) Light.B) Nil.#C) Severe.D) Moderate.23749. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to figure 033-78)Which best describes the significant cloud forecast overTOULOUSE (44°N 001°E)?#A) Broken AC/CU base below FL100 tops FL150, embeddedisolated CB base below FL100 tops FL270.B) Well separated CB base FL100 tops to FL270.C) Isolated CB embedded in layer cloud, surface to FL270.D) 5 to 7 oktas CU and AC base below FL100 tops to FL270.

033-04 IFR (AIRWAYS) FLIGHT PLANNING28© 2008AVIATIONEXAM.com

23790 (B) 23791 (B) 23792 (D) 23793 (D) 23794 (D) 23795 (A) 23796 (A) 23797 (A)25062 (C) 25063 (D) 25064 (A) 25069 (A) 25158 (B) 25159 (D)23790. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-82)The W/V (°/kts) at 40°N 020°W is:A) 334/40##B) 310/40C) 135/40D) 155/4023791. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-82)The W/V (°/kts) at 50°N 015°W is:A) 310/85

B) 290/75C) 310/75D) 100/7523792. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-82)The W/V (°/kts) at 60°N 015°W is:A) 115/60B) 300/70C) 320/60#D) 300/60



23793. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-78)In the vicinity of SHANNON (52°N 009°W) the tropopauseis at about:A) FL270B) FL350C) FL300#D) FL36023794. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-78)The surface system over VIENNA (48°N 016°E) is a:A) cold front moving west.B) warm front moving north.C) stationary occluded front.#D) cold front moving east.23795. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-78)Which best describes the maximum intensity of icing, ifany, at FL160 in the vicinity of BERLIN (53°N 013°E)?#A) ModerateB) SevereC) LightD) Nil23796. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to figure 033-78)Which best describes the significant cloud forecast for thearea east of Tunis (36°N 010°E)?#A) 5 to 7 oktas CU and AC base below FL100 tops FL180.B) 3 to 4 oktas CU and AC base below FL100 tops FL180.C) 5 to 7 oktas CU and AC base FL100 tops FL180.D) 3 to 4 oktas CU and AC base FL100 tops FL160.23797. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-78)Which describes the intensity of icing, if any, at FL150 inthe vicinity of TOULOUSE (44°N 01°E)?#A) Moderate or severe.B) moderate.

C) Light.D) Nil.25062. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-76)The lowest height of the tropopause on the whole chart is:A) FL240B) FL250#C) FL220D) FL20025063. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-76)On a flight from Cairo to Madrid at FL350 when Mt. Etna isnot active, what sort of in-flight weather hazard might you

encounter?A) None.B) Severe icing and turbulence within any CB.C) Light CAT.#D) Moderate CAT.25064. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-76)The strongest wind and its level associated with any jetstreamon the chart is:#A) 160 kts at FL320.



B) 100 kts at FL340.C) 150 kts at FL310.D) 130 kts at FL300.25069. (AIR: atpl, ir; HELI: atpl, ir)In a METAR report the abbreviation NOSIG means:#A) no significant change.B) no significant cloud.C) no significant weather.D) no significant problems.25158. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-81)The approximate mean wind velocity expected enroute atFL300 from Oslo (position O) to London (position L) is:A) 056/45#B) 236/45C) 236/51D) 056/5125159. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-81)The approximate mean temperature expected on route atFL260 from Oslo (position O) to London (position L) is:A) -59 °CB) -51 °CC) -56,5 °C

#D) -43 °C033-04 IFR (AIRWAYS) FLIGHT PLANNING29© 2008AVIATIONEXAM.com25160 (C) 25181 (C) 25182 (B) 25183 (C) 26301 (A) 28324 (C) 28332 (A) 28333 (C)28334 (A) 1119 (B) 1124 (B) 1134 (A)25160. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-81)The W/V over position S in Ireland is:A) 330/20B) 330/50

#C) 330/60D) 150/2025181. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-76)Over PALMA (39°N 003°E) the lowest FL listed which is unaffectedby CAT is:A) FL265B) FL380#C) FL260D) FL27025182. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-80)The approximate mean wind component along the true

course 180° from 50°N to 40°N at 005°W is:A) 345/75#B) 325/65C) 145/75D) 165/6025183. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-80)What is the temperature deviation (°C) from ISA over 50°N010°E?A) -58



B) -6#C) +2D) +1026301. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-82)The approximate mean wind component (kts) along truecourse 180° from 50°N to 40°N at 005° W is:#A) tail wind 55 kts.B) tail wind 40 kts.C) tail wind 70 kts.D) headwind 45 kts.28324. (AIR: atpl)(Refer to figures 033-75)The surface weather system over England (53°N 002°W)is:A) a warm front moving southeast.B) a depression moving north.#C) an occluded front moving east.D) a cold front moving east.28332. (AIR: atpl)(Refer to figure 033-80)The W/V (°/kts) at 50°N 015°W is:#A) 300/45B) 120/45

C) 300/25D) 120/4828333. (AIR: atpl)(Refer to figure 033-80)What ISA deviation from the mean temperature (°C) is likelyon a true course of 270° from 025°E to 010°E at 45°N?A) -49°B) +2°#C) -4°D) -2°28334. (AIR: atpl)The surface system west of PARIS is a:#A) cold front moving southeast.

B) warm front moving north.C) stationary occluded front.D) cold front moving west.033-04-02 Selection of routes to destination and alternates1119. (AIR: atpl, ir; HELI: atpl, ir)According to the chart the minimum obstruction clearancealtitude (MOCA) is 8.500 ft. The meteorological data givesan outside air temperature of -20 °C at FL85. The QNH, givenby a meteorological station at an elevation of 4.000 ft is1.003 hPa. What is the minimum pressure altitude whichshould be flown according to the given MOCA?A) 8.500 ft#B) 8.800 ft

C) 12.800 ftD) 8.200 ft1124. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(HI)4 or figure HI-29)The radio navigation aid at ZURICH (47°36N 008°49E) is:A) a NDB, frequency 115,0 kHz.#B) a VOR, frequency 115,0 MHz.C) a VOR/DME, frequency 115,0 MHz.D) a TACAN on channel 11.1134. (AIR: atpl, ir)



On a given path, it is possible to chose between four flightlevels (FL), each associated with a mandatory flight Machnumber (M). The flight conditions, static air temperature(SAT) and headwind component (HWC) are given below:FL370 M 0,80 Ts: -60 °C HWC: -15 ktsFL330 M 0,78 Ts: -60 °C HWC: - 5 ktsFL290 M 0,80 Ts: -55 °C HWC: -15 ktsFL270 M 0,76 Ts: -43 °C HWC: 0The flight level allowing the highest ground speed is:#A) FL270B) FL290C) FL330D) FL370

033-04 IFR (AIRWAYS) FLIGHT PLANNING30© 2008AVIATIONEXAM.com1156 (A) 1157 (D) 1174 (B) 1175 (B) 1176 (A) 1270 (D) 1288 (A) 1304 (D)1312 (A) 2176 (C) 2178 (B) 2179 (C) 2180 (D)1156. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(HI)4 or figure HI-01)The radio aid at STAD (51°45N 004°15E) is:#A) a NDB, frequency 386 kHz.

B) a VOR frequency 386 Mhz.C) a VOR/DME on channel 386.D) a TACAN on channel 386.1157. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(LO)1 or figure LO-01)From SHANNON (52°43,3N 008°53,1W) by W13 to KORAK.What is meant by 5000 by the route centerline?A) MORA 5.000 ft.B) MAA 5.000 ft.C) MOCA 5.000 ft.#D) MEA 5.000 ft.1174. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(LO)1 or figure LO-01)

What radio navigation aid is at SHANNON (52°43N008°53W)?A) VOR SHA 113,3 MHz only.#B) VOR DME SHA 113,3 MHz.C) NDB frequency 353 kHz.D) TACAN frequency 113,3 kHz.1175. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(LO)5 or figure LO-03)See DENKO (52°49N 015°50E). What does 440 DREmean?A) 440 kHz plus ident.#B) 440 kHz plus ident only when BFO switched on.C) 440 kHz plus ident only when BFO switched off.

D) 440 MHz plus ADF only when BFO off.1176. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(LO)1 or figure LO-02)The radio navigation aid at TOPCLIFFE (54°12N 001°22W)is a:#A) TACAN only, channel 84, (frequency 113,7 MHz).B) TACAN, channel 84, and a VOR frequency 113,7 MHzonly.C) TACAN, channel 84, and an NDB frequency 92 kHz only.D) VORTAC, frequency 113,7 MHz, and an NDB frequency



92 kHz.1270. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)4 or figure HI-02)The magnetic course and distance from SALZBURG SBG113.8 (N48 00 E012 54) to STAUB (N48 44 E 012 38) on airwayUB5 is:A) 346 / 43 NM.B) 166 / 64 NM.C) 346 / 64 NM.#D) 346 / 45 NM.1288. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)4 or figures HI-03_a andHI-03_b)Of the following, the preferred airways routing from FRANKFURTFFM 114,2 (50°03N 008°38E) to KOKSY (51°06N002°39E) above FL245, on a Wednesday is:#A) UR10 NTM UB6 BUB ATS.B) UG108 SPI UG1.C) UB69 DINKI UB6 BUB ATS.D) UG1.1304. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)5 or figure HI-05)Given Leg MOULINS (46°42N 003°38,0E) / DIJON (47°16,3N005°05,9E).

Find route designator and distance.A) UG12, 69 NM.B) UG21, 70 NM.C) D, 44 NM.#D) Direct route, 69 NM.1312. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)5 or figure HI-06)What radio navaids are shown at CHIOGGIA (45°04N012°16E)?#A) VOR/DME freq 114,1, NDB freq 408.B) VOR freq 114,1, TACAN freq 408.C) VOR freq 114,1, TACAN channel 408.D) VOR/DME 114,1, DME freq 408.

2176. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)5 or figure HI-07)Of the following, the preferred airways routing from AMBOISEAMB 113,7 (47°26N 001°04E) to AGEN AGN (43°53N000° 52E) above FL200 is:A) UB19 POI UB195.B) UH40 FOUCO UH20 PERIG UA34.#C) UA34.D) UB19 CGC UA25.2178. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(HI)4 or figure HI-08)The magnetic course and distance from ST PREX SPR113,9 (46°28N 006°27E) to FRIBOURG FRI 115,1 (46°47N

007°14E) on airway UG60.A) 048° / 46 NM.#B) 061° / 37 NM.C) 061° / 28 NM.D) 041° / 78 NM.2179. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(LO)5 or figure LO-06)The airway intersection at RONNEBY (56°18N 015°16E) ismarked by:A) a fan marker callsign LP.



B) a TACAN callsign RON.#C) a NDB callsign N.D) a NDB callsign LF.2180. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual STAR charts PARIS (Charlesde-Gaulle - 20-2) or figure AP-04)The route distance from CHIEVRES (CIV) to BOURSONNE(BSN) is:A) 73 NMB) 83 NMC) 88 NM#D) 96 NM

033-04 IFR (AIRWAYS) FLIGHT PLANNING31© 2008AVIATIONEXAM.com2182 (B) 2187 (A) 2189 (A) 2192 (A) 2193 (B) 2196 (B) 2197 (C) 2198 (D)2200 (B) 2202 (B) 2203 (B) 2204 (C)2182. (AIR: atpl, ir; HELI: atpl, ir)An airway is marked 3500T 2100a. This indicates that:A) the minimum enroute altitude (MEA) is 3.500 ft.#B) the minimum obstruction clearance altitude (MOCA) is3.500 ft.

C) the airway base is 3.500 ft MSL.D) the airway is a low level link route 2.100 ft - 3.500 ft MSL.2187. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart NAP or figure HI-23)The initial magnetic course from A (64°N 006°E) to C (62°N020°W) is:#A) 275°B) 267°C) 271°D) 262°2189. (AIR: atpl, ir; HELI: atpl, ir)An aircraft, following a 215° true track at variation 3°W,must fly over a 10.600 ft obstacle with a minimum obstacle

clearance of 1.500 ft. Knowing the QNH received from anairport close by, which is almost at sea-level, is 1.035 andthe temperature is ISA -15 °C, the minimum flight level willbe:#A) 140B) 120C) 130D) 1502192. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 5 or figure LO-04)The magnetic course/distance from EELDE EEL 112,4(53°10N 006°40E) to WELGO (54°18N 007°25E) on airwayA7 are:

#A) 024° / 73 NM.B) 023° / 73 NM.C) 024° / 67 NM.D) 023° / 47 NM.2193. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(HI)5 or figure HI-04)An appropriate FL for flight along airway UG5 from MENDENASBINALSMEN 115,3 (44°36N 003°10E) to GAILLAC GAI115,8 (43°57N 001°50E) is:A) FL280



#B) FL290C) FL300D) FL3102196. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)4 or figure HI-15)The magnetic course / distance from DINKESBUHL DKB117,8 (49°09N 010°14E) to ERLANGEN ERL 114,9 (49°39N011°09E) on airway UR11 are:A) 052° / 97 NM.#B) 050° / 47 NM.C) 133° / 85 NM.D) 230° / 97 NM.2197. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(HI)4 or figure HI-15)An appropriate flight level for flight on airway UG1 fromERLANGEN ERL 114,9 (49°39N 011°09E) to FRANKFURTFFM 114,2 (50°03N 008°38E) is:A) FL300B) FL290#C) FL310D) FL3202198. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)4 or figure HI-16)What is the best route from CLACTON CLN (51°50,9N

001°09,0E) to MIDHURST MID (51°03,2N 000°37,4W)?A) UR12.B) TRIPO UR1 LAM UR1.C) UR123.#D) UB29 LAM UR1.2200. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(LO)1 or figure LO-07)The magnetic course / distance from WALLASEY WAL 114,1(53°23N 003°28W) to LIFFY (53°29N 005°30W) on airwayB1 are:A) 279° / 114 NM.#B) 279° / 85 NM.C) 311° / 114 NM.

D) 311° / 85 NM.2202. (AIR: atpl, ir; HELI: atpl, ir)Using the following information, what is the minimum flightlevel considering the temperature?True track: 215°Mountain elevation: 11.600 ftLocal airfield gives QNH as 1.035 mbRequired terrain clearance: 1.500 ftTemperature: ISA - 15CA) FL150#B) FL140C) FL120D) FL110

2203. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart 5AT(HI) or figure HI-17)On airway PTS P from VIGRA (62°34N 006°02E), the initialgreat circle grid course is:A) 353°#B) 344°C) 347°D) 350°2204. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(HI)4 or figure HI-11)



Planning a IFR flight from Paris Charles de Gaulle (49°00,9N002°36,9E) to London Heathrow (51°29,2N 000°27,9W).Find the average true course from Paris to London.A) 330°B) 142°#C) 322°D) 343°

033-04 IFR (AIRWAYS) FLIGHT PLANNING32© 2008AVIATIONEXAM.com2207 (D) 2209 (B) 2210 (D) 2211 (C) 2212 (B) 2213 (C) 2214 (C) 2215 (D)2216 (B) 2218 (A) 2219 (A) 2223 (D) 2224 (C)2207. (AIR: atpl, ir; HELI: atpl, ir)An IFR flight is planned outside airways on a course of 235°magnetic. The minimum safe altitude is 7.800 ft. Knowingthe QNH is 995 hPa, the minimum flight level you must flyis:A) 80B) 90C) 85#D) 1002209. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Route Manual chart E(HI)4 or figure HI-09)An aeroplane has to fly from Abbeville (50°08,1 N 001°51,3E)to Biggin (51°19,8N 00°00,2E).What is the first FL above FL295 that can be flown on anIFR flight plan?A) FL330#B) FL310C) FL320D) FL3002210. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (HI)5 or figure HI-21)The magnetic course and distance from LIMOGES LMG114,5 (45°49N 001°02E) to CLERMONT FERRAND CMF

117,5 (45°47N 003°11E) on airway UG22 are:A) 046° / 70 NMB) 067° / 122 NMC) 113° / 142 NM#D) 094° / 90 NM2211. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual 5AT(HI) or figures HI-18_a andHI-18_b)Flying from 80°N 170°E to 75°N 11°E. Initial track is 177 grid.What is the initial true track?A) 177°B) 357°#C) 347°

D) 167°2212. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(HI)4 or figure HI-14)An aeroplane has to fly from Salzburg (48°00,2N 012°53,6E)to Klagenfurt (46°37,5N 014°33,8E).Which statement is correct?A) The minimum enroute altitude (MEA) is 13.400 ft.#B) The minimum grid safe altitude on this route is 13.400 ftabove MSL.C) The minimum sector altitude (MSA) is 13.400 ft.



D) The minimum obstacle clearance altitude (MOCA) on thisroute is 10.800 ft above MSL.2213. (AIR: atpl, ir; HELI: atpl, ir)You must fly IFR on an airway orientated 135° magneticwith a MSA at 7.800 ft. Knowing the QNH is 1.025 hPa andthe temperature is ISA + 10°, the minimum flight level youmust fly at is:A) 75B) 80#C) 90D) 702214. (AIR: atpl, ir; HELI: atpl, ir)For an IFR flight using ICAO semi-circular cruising levelson a magnetic track of 200, which is a suitable level?A) FL290B) FL300#C) FL310D) FL3202215. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(HI)4 or figure HI-09)An aeroplane has to fly from Abbeville (50°08,1N 001°51,3E)to Biggin (51°19,8N 000°00,2E).What is the distance of this leg?A) 62 NM

B) 38 NMC) 64 NM#D) 100 NM2216. (AIR: atpl, ir; HELI: atpl, ir)An appropriate flight level for IFR flight in accordance withsemi-circular height rules on a magnetic course of 200° is:A) FL320#B) FL310C) FL290D) FL3002218. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(LO)2 or figure LO-11)The minimum enroute altitude (MEA) that can be maintained

continuously on airway G4 from JERSEY JSY 112,2(49°13N 002°03W) to LIZAD (49°35N 004°20W) is:#A) FL140B) 1.000 ft MSLC) FL60D) 2.800 ft MSL2219. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(LO)5 or figure LO-09)The minimum enroute altitude that can be maintainedcontinuously on airway B65/H65 from DOXON (55°27N018°10E) to RONNE ROE 112,0 (55°04N 014°46E) is:#A) FL100B) 1.000 ft

C) FL60D) 2.500 ft2223. (AIR: atpl, ir; HELI: atpl, ir)An appropriate flight level for IFR flight in accordance withsemi-circular height rules on a course of 180° magnetic is:A) FL105B) FL90C) FL95#D) FL1002224. (AIR: atpl, ir; HELI: atpl, ir)



Unless otherwise stated on charts for standard instrumentdepartures the routes shown are given with:A) magnetic headings.B) true course.#C) magnetic course.D) true headings.

033-04 IFR (AIRWAYS) FLIGHT PLANNING33© 2008AVIATIONEXAM.com2227 (C) 2228 (D) 2229 (B) 2231 (A) 2232 (A) 2235 (A) 2236 (C) 2237 (B)2238 (A) 2242 (A) 2244 (A) 2245 (D)2227. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual STAR 10-2 and instrument approachchart 11-4 ILS/DME Rwy 27R for London Heathrowor figures AP-08 and AP-09)Planning an IFR flight from Paris to London (Heathrow).Name the identifier and frequency of the initial approach fix(IAF) of the BIG2A arrival route:A) EPM; 316 kHz.B) BIG; 115,1 kHz.#C) BIG; 115,1 MHz.D) OCK; 115,3 MHz.

2228. (AIR: atpl, ir; HELI: atpl, ir)An airway is marked 5000 2900a. The notation 5000 is the:A) base of the airway (AGL).B) maximum authorised altitude (MAA).C) minimum holding altitude (MHA).#D) minimum enroute altitude (MEA).2229. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(HI)4 or figure HI-11)Planning a IFR flight from Paris Charles de Gaulle (N49 00.9E002 36.9) to London Heathrow (51°29,2N 000°27,9E). Determinethe preplanning distance by calculating the directdistance plus 10%.A) 188 NM

#B) 207 NMC) 308 NMD) 218 NM2231. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual MADRID BARAJAS 10-2B STARor figure AP-13)For runway 33 arrivals from the east and south, the InitialApproach Fix (IAF) inbound from airway UR10 is:#A) VTBB) CJNC) CENTAD) MOTIL2232. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Jeppesen Manual E(HI)5 or figure HI-22)The minimum enroute altitude available on airway UR160from NICE NIZ 112,4 (43°46N 007°15E) to BASTIA BTA116,2 (42°32N 009°29E) is:#A) FL250B) FL260C) FL210D) FL2002235. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual SID chart for AMSTERDAM



ARNEM (10-3B) or figure AP-14)The route distance from DER 27 to ARNEM is:#A) 67 NMB) 35 NMC) 59 NMD) 52 NM2236. (AIR: atpl, ir; HELI: atpl, ir)(For this question use Route Manual chart E(HI)4 or figureHI-14)An aeroplane has to fly from Salzburg (48°00,2N 012°53,6E)to Klagenfurt (46°37,5N 014°33,8E). Which statement iscorrect?A) The airway UB5 is closed for southbound traffic aboveFL200.B) The airway UB5 cannot be used, there is one way trafficto the north.#C) The airway UB5 can be used for flights to/from Klagenfurtand Salzburg.D) The airway UB5 is closed in this direction except duringthe weekends.2237. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(LO)1 or figure LO-08)The minimum enroute altitude that can be maintained continuouslyon airway G1 from STRUMBLE 113,1 (52°00N

005°02W) to BRECON 117,45 (51°43N 003°16W) is:A) FL80#B) FL110C) 4.100 ft AMSLD) 2.900 ft AMSL2238. (AIR: atpl, ir; HELI: atpl, ir)On an IFR navigation chart, in a 1° quadrant of longitudeand latitude, appears the following information: 80.This means that within this quadrant:#A) the minimum safe altitude is 8.000 ft.B) the minimum flight level is FL80.C) the altitude of the highest obstacle is 8.000 ft.D) the floor of the airway is at 8.000 ft.

2242. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart 5 AT(HI) or figure HI-20)What is the initial grid track from Stornoway (58°12,4N006°11,0W) to Keflavik (64°00N 022°40W)?#A) 320B) 140C) 313D) 1332244. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(HI)4 or figure HI-14)An aeroplane has to fly from Salzburg (48°00,2N 012°53,6E)to Klagenfurt (46°37,5N 014°33,8E). At Salzburg there isstated on the chart D 113,8 SBG. That means:

#A) VOR/DME with identification SBG frequency 113,8 MHzcan be used.B) only the DME with identification SBG can be used, forwhich frequency 113,8 MHz should be tuned, VOR is notavailable.C) VOR/DME SBG will be deleted in the future and cannot beused for navigation.D) ILS/DME 113,8 MHz of Salzburg airport can be used fornavigation.2245. (AIR: atpl, ir; HELI: atpl, ir)



(Refer to Jeppesen Manual Munich STAR charts for MUNICH10-2A,B or figures AP-17, AP-18 and AP-19)With an easterly surface wind, approaching from the west,to Munich via the TANGO VOR. Which is the best STAR andits associated IAF (Initial Approach Fix)?A) Kempten 2T / BETOS.B) NDG 1T / ROKIL.C) RODING 1R / MOOSBURG.#D) AALEN 1T / ROKIL.

033-04 IFR (AIRWAYS) FLIGHT PLANNING34© 2008AVIATIONEXAM.com2247 (A) 2248 (C) 2253 (B) 2254 (D) 2256 (B) 2907 (D) 12251 (C) 12252 (B)12253 (B) 12254 (B) 12255 (A)2247. (AIR: atpl, ir; HELI: atpl, ir)An appropriate flight level for IFR flight in accordance withsemi-circular height rules on a course of 180° (M) is:#A) FL100B) FL90C) FL95D) FL1052248. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Jeppesen Manual E(LO)5 or figure LO-10)An appropriate flight level for flight on airway G9 fromSUBI SUI 116,7 (52°23N 014°35E) to CZEMPIN CZE 114,5(52°08N 016°44E) is:A) FL50B) FL60#C) FL70D) FL802253. (AIR: atpl, ir; HELI: atpl, ir)On an instrument approach chart, a minimum sector altitude(MSA) is defined in relation to a radio navigation facility.Without any particular specification on distance, thisaltitude is valid to:

A) 20 NM#B) 25 NMC) 15 NMD) 10 NM2254. (AIR: atpl, ir; HELI: atpl, ir)An airway is marked FL80 1500 a. This indicates that:A) 1.500 ft MSL is the minimum radio reception altitude(MRA).B) the airway base is 1.500 ft MSL.C) the airways extends from 1.500 ft MSL to FL80.#D) the minimum enroute altitude (MEA) is FL80.2256. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)4 or figure HI-13)

The minimum enroute altitude that can be maintained continuouslyon airway UA34 from WALLASEY WAL 114,1(53°23N 003°08W) to MIDHURST MID 114,0 (51°03N000°37W) is:A) FL245#B) FL290C) 5.300 ftD) 16.800 ft2907. (AIR: atpl, ir; HELI: atpl, ir)(Refer to SID chart Paris Charles de Gaulle 20-3 or figure



AP-03)Planning an IFR-flight from Paris Charles de Gaulle to London.SID is ABB 8A. Assume:Variation 3° WTAS 430 ktsW/V 280/40Distance to top of climb 50 NMDetermine the magnetic course, ground speed and windcorrection angle from top of climb to ABB 116.6.A) MC 169°, GS 450 kts, WCA +4°.B) MC 349°, GS 414 kts, WCA +5°.C) MC 169°, GS 414 kts, WCA +5°.#D) MC 349°, GS 414 kts, WCA -5°.12251. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(HI)4 CAA-Edition, STAR10-2 and Instrument approach chart 11-4 ILS DME Rwy 27Rfor London Heathrow or figures HI-09; AP-08 and AP-09)Planning an IFR-flight from Paris to London (Heathrow).Assume:STAR is BIG 2AVariation 5° WEnroute TAS 430 ktsW/V 280/40Descent distance 76NM

Determine the magnetic course, ground speed and windcorrection angle from ABB 116,6 (50°08,1N 001°51,3E) totop of descent.A) MC 319°, GS 396 kts, WCA -3°.B) MC 141°, GS 396 kts, WCA -3°.#C) MC 321°, GS 396 kts, WCA -3°.D) MC141°, GS 396 kts, WCA +3°.12252. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-30)An appropriate flight level for flight on airway UR1 fromORTAC (50°00N 002°00W) to MIDHURST MID 114,0 (51°03N000°37W) is:

A) FL230#B) FL250C) FL260D) FL24012253. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(HI) 5 CAA-Edition or figureHI-36)An appropriate flight level for flight on airway UR24 fromNANTES NTS 117,2 (47°09N 001°37W) to CAEN CAN(49°10N 000°27W) is:A) FL270#B) FL310C) FL290

D) FL30012254. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (LO)2 or figure LO-13)An appropriate flight level for flight on airway B3 from CHATILLONCTL 117,6 (49°08N 003°35E) to CAMBRAI CMB112,6 (50°14N 003°09E) is:A) FL50#B) FL170C) FL80D) FL60



12255. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (LO)6 or figure LO-16)An appropriate flight level for flight on airway W37 fromCHEB OKG 115,7 (50°04N 012°24E) to RODING RDG 114,7(49°02N 012°32E) is:#A) FL80B) FL40C) FL50D) FL70

033-04 IFR (AIRWAYS) FLIGHT PLANNING35© 2008AVIATIONEXAM.com12256 (B) 12257 (D) 12258 (C) 12273 (B) 12274 (C) 12275 (A) 12276 (C) 12277 (A)12278 (B) 12279 (C) 12280 (A) 12281 (A)12256. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(LO)6 or figure LO-17)An appropriate flight level for flight on airway R10 fromMONTMEDY MMD 109,4 (49°24N 005°08E) to CHATILLONCTL 117,6 (49°08N 003°35E) is:A) FL40#B) FL60C) FL70

D) FL5012257. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual Instrument approach charts forZURICH (10-2,10-2A,10-2B) or figures AP-21, AP-22 andAP-23)Aeroplane arriving via route BLM 2Z only, should proceedvia which route to EKRON int?A) TRA R247 outbound to EKRON int.B) WIL R018 outbound to EKRON int.C) HOC R067 via GOLKE to EKRON int.#D) BLM R111 to GOLKE int then TRA R-247 inbound to EKRONint.12258. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Route Manual STAR chart for LONDON HEATHROW(10-2D) or figure AP-25)The minimum holding altitude (MHA) and maximum holdingspeed (IAS) at MHA at OCKHAM OCK 115,3 are:A) 7.000 ft and 250 kts.B) 9.000 ft and 250 kts.#C) 7.000 ft and 220 kts.D) 9.000 ft and 220 kts.12273. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (HI)5 CAA-Edition or figureHI-37)Of the following, the preferred airways routing from MARTIGUESMTG 117,3 (43°23N 005°05E) to ST PREX SPR

113,9 (46°28N 006°27E) above FL245 is:A) UA6 LSA UG52.#B) UB282 DGN UB46.C) UB284 VILAR UB28.D) UB28.12274. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-31)Of the following, the preferred airways routing from CLACTONCLN 114,55 (51°51N 001°09E) to DINARD DIN 114,3



(48°35N 002°05W) above FL245 is:A) UR12 MID UR8 SAM UB11 BARLU UW115.B) UB29 LAM UR1 MID UA34 LILAN UR9.#C) UB29 LAM UR1 ORTAC UR14.D) UR12 MID UA47 DPE UA475 SOKMU UH111.12275. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-32)The magnetic course/distance from DINKELSBUHL DKB117,8 (49°09N 010°14E) to ERLANGEN ERL 114,9 (49°39N011°09E) on airway UR11 is:#A) 050° / 47 NM.B) 230° / 97 NM.C) 133° / 85 NM.D) 052° / 97 NM.12276. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (LO)6 or figure LO-14)The magnetic course/distance from GROSTENQUIN GTQ111,25 (49°00N 006°43E) to LINNA (49°41N 006°15E) onairway R7 is:A) 337° / 31 NM.B) 337° / 58 NM.#C) 337° / 46 NM.D) 157° / 58 NM.

12277. (AIR: atpl, ir; HELI: atpl, ir)(Refer toRoute Manual chart E(LO)5) or figure LO-15)The magnetic course/distance from ELBE LBE 115,1(53°39N 009°36E) to LUNUD (54°50N 009°19E) on airwayH12 is:#A) 352° / 72 NM.B) 352° / 96 NM.C) 339° / 80 NM.D) 339° / 125 NM.12278. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (LO)2 or figure LO-13)The magnetic course/distance from CAMBRAI CMB 112,6(50°14N 003°09E) to TALUN (49°33N 003°25E) on airway

B3 is:A) 349° / 42 NM.#B) 169° / 42 NM.C) 349° / 26 NM.D) 169° / 68 NM.12279. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-34)The magnetic course/distance from TRENT TNT 115,7(53°03N 001°40W) to WALLASEY WAL 114,1 (53°23N003°08W) on airway UR3 is:A) 297° / 70 NM.B) 117° / 71 NM.

#C) 297° / 57 NM.D) 117° / 57 NM.12280. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-32)The magnetic course/distance from TANGO TGO 112,5(48°37N 009°16E) to DINKELSBUHL DKB 117,8 (49°09N010°14E) on airway UR11 is:#A) 052° / 50 NM.B) 007° / 60 NM.



C) 105° / 105 NM.D) 132° / 43 NM.12281. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(HI)5 CAA-Edition or figureHI-35)The magnetic course/distance from ELBA ELB 114,7(42°44N 010°24E) to SPEZI (43°49N 009°34E) on airwayUA35 is:#A) 332° / 76 NM.B) 152° / 42 NM.C) 322° / 60 NM.D) 332° / 118 NM.

033-04 IFR (AIRWAYS) FLIGHT PLANNING36© 2008AVIATIONEXAM.com12282 (C) 12283 (D) 12284 (A) 12285 (A) 12286 (C) 12292 (B) 14367 (C) 23737 (D)23738 (C) 23769 (C) 23770 (C) 23771 (D) 23772 (A)12282. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E(LO)5 or figure LO-05)The VOR and TACAN on airway G9 at OSNABRUCK (52°12N008°17E) are:A) NOT frequency paired, and have the same identifier.

B) frequency paired, and have the same identifier.#C) NOT frequency paired, and have different identifiers.D) frequency paired, and have different identifiers.12283. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart E (HI)4 CAA-Edition or figureHI-33)Aeroplanes intending to use airway UR14 should crossGIBSO intersection (50°45N 002°30W) at or above:A) FL140B) FL160C) FL200#D) FL25012284. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Route Manual SID chart for ZURICH (10-3) or figureAP-20)Which is the correct ALBIX departure via AARAU for runway16?#A) ALBIX 7S.B) ALBIX 7A.C) ALBIX 6H.D) ALBIX 6E.12285. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart AMSTERDAM JAA MINIMUMS(10-9X) or figure AP-26)The Radio Altimeter minimum altitude for a CAT II ILS DMEapproach to RWY 01L is:

#A) 100 ftB) 88 ftC) 300 ftD) 188 ft12286. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart PARIS CHARLES DE GAULLEILS Rwy 27 (21-2) or figure AP-24)The crossing altitude and descent instruction for a propelleraircraft at COULOMMIERS (CLM) are:A) cross at FL80 descend to FL70.



B) cross at FL60 and maintain.#C) cross at FL60 descend to 4.000 ft.D) cross at FL70 descend to 4.000 ft.12292. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-75)The maximum wind velocity (°/kts) shown in the vicinity ofMUNICH (48°N 012°E) is:A) 290/110#B) 300/140C) 300/100D) 300/16014367. (AIR: atpl, ir; HELI: atpl, ir)The Final Reserve Fuel for aircraft with reciprocating enginesshould be:A) fuel to fly for 30 minutes.B) fuel to fly for 60 minutes.#C) fuel to fly for 45 minutes.D) 5 minutes fuel at the holding speed at 1.500 ft above theaerodrome in standard conditions.23737. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(LO)5 or figure LO-03)The NDB at DENKO (52°49N 015°50E) can be identifiedon:A) channel 440, BFO on.

B) channel 440, BFO off.C) frequency 440 kHz, BFO off.#D) frequency 440 kHz, BFO on.23738. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual Munich STAR charts for MUNICH10-2A,B or figures AP-17, AP-18 and AP-19)The correct arrival route and Initial Approach Fix (IAF) foran arrival from the west via TANGO for runway 08 L/R is:A) NDG 1T, IAF ROKIL.B) DKB 1T, IAF ROKIL.#C) AALEN 1T, IAF ROKIL.D) AALEN 1T, IAF MBG.23769. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Jeppesen Student Route Manual chart NAP)On a direct great circle course from REYKJAVIK (64°10N020°00W) to AMSTERDAM (52°32N 004°50E), the averagetrue course and distance are:A) 118°, 1.095 NM.B) 311°, 1.824 NM.#C) 131°, 1.095 NM.D) 140°, 1.824 NM.23770. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)An appropriate flight level for flight on airway A2 from TALLA113,8 TLA (55°30N 003°21W) to DEAN CROSS 115,2DCS (54°43N 003°20W) is:

A) FL100B) FL80#C) FL90D) FL5023771. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)The distance on airway B4 from POLE HILL 112,1 POL(53°45N 002°06W) to SHAPP (54°30N 002°38W) is:A) 30 NMB) 31 NM



C) 51 NM#D) 49 NM23772. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)The magnetic course from DEAN CROSS 115,2 DCS (54°43N003°20W) to NEWCASTLE 114,25 NEW (55°02N 001°41W)on airway W911D is:#A) 077°B) 083°C) 257°D) 263°

033-04 IFR (AIRWAYS) FLIGHT PLANNING37© 2008AVIATIONEXAM.com23773 (B) 23774 (D) 23775 (A) 23777 (A) 23778 (D) 23779 (A) 23780 (D) 23781 (D)23782 (D) 23783 (D) 23784 (D) 23785 (B)23773. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)The magnetic course/distance from TALLA 113,8 TLA(55°30N 003°21W) to DEAN CROSS 115,2 DCS (54°43N003°20W) on airway A2 is:A) 185° / 18 NM.

#B) 185° / 47 NM.C) 005° / 47 NM.D) 005° / 18 NM.23774. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)The minimum enroute altitude (MEA) that can be maintainedcontinuously on advisory route W911D from NEWCASTLE114,25 NEW (55°02N 001°24W) to DEAN CROSS 115,2 DCS(54°43N 003°20W) is:A) 4.520 ftB) FL150C) 4.700 ft#D) FL50

23775. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)The minimum enroute altitude (MEA) that can be maintainedcontinuously on airway B226 from TALLA 113,8TLA (55°30N 003°21W) to reporting point ANGUS (56°42N003°03W) is:#A) FL70B) FL80C) 5.000 ftD) 5.500 ft23777. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)The radio navigation aid at LEEDS BRADFORD (53°52N

001°39W) is:#A) an NDB, frequency 402,5 kHz, NOT continuous operation.B) a TACAN, channel 402,5.C) a fan marker, frequency 402,5 kHz.D) an NDB, frequency 402,5 kHz, continuous operation.23778. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)The radio navigation aid at ST. ABBS (55°55N 002°12W)is:A) a VOR only, frequency 112,5 MHz.



B) an NDB, frequency 112,5 MHz.C) a TACAN, channel 112,5.#D) a VOR/DME, frequency 112,5 MHz.23779. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)What is the Minimum Enroute Altitude (MEA) on airwayW911D from DEAN CROSS 115,2 DCS (54°43N 003°20W)to NEWCASTLE 114,25 NEW (55°02N 001°41W)?#A) FL50B) FL150C) 4.700 ftD) 4.200 ft23780. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)The magnetic course / distance from DEAN CROSS 115,2DCS (54°43N 003°20W) to POLE HILL 112,1 POL (53°45N002°06W) on airway A2 is:A) 329° / 53 NM.B) 143° / 53 NM.C) 155° / 73 NM.#D) 149° / 73 NM.23781. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(LO)1)What is the Maximum Authorised Altitude (MMA) on airway

W911D from DEAN CROSS 115,2 DCS (54°43N 003°20W) toNEWCASTLE 114,25 NEW (55°02N 001°41W)?A) 4.200 ftB) FL50C) 4.700 ft#D) FL15023782. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)The initial magnetic course from INVERNESS 109.2 INS(57°32N 004°03W) direct to TIREE 117,7 TIR (59°30N006°53W) is:A) 230°B) 237°

C) 218°#D) 244°23783. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)The initial magnetic course from TIREE 117,7 TIR (59°30N006°53W) direct to INVERNESS 109,2 INS (57°32N004°03W) is:A) 236°B) 056°C) 048°#D) 064°23784. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)

The initial magnetic course from TIREE 117,7 TIR (59°30N006°53W) direct to STORNOWAY 115,1 STN (58°12N006°11W) is:A) 003°B) 192°C) 011°#D) 019°23785. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)The initial true course from INVERNESS 109,2 INS (57°32N



004°03W) direct to TIREE 117,7 TIR (59°30N 006°53W) is:A) 244°#B) 237°C) 218°D) 230°

033-04 IFR (AIRWAYS) FLIGHT PLANNING38© 2008AVIATIONEXAM.com23786 (B) 23787 (B) 23788 (B) 23798 (C) 23799 (B) 23800 (D) 23801 (C) 23856 (C)23857 (A) 23858 (D) 23859 (C) 23860 (D)23786. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)The initial true course from TIREE 117,7 TIR (59°30N006°53W) direct to INVERNESS 109,2 INS (57°32N004°03W) is:A) 062°#B) 054°C) 048°D) 236°23787. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)The initial true course from TIREE 117,7 TIR (59°30N

006°53W) direct to STORNOWAY 115,1 STN (58°12N006°11W) is:A) 192°#B) 011°C) 019°D) 003°23788. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)The direct distance from TIREE 117.7 TIR (59°30N006°53W)to INVERNESS 109.2 INS (57°32N004°03W) is:A) 204 NM#B) 112 NMC) 192 NM

D) 360 km23798. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - TRM, Esbjerg Aerodromechart (19-2) or figure AP-32)What are the dimensions of runway 08/36 at Esbjerg?A) 8.530 ft x 45 ft.B) 8.530 m x 45 m.#C) 2.600 m x 45 m.D) 2.600 ft x 148 ft.23799. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - TRM, Esbjerg Aerodromechart (19-2) or figure AP-32)What is the position of the aerodrome reference point at

ESBJERG?A) 55°31,6N 008°33,1W#B) 55°31,6N 008°33,1EC) 55°32,2N 008°34,9ED) 55°32,2N 008°34,9W23800. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - TRM, Esbjerg Areachart (19-1) or figure AP-33)What is the course and distance from Locator HP to thethreshold of Runway 08?







What is the magnetic track and distance for this flight?A) 007° / 131 NM.B) 029° / 69 NM.C) 013° / 117 NM.#D) 018° / 129 NM.23868. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft has to fly from Aalborg (57°06N 010°00E) toBottna (57°45N 013°48E) on airway UR46. What is thetrack distance for this flight?A) 260 NMB) 70 NM#C) 130 NMD) 60 NM23869. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft has to fly on airways from ODIN (55°35N010°39E) to BOTTNA (57°45N 013°48E). Which of the followingis an acceptable route for this flight?#A) ODN UR156 SKA UH42 BTD.B) ODN UR12 PER UG5 SHG UH42 BTD.C) ODN UR156 LAV D17 CINDY UR46 BTD.D) ODN UR12/UN872 HIL UV30 BTD.23870. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft has to fly on airways from SKARA (58°23N013°15E) to SVEDA (56°10N 012°34E). Which of the followingis an acceptable route for this flight?A) SKA UR156 LAV UB45 SVD.B) SKA UB44 BAK UA9 PAPER UH40 SVD.#C) SKA UH42 BTD UV30 HIL UR1 SVD.D) SKA DCT SVD.23871. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft is flying from BACKA (57°33N 011°59E) toBOTTNA (57°45N 013°48E) on airway UR46. Which of thefollowing would be a useful cross-reference to check the

airway intersection CINDY?A) BAK078/BTD258#B) HAR161/LAV092C) LAV D17D) BTD D6023872. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)What is the meaning of the chart information for thebeacon(s) at position 55°59N 014°06E?A) NDB, ident OE and VOR, ident VEY.#B) NDB only, ident OE.C) VOR only, ident VEY.D) Doppler VOR, ident SUP and NDB, ident OE.

23873. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft has to fly from ALMA (55°25N 013°34E) to PETER(56°50N 013°35E). Excluding RVSM, what is the lowestflight level above FL400 that can be flown on an IFRflight on this leg?#A) FL430B) FL410C) FL420D) FL440



033-04 IFR (AIRWAYS) FLIGHT PLANNING40© 2008AVIATIONEXAM.com23874 (B) 23875 (B) 23876 (B) 23877 (B) 23878 (A) 23880 (D) 23881 (B) 23882 (C)23883 (D) 23884 (D) 23885 (D) 23886 (D) 23887 (D)23874. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft has to fly from ODIN (55°35N 010°39E) to LANDVETTER(57°39N 012°17E). What is the magnetic courseon this route?A) 204°#B) 024°C) 052°D) 156°23875. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft has to fly from SHILLING (57°33N 014°00E) toALMA (55°25N 013°34E). What is the minimum grid safealtitude for this route?A) 2.700 ft#B) 3.200 ftC) 2.500 ft

D) 2.900 ft23876. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft has to fly on airways from ALMA (55°25N013°34E) to SHILLING (57°33N 014°00E). What is the distancebetween these two points?A) 86 NM#B) 131NMC) 45 NMD) 60 NM23877. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)An aircraft has to fly on airways from SVEDA (56°10N

012°34E) to SKARA (58°23N 013°15E). Which of the followingis the correct route?A) SVD UB45 LAV UR156 SKA.#B) SVD UH40 PAPER UA9 BAK UB44 SKA.C) UR1 HIL UV30 BTD UH42 SKA.D) SVD UH40 PAPER UA9 BAK UR156 SKA.23878. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)2)What is the meaning of the chart information for thenavaid(s) LANDVETTER (57°39N 012°17E)?##A) VORDME with identification LAV available on frequency114,6 MHz.B) DME only with identification LAV available on frequency

114,6 MHz.C) Doppler VOR only with identification LAV available on frequency114,6 MHz.D) VORDME and NDB with identification LAV available onfrequency 114,6 MHz.23880. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)The radio navigation aid(s) at (57°32N 004°03W) is/are:A) VORDME, frequency 109,2 kHz.B) VOR, frequency 109,2 MHz, for INS update only.





24745. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual, London Heathrow,pages 10-2, 11-4 or figures AP-08, AP-09)Using STAR Biggin Two Alfa for ILS DME RWY 27R, What isthe Initial Approach Fix?A) Epsom, 316.#B) Biggin, 115,1.C) IRR, 110,3.D) Ockham, 115,3.24747. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual chart 5AT(HI)Route PTS P from VIGRA (62°33N 006°02E) to ADOBI(68°30N 003°00E). What is the grid track?A) 353°#B) 344°C) 173°D) 349°24749. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(HI)4)What is the mean true course from Paris Charles de Gaulleto London Heathrow?#A) 321° (T)B) 312° (T)C) 322° (M)

D) 142° (T)24750. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MADRID, BARAJASpage 11-1 or figure AP-15)ILS DME RWY 33. What is the minimum altitude forglideslope interception?A) 3.500 ft#B) 4.000 ftC) 2.067 ftD) 1.567 ft24753. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - Paris Charles deGaulle - SID chart 20-3 or figure AP-03)

What is the distance to Abbeville on SID ABB 8 A?A) 72 NMB) 74 NMC) 72,5 NM#D) 74,5 NM24757. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - AMSTERDAM SCHIPOL11-6 or figure AP-07)ILS DME RWY 22. Complete the blanks for the missed approach:Turn ___ on track ___° climbing to ___.A) left; 005; 2.000 ft (2.012 ft)B) left; 266; 2.000 ft (2.102 ft)C) right; 240; 2.000 ft (2.011 ft)

#D) left; 160; 2.000 ft (2.014 ft)24846. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(HI)3)Are the VOR and TACAN navaids at OSNABRUCH (52°12N008°17E) co-located?A) Yes.B) VOR/DME only.C) VOR/NDB only.#D) No.24847. (AIR: atpl, ir; HELI: atpl, ir)



(Refer to Jeppesen Manual chart E(HI)4)For a flight from Paris Charles de Gaulle to London Heathrow,what is the average true course?#A) 320°B) 300°C) 120°D) 140°24848. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(LO)5)OSNABRUCH VOR and TACAN (52°12N 008°17E). Whatcan be said about the VOR and TACAN?A) They are frequency paired.B) They are not frequency paired.C) They are frequency paired and have the same ident.#D) They are not frequency paired and have different idents.24852. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart 5 AT(HI)The initial true course from A (65°N 006°E) to C (62°N 020°W)is:A) 272°#B) 266°C) 256°D) 246°24889. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Jeppesen Manual chart E (LO) 5)This chart is a ___ projection with a scale of ___ .#A) Lambert Conformal Conic; 1 cm = 14,60 kmB) transverse Mercator; 1 inch = 15 NMC) Mercator; 1 inch = 20 NMD) Lambert Conformal Conic; 1cm = 10,95 km24891. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 6)Position NESLA at (49°48,6N 002°44,4E) is a ___.A) compulsory reporting point on both G40 and A5B) non-compulsory reporting point on both G40 and A5#C) compulsory reporting point G40 onlyD) non-compulsory reporting point on G40 only

24892. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 5)On what frequency could you expect to receive plain languagein-flight weather information for Amsterdam?A) 123,70 MHz#B) 126,20 MHzC) 113,95 MHzD) 124,30 MHz

033-04 IFR (AIRWAYS) FLIGHT PLANNING42© 2008AVIATIONEXAM.com

24894 (A) 24895 (D) 24897 (D) 24899 (D) 24900 (C) 24901 (D) 24903 (B) 24916 (D)25013 (A) 25014 (B) 25015 (C)24894. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 6)While flying IFR on A5 between PERON (49°54,8N002°50,4E) and CAMBRAI (50°13,7N 003°09,1E) the highestsuitable ICAO cruising level would be?#A) FL120B) FL150C) FL180



D) FL19024895. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E(LO) 6)You plan to fly at FL180 from DRESDEN (51°00,9N 013°35,9E)to BAROM (50°02,5N 010°43,9E) when ED(R)-208 is active,your expected routing is:A) DRN Z715 BAROM.B) DRN Z715 DCT BAROM.C) as directed by ATC.#D) DRN A19 BAROM.24897. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 5)Flying westbound overhead DOXON (55°26,9N 018°10,0E)you fly from ___ into ___.A) Warsaw FIR (ICAO code EPWW); Riga FIR (ICAO codeEVRR)B) Latvia; PolandC) Riga FIR (ICAO code EVRR); Malmo FIR (ICAO codeESMM)#D) Riga FIR (ICAO code EVRR); Warsaw FIR (ICAO codeEPWW)24899. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 5)To positively identify the DENKO (52°49,0N 015°50,1E)

NDB you must ensure the following radio/navigation equipmentis on:A) the ADF with the Beat Frequency Oscillator (BFO) off.B) the VOR/DME.C) radio tuned to 134,22 MHz.#D) the ADF with the Beat Frequency Oscillator (BFO) on.24900. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 6)Overhead STRASBOURG (48°30,4N 007°34,4E) the GridMORA is?A) FL57B) 5.500 ft#C) 5.700 ft

D) 5.700 m24901. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 6)Overhead PRAGUE (50°05,8N 014°15,8E) you should expectto communicate with Prague Control/Radar on:A) 112,60 MHzB) 127,90 MHzC) 120,47MHz#D) 134,00 MHZ24903. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (LO) 5)You are flying along R12 on track, heading 030° (M) towardsHELGOLAND (54°11,1N 007°54,6E) and you have 30 NM to

run, your RMI indicates a QDM of ___ to HELGOLAND.A) 030°#B) 045°C) 225°D) 054°24916. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (HI) 4)Your aircraft registered in the UK is outbound from Londontowards New York via UG1 and Shanwick CTA/FIR, prior tocrossing W002 what should you have obtained:



A) airways clearance from London on 133,60 MHz.B) oceanic entry clearance on 133,80 MHz.C) oceanic entry clearance on123,95 MHz.#D) oceanic entry clearance on 127,65 MHz.25013. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (HI) 4)You are cleared to route LANDS END (50°08,1N 005°38,2W)direct to HONILY (52°21,4N 001°39,7W) you estimateLANDS END at 09:57.TAS is 500 ktsW/V is 270° (M)/50 ktsWhat is your mean magnetic track and estimate for HONILY:#A) 055°, 1019.B) 048°, 1019.C) 053°, 1005.D) 048°, 1021.25014. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - LONDON AREAchart)You are required to hold at BOVINGDON (51°43,6N000°33,0W) however, the VOR is unserviceable. What procedureshould now follow?A) Enter the BOVVA alternate hold which is on the 141° radialat 37 DME BIGGIN.

#B) Enter the BOVVA alternate hold which STARTS AT 32DME BIGGIN on 141° QDM.C) Enter the BOVVA alternate hold which starts at 37 DMEBIGGIN on 141° QDM.D) Ask ATC for radar vectors instead.25015. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (HI) 4)What navigation aids are available at CLACTON (51°50,9N001°09,0E)?A) VOR/DME and NDB always.B) NDB only.#C) VOR/DME and NDB only when the VOR/DME is unserviceable.D) VOR/DME when the NDB is unserviceable.

033-04 IFR (AIRWAYS) FLIGHT PLANNING43© 2008AVIATIONEXAM.com25017 (B) 25019 (B) 25020 (D) 25022 (D) 25026 (C) 25028 (D) 25029 (A) 25031 (B)25033 (D) 25035 (A) 25036 (C) 25037 (D)25017. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (HI) 4)Regarding restricted airspace EG (D)-056 at (50°05N000°50W) it is a:A) permanently active danger area from sea level up toFL550.

#B) danger area from sea level up to 55.000 ft activated byNOTAM.C) restricted area from sea level up to 55.000 ft activated byNOTAM.D) permanently active danger area from sea level up to55.000 ft.25019. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (HI) 4)How could you confirm your position at SKESO (49°49,5N003°02,0W) if BHD is unserviceable?



A) 339° QDR at 122 DME DIN.#B) 331° QDR at 29 DME GUR.C) 339° QDM at 122 DME DIN.D) 331° QDM at 29 DME GUR.25020. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (HI) 4)The initial magnetic track and total distance from ROLAMPONT(47°54,4N 005°15,0E) to MONUR (49°51,6N002°47,3E) along UB4 are:A) 322° and 99 NM.B) 328° and 53 NM.C) 321° and 69 NM.#D) 322° and 152 NM.25022. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual chart E (HI) 5)Flying eastbound between BOLOGNA (44°32,2N 011°17,5E)and ANCONA (43°35,2N 013°28,3E) what is the minimumICAO IFR cruising level?A) FL250B) FL310C) FL260#D) FL33025026. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MADRID BARAJAS

10-3H or figure AP-34)You are cleared on a NAVAS THREE DELTA departure, afterpassing ARGAS what is the maximum IAS in the turn toNVS and at what level should you be by NVS:A) 230 kts, 4.000 ft.B) 250 kts, 4.000 ft.#C) 230 kts, FL80 or above.D) 250 kts, FL80 or above.25028. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E (LO) 5)The solid green symbol 10 NM south west of EELDE(53°09,8N 006°40,0E) is:A) a VOR/DME with a Morse ident of EEL.

B) an NDB with a Morse ident of VZ.C) a fan marker with a Morse ident of VZ.#D) a fan marker with a Morse ident of DN.25029. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MUNICH 10-2B or figureAP-19)Standard arrival AALEN ONE TANGO with runway 26R inuse, therefore your route and track miles to the IAF are expectedto be:#A) AALEN - WLD - ROKIL - MBG, 90 NM.B) AALEN - WLD - ROKIL, 51 NM.C) AALEN - WLD - ROKIL, 124 NM.D) WLD - ROKIL, 10 NM.

25031. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - ZURICH 11-2 or figureAP-11)The MSA is based on the ___ and is ___ to the southeast ofthe reference point.A) aerodrome reference point; 8.600 ft#B) KLOTEN VOR; 8.600 ftC) aerodrome reference point; 5.300 ftD) KLOTEN VOR; 4.400 ft25033. (AIR: atpl, ir; HELI: atpl, ir)



(Refer to Jeppesen Student Manual - AMSTERDAM SCHIPOL11-3A or figure AP-36)The touchdown elevation for runway 27 is:A) 12 ft above mean sea level.B) 11 ft above mean sea level.C) 11 ft below mean sea level.#D) 12 ft below mean sea level.25035. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - LONDON 11-4 or figureAP-09)The frequency, identification and localiser final approachQDM for runway 27R are:#A) 110,3 MHz, IRR, 274°.B) 109,5 MHz, ILL, 274°.C) 110,3 MHz, IRR, 094°.D) 113,6 MHZ, LON, 094°.25036. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - charts E (LO) 5and 6)It is August and you are flying overhead Latvia at 0200 Latviastandard time. What is the correct UTC time?A) 0500 hrs.B) 1400 hrs.#C) 2300 hrs.

D) 2400 hrs.25037. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MADRID BARAJAS11-1 or figure AP-15)The final approach fix is ___ from the runway 33 displacedthreshold.A) D1,1B) D10,7C) D7,1#D) D4,7

033-04 IFR (AIRWAYS) FLIGHT PLANNING44

© 2008AVIATIONEXAM.com25038 (A) 25039 (C) 25059 (C) 25061 (C) 25065 (B) 25071 (A) 25073 (A) 25074 (B)25096 (B) 25097 (C) 25098 (B) 25099 (C)25038. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - AMSTERDAM SCHIPOL13-5 or figure AP-37)When carrying out the procedure turn in a category A aeroplanewhat outbound QDR should you fly:#A) 122°B) 140°C) 266°D) 091°

25039. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MUNICH 11-4 or figureAP-01)If the glidescope was out while carrying out an ILS approachto runway 26R when 4,0 DME your recommendedaltitude is:A) 1.001 ftB) 2.660 ft#C) 2.450 ftD) 1.211 ft



25059. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E (HI) 4)You are flying overhead TANGO (48°37,2N 009°15,6E) at0947 maintaining TAS of 480 kts experiencing a 50 kts headwindcomponent while routing UG313 KPT UG60 BRENOUA12 BZO. Your estimate for the LOVV/LIMM FIR boundaryis?A) 0958 hrs.B) 0956 hrs.#C) 1005 hrs.D) 1015 hrs.25061. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E (LO) 5)The airspace ED (R)-74 centered on 52°25N 011°30E isusually active:A) from ground to 39.000 ft AMSL, Monday 0700 to Friday1800 UTC.B) from MSL to FL39, Monday to Friday 0700 - 1800 LT.#C) from ground to 3.900 ft AMSL, Monday 0700 to Friday1800 LT.D) activated only by NOTAM.25065. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figure 033-76)Flying north bound just out of Moscow at FL120. What sort

of in-flight weather hazard might be encountered?A) None.#B) Moderate icing and turbulence.C) Moderate icing and severe turbulence.D) Severe icing and moderate turbulence.25071. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart (LO) 5)Regarding airway G5 between HAMBURG (53°41,1N010°12,3E) and GEDSER (54°37,1N 011°56,0E) it is true tosay:#A) the total distance is 82 NM, FL180 is a suitable IFR level.B) the total distance is 82 NM, FL170 is a suitable IFR level.C) the total distance is 60 NM, FL180 is a suitable IFR level.

D) the total distance is 60 NM, FL170 is a suitable IFR level.25073. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E (HI) 5)Who should you make your position report to on passingLYON (45°43,5N 005°05,4E) if you are maintaining FL350northwest bound along UA2:#A) Marseille control on 132,25 MHz.B) Marseille control on 133,42 MHz.C) Marseille control on 134,10 MHz.D) Marseille control on 125,85 MHz.25074. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E (LO) 6)The symbol at BOULOGNE (50°37,5N 001°54,5E) has the

meaning:A) VOR/DME ON 113,80 MHz and a compulsory point.#B) VOR on 113,80 MHz and a compulsory reporting point.C) VOR on 113,80 MHz and on request reporting point.D) a compulsory reporting point with no associated navigationaid.25096. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E(HI)4 )To the east of Koksy (51°06N 002°39E):A) airway UJ 34 is available not below FL300.



#B) a plain language inflight weather service is available on127,8 MHz.C) maastricht Control/Radar is the Control Service for usewithin the portrayed boundaries below FL245.D) brussels Control is the Control Service for use within theportrayed boundaries at FL245 and above.25097. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E(LO)1 )The altimeter setting to be used is:A) QNE.B) QNH until above transition level thereafter QNE.#C) QNH until above transition altitude thereafter QNE.D) QNE until below transition altitude thereafter QNH.25098. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E(HI)4 )Airway UL3 at GIBSO intersection (50°45N 002°30W):A) is available eastbound only.#B) is available at 1000LT on a public holiday.C) is available westbound to Gibso routing thereafter viaUR14 below FL245.D) is a Diversionary Route only.25099. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MADRID BARAJAS(10-2B) or figure AP-13)

The IAF for runway 33 arrivals from Airway A869 is:A) CJN.B) ADUXO.#C) a frequency paired VOR and DME.D) CJN and a frequency paired VOR and DME.

033-04 IFR (AIRWAYS) FLIGHT PLANNING45© 2008AVIATIONEXAM.com25100 (B) 25101 (B) 25106 (B) 25107 (B) 25108 (C) 25109 (D) 25110 (C) 25111 (A)25112 (A) 25113 (D) 25114 (D) 25115 (C)25100. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Jeppesen Student Manual - Munich SID (10-3D) orfigure AP-10)Pilots departing Munich via a KPT 5S departure:A) when airborne should contact Munich Departure on127,95.#B) should climb to FL70.C) may climb to FL110.D) should remain below transition altitude 5.000 feet until otherwiseinstructed by ATC.25101. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - Paris Charles-de-Gaulle - STAR chart (20-2) or figure AP-04)Turboprop aircraft arriving via Chievres should expect:

A) a CIV 1P arrival crossing the IAF at FL110.#B) a CIV 1P arrival crossing the IAF at FL60.C) a CIV 1W arrival crossing the IAF at FL110.D) a CIV 1W arrival crossing the IAF at FL80.25106. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart E(HI)4)An appropriate flight level for flight on airway UR 106 fromRambouillet (48°39,2N 001°59,7E) is:A) FL310#B) FL290



C) FL300D) FL32025107. (AIR: atpl, ir; HELI: atpl, ir)An appropriate flight level for IFR flight in accordance withsemi-circular height rules on a course of 360° (M) is:A) FL200#B) FL210C) FL220D) FL24025108. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MUNICH ILS Rwy 26R(11-4) or figure AP-01)The height of the aircraft at the Final Approach Fix (FAF) forthe ILS runway 26R is:A) 1.649 feetB) 1.850 feet#C) 3.551 feetD) 5.000 feet25109. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MUNICH ILS Rwy 26R(11-4) or figure AP-01)DMN is a:A) NDB facility.B) ILS facility with paired DME reading zero NM at runway

threshold.C) VOR facility with paired DME reading zero NM at runwaythreshold.#D) DME facility reading 1 NM at runway threshold.25110. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - AMSTERDAM SCHIPOLILS/DME Rwy 22 (11-6) or figure AP-07)The intermediate fix is shown at:A) D6,0 SPL VOR.B) D6,2 SCH ILS.#C) D9,9 SPL VOR.D) D11,7 SPL VOR.25111. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Jeppesen Student Manual - LONDON HEATHROWILS DME Rwy 09R (11-1A) or figure AP-39)The height indicated by the radio altimeter at DA for a CATII equipped aircraft is:#A) 100 ftB) 175 ftC) 150 ftD) 225 ft25112. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - Munich NDB DME RW26L (16-3) or figure AP-02)The frequency and identifier of the NDB for the publishedapproach are:

#A) 400 MSW.B) 338 MNW.C) 108,6 DMS.D) 112,3 MUN.25113. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - Munich NDB DME RW26L (16-3) or figure AP-02)The missed approach procedure should be executed at orbefore:A) 0,5 NM from runway 26L threshold.



B) 1,5 NM from runway 26L threshold.C) D1,5 DMS.#D) 0,5 NM from runway 26L threshold and D1,5 DMS.25114. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MUNICH ILS Rwy 08R(11-2) or figure AP-35)The lowest published authorised RVR for an ILS approach,glide slope out, all other aids serviceable, aeroplane categoryA, is:A) 1.500 mB) 600 mC) 800 m#D) 720 m25115. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - MUNICH ILS Rwy 08R(11-2) or figure AP-35)The highest Minimum Safe Altitude (MSA) providing 1.000feet clearance from obstructions within a radius of 25 NMcentered on the MNW locator is ___, while the highest portrayedterrain high point or man-made structure in the chartplanview is ___.A) 3.200 feet; 2.631 feetB) 3.200 feet; 3.700 feet#C) 3.700 feet; 2.631 feet

D) 3.700 feet; 3.200 feet033-04 IFR (AIRWAYS) FLIGHT PLANNING46© 2008AVIATIONEXAM.com25123 (C) 28319 (B) 28321 (C) 1118 (D) 1144 (A) 1147 (A) 1153 (C) 1154 (A)1177 (B) 1180 (C)25123. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Manual - chart NAP)Given an initial true heading at Shannon of 270° and a compassdeviation of +3°, the corresponding compass headingwould be:

A) 265°B) 273°#C) 275°D) 281°28319. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual E(HI)5)The magnetic course/distance from TANGO TGO 112.5(48°37N 009°16E) to DINKELSBUHL DKB 117.8 (49°09N010°14E) on airway UR11 is:A) 007°/60 NM.#B) 052°/50 NM.C) 105°/105 NM.D) 132°/43 NM.

28321. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Manual - London Heathrow, 11-1, ILSDME Rwy 09R)What is the Minimum Descent Altitude (MDA) for an ILSglide slope out?A) 275 ft.B) 405 ft.#C) 480 ft.D) 200 ft.033-04-03 General flight planning tasks



1118. (AIR: atpl, ir)An aircraft is flying at MACH 0,84 at FL330. The static airtemperature is -48 °C and the headwind component 52 kts.At 1338 UTC the controller requests the pilot to cross themeridian of 030W at 1500 UTC. Given the distance to go is570 NM, the reduced Mach Number should be:A) 0,72B) 0,78C) 0,76#D) 0,801144. (AIR: atpl, ir; HELI: atpl, ir)A public transport aeroplane with reciprocating engines isflying from PARlS to LYON. The final reserve correspondsto:#A) 45 minutes at holding speed.B) 2 hours at cruise consumption.C) 1 hour at holding speed.D) 30 minutes at holding speed.1147. (AIR: atpl, ir; HELI: atpl, ir)A turbine-engined aircraft burns fuel at 200 gals per hour(GPH) with a Fuel Density of 0,8. What is the fuel flow if FuelDensity is 0,75?#A) 213 GPHB) 208 GPH

C) 200 GPHD) 188 GPH1153. (AIR: atpl, ir; HELI: atpl, ir)Given:True course (TC) 017°W/V 340°/30 ktsTrue air speed (TAS) 420 ktsFind: Wind correction angle (WCA) and ground speed(GS):A) WCA -2°, GS 426 kts.B) WCA +2°, GS 396 kts.#C) WCA -2°, GS 396 kts.D) WCA +2°, GS 416 kts.

1154. (AIR: atpl, ir; HELI: atpl, ir)Flight planning chart for an aeroplane states, that the timeto reach the cruising level at a given gross mass is 36 minutesand the distance travelled is 157 NM (zero-wind). Whatwill be the distance travelled with an average tailwind componentof 60 kts?#A) 193 NMB) 128 NMC) 157 NMD) 228 NM1177. (AIR: atpl, ir; HELI: atpl, ir)An aeroplane flies at an airspeed of 380 kts. lt flies from Ato B and back to A. Distance AB = 480 NM. When going from

A to B, it experiences a headwind component = 60 kts. Thewind remains constant. The duration of the flight will be:A) 3 hrs 00 min#B) 2 hrs 35 minC) 2 hrs 10 minD) 2 hrs 32 min1180. (AIR: atpl, ir; HELI: atpl, ir)A multi-engined AC on IFR flight. Given:Trip fuel 65 USGContingency 5% trip



Alternate fuel including final reserve 17 USGUseable fuel at departure 93 USGAt a point halfway to destination, fuel consumed is40 USGAssuming fuel consumption is unchangedWhich of the following is correct?A) At departure Reserve Fuel was 28 USG.B) At destination required reserves remain intact.#C) Remaining fuel is insufficient to reach destination with reservesintact.D) Remaining fuel is insufficient to reach destination.

033-04 IFR (AIRWAYS) FLIGHT PLANNING47© 2008AVIATIONEXAM.com1182 (A) 1193 (A) 1199 (A) 1215 (D) 1220 (D) 1268 (C) 1281 (C) 1292 (C)2190 (A) 2191 (A) 2230 (B) 2239 (B) 2255 (D)1182. (AIR: atpl, ir; HELI: atpl, ir)The fuel burn of an aircraft turbine engine is 220 l/hrs witha fuel density of 0,80. If the density is 0,75, the fuel burnwill be:#A) 235 l/hrsB) 206 l/hrs

C) 220 l/hrsD) 176 l/hrs1193. (AIR: atpl, ir; HELI: atpl, ir)An aircraft is in cruising flight at FL095, GS 155 kts. Thepilot intends to descend at 500 ft/min to arrive overheadthe MAN VOR at 2.000 ft (QNH 1.030hPa). The TAS remainsconstant in the descent, wind is negligible, temperaturestandard. At which distance from MAN should the pilotcommence the descent?#A) 41 NMB) 48 NMC) 38 NMD) 45 NM

1199. (AIR: atpl, ir; HELI: atpl, ir)An executive pilot is to carry out a flight to a French aerodrome,spend the night there and return the next day.Where will he find the information concerning parking andlanding fees?#A) In the FAL section of the French Aeronautical InformationPublication (AIP).B) In the AGA chapter of the French Aeronautical InformationPublication (AIP).C) In the GEN chapter of the French Aeronautical InformationPublication (AIP).D) By telephoning the aerodromes local chamber of commerce,this type of information not being published.

1215. (AIR: atpl, ir; HELI: atpl, ir)Where would you find information regarding Customs andHealth facilities?A) ATCC broadcasts.B) NOTAMs.C) NAV/RAD supplements.#D) AIPs.1220. (AIR: atpl, ir; HELI: atpl, ir)Where would you find information regarding Search andRescue procedures?





#B) AIP (Air Information Publication).C) NOTAM.D) SIGMET.2255. (AIR: atpl, ir; HELI: atpl, ir)From which of the following would you expect to find facilitationinformation (FAL) regarding customs and healthformalities?A) NOTAM.B) NAV/RAD charts.C) ATCC.#D) AIP (Air Information Publication).

033-04 IFR (AIRWAYS) FLIGHT PLANNING48© 2008AVIATIONEXAM.com12240 (C) 12248 (D) 12527 (A) 12556 (B) 12557 (D) 12558 (B) 12563 (C) 12564 (D)12565 (C) 12566 (D) 12567 (B) 12568 (B)12240. (AIR: atpl, ir; HELI: atpl, ir)You are flying a constant compass heading of 252°. Variationis 22°E, deviation is 3°W and your INS is showing adrift of 9° to the right. True track is?A) 242°B) 262°

#C) 280°D) 224°12248. (AIR: atpl, ir)(Refer to figure 033-37)Planning an IFR-flight from Paris to London for the twin jetaeroplane. Given:Estimated Landing Mass: 49.700 kgFL280W/V 280°/40 ktsAverage True Course: 320°Procedure for descent: 0,74 M/250 KIASDetermine the time from the top of descent to London (elevation80 ft).

A) 10 minB) 17 minC) 8 min#D) 19 min12527. (AIR: atpl, ir; HELI: atpl, ir)(Refer to figures 033-71)True Air speed: 170 ktsWind in the area: 270° / 40 ktsAccording to the attached the navigation log, an aircraftperforms a turn overhead BULEN to reroute to ARD viaTGJ. The given wind conditions remaining constant. Thefuel consumption during the turn is 20 litres. The total fuelconsumption at position overhead ARD will be:

#A) 1.545 litresB) 1.182 litresC) 1.326 litresD) 1.600 litres12556. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-24)On a direct great circle course from Shannon (52°43N008°53W) to Gander (48°54N 054°32W), what is the averagetrue course and distance?A) 281°, 1.877 NM.



#B) 262°, 1.720 NM.C) 281°, 2.730 NM.D) 244°, 1.520 NM.12557. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart 5 AT(HI) or figure HI-25)The initial great circle true course from Keflavik (64°00N022°36W) to Vigra (62°33N 006°02E) measures 084°. On apolar enroute chart where the grid is aligned with the 000°meridian the initial grid course will be:A) 080°B) 096°C) 066°#D) 106°12558. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart 5 AT(HI) or figures HI-18_aand HI-18_b)The initial great circle course from position A (80°N 170°E)to position B (75°N 011°E) is 177° (G). The final grid courseat position B will be:A) 353° (G)#B) 177° (G)C) 194° (G)D) 172° (G)12563. (AIR: atpl, ir; HELI: atpl, ir)

(Refer to Route Manual chart NAP or figure HI-23)The average magnetic course from C (62°N 020W) to B(58°N 004E) is:A) 099°B) 118°#C) 119°D) 109°12564. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-23)The average true course from C (62°N 020W) to B (58°N004E) is:A) 119°B) 099°

C) 120°#D) 109°12565. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-23)The initial magnetic course from C (62°N 020°W) to B (58°N004°E) is:A) 098°B) 113°#C) 116°D) 080°12566. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-23)The initial true course from C (62°N 020°W) to B (58°N

004°E) is:A) 116°B) 080°C) 278°#D) 098°12567. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-23)The distance (NM) from C (62°N 020°W) to B (58°N 004°E)is:A) 775



#B) 760C) 725D) 70012568. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-23)The distance (NM) from A (64°N 006°E) to C (62°N 020°W)is:A) 1.440#B) 720C) 690D) 1.590

033-04 IFR (AIRWAYS) FLIGHT PLANNING49© 2008AVIATIONEXAM.com12569 (D) 12570 (A) 12571 (A) 23739 (A) 23863 (D) 28322 (B) 28344 (D) 28345 (B)12569. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-23)The average magnetic course from A (64°N 006°E) to C(62°N 020°W) is:A) 259°B) 247°C) 279°

#D) 271°12570. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-23)The average true course from A (64°N 006°E) to C (62°N020°W) is:#A) 259°.B) 247°.C) 271°.D) 079°.12571. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Route Manual chart NAP or figure HI-23)The initial true course from A (64°N 006°E) to C (62°N 020°W)is:

#A) 271°B) 275°C) 267°D) 246°23739. (AIR: atpl, ir)A twin-jet aeroplane carries out the WASHINGTON - PARISflight. When it reaches point K (35°N 048°W) a non-mechanicalevent makes the Captain consider rerouting to one ofthe three following fields. The flight conditions are:from K to BERMUDAS (distance 847 NM, headwind component18 kts)from K to SANTA MARIA (distance 1.112 NM, tailwind component120 kts)

from K to GANDER (distance 883 NM, wind component 0)With an aeroplane true airspeed of 460 kts, the field selectedwill be that more rapidly reached:#A) BERMUDAS, GANDER, or SANTA MARIA.B) SANTA MARIA.C) BERMUDAS.D) either GANDER or BERMUDAS.23863. (AIR: atpl, ir; HELI: atpl, ir)(Refer to Jeppesen Student Route Manual chart E(HI)1)An aircraft has to fly from the airport at Aberdeen (57°19N



002°16W) to the airport at Benbecula (57°29N 007°22W).Given:Time to climb: 11 minTime to descend: 9 minTAS: 170 ktsW/V: 230/50What is the flight time during the cruise?A) 16 minB) 47 minC) 28 min#D) 54 min28322. (AIR: atpl)LFPG ILS Rwy 09: The ILS localizer course is:A) 100°#B) 088°C) 118°D) 268°28344. (AIR: atpl, ir; HELI: atpl, ir)Which approach segment starts at the point were you reportestablished?A) Final approach.B) Initial approach.C) Go around.#D) Intermediate approach.

28345. (AIR: atpl, ir; HELI: atpl, ir)Which approach segment starts at the FAF and ends at theMAP?A) Initial approach.#B) Final approach.C) Go around.D) Intermediate approach.

033-05 JET AEROPLANES FLIGHT PLANNING50© 2008AVIATIONEXAM.com1128 (B) 1136 (D) 1140 (B) 1143 (B) 1148 (A) 1149 (C) 1151 (D) 1152 (B)

1160 (C) 1162 (D)033-05-01 Advanced flight planning aspects for jet aeroplanes1128. (AIR: atpl)What is decision point procedure? It is a procedure to reducethe amount of fuel carried on a flight by:A) reducing contingency fuel from 10% to 5% of trip fuel.#B) reducing contingency fuel to only that required from decisionpoint to destination.C) reducing trip fuel to only that required from decision aerodrometo destination.D) reducing trip distance.1136. (AIR: atpl)(Refer to figures 033-23)

Given:Brake release mass: 62.000 kgTemperature: ISA + 15 °CThe fuel required for a climb from Sea Level to FL330 is:A) 1.800 kgB) 1.650 kgC) 1.750 kg#D) 1.700 kg1140. (AIR: atpl)(Refer to figure 033-21)



The fuel required for 30 minutes holding, in a racetrack pattern,at PA 1.500 ft, at mean gross mass of 45.000 kg, is:A) 1.010 kg#B) 1.090 kgC) 1.310 kgD) 2.180 kg1143. (AIR: atpl)(Refer to figures 033-25 and 033-36)Given:Distance B - C: 350 NMCruise 300 KIAS at FL210 Temperature: - 40 °CTailwind component: 70 ktsGross mass at B: 53.200 kgThe fuel required from B - C is?A) 1.810 kg#B) 1.940 kgC) 2.800 kgD) 2.670 kg1148. (AIR: atpl)(Refer to figure 033-21)The fuel required for 45 minutes holding, in a racetrack pattern,at PA 5.000 ft, mean gross mass 47.000 kg, is:#A) 1.635 kgB) 1.090 kg

C) 1.690 kgD) 1.125 kg1149. (AIR: atpl)(Refer to figure 033-19)Given:Head wind component 50 ktsTemperature ISA + 10 °CBrake release mass 65.000 kgTrip fuel available 18.000 kgWhat is the maximum possible trip distance?A) 3.480 NMB) 3.100 NM#C) 2.740 NM

D) 2.540 NM1151. (AIR: atpl)(Refer to figure 033-15)For a flight of 2.800 ground nautical miles the following applies:Head wind component: 15 ktsTemperature: ISA + 15 °CCruise altitude: 35.000 ftLanding mass: 50.000 kgThe trip fuel and trip time respectively are:A) 20.000 kg; 7 hrs 00 min.B) 16.200 kg; 6 hrs 20 min.C) 17.000 kg; 6 hrs 10 min.#D) 17.600 kg; 6 hrs 50 min.

1152. (AIR: atpl)The Trip Fuel for a jet aeroplane to fly from the departureaerodrome to the destination aerodrome is 5.350 kg. Fuelconsumption in holding mode is 6.000 kg/hrs. The quantityof fuel which is needed to carry out one go-around and landon the alternate airfield is 4.380 kg. The destination aerodromehas a single runway. What is the minimum quantityof fuel which should be on board at takeoff?A) 13.000 kg#B) 13.230 kg



C) 14.730 kgD) 11.730 kg1160. (AIR: atpl)(Refer to figure 033-19)For a flight of 2.800 ground nautical miles the following applies:Head wind component: 20 ktsTemperature: ISA + 15 °CBrake release mass: 64.700 kgThe trip fuel and trip time respectively are:A) 16.200 kg; 6 hrs 20 min.B) 15.800 kg; 6 hrs 15 min.#C) 17.000 kg; 6 hrs 45 min.D) 18.400 kg; 7 hrs 00 min.1162. (AIR: atpl)A turbo-jet AC is enroute to an isolated destination. On topof taxi, trip and contingency fuel, what fuel is required?A) Greater of 45 mins + 15% of trip or 2 hours.B) 30 mins holding at 450 m AMSL.C) 30 mins holding at 450 m AAL.#D) 2 hours at normal cruise consumption.

033-05 JET AEROPLANES FLIGHT PLANNING51© 2008

AVIATIONEXAM.com1163 (B) 1178 (D) 1179 (B) 1184 (A) 1186 (C) 1189 (B) 1196 (B) 1197 (B)1198 (A)1163. (AIR: atpl)(Refer to figures 033-25 and 033-28)Given:Distance C-D: 680 NMLong Range Cruise at FL340Temperature Deviation from ISA: 0 °CHeadwind component: 60 ktsGross mass at C: 44.700 kgThe fuel required from C - D is:A) 3.400 kg

#B) 3.700 kgC) 3.100 kgD) 4.000 kg1178. (AIR: atpl)(Refer to figure 033-19)The following apply:Temperature ISA +15 °CBrake release mass 62.000 kgTrip time 5 hrs 20 minWhat is the trip fuel?A) 13.800 kg.B) 13.000 kg.C) 13.200 kg.

#D) 13.500 kg.1179. (AIR: atpl)Which is true regarding a balanced field?A) Provides largest gap between net and gross margins.#B) Provides minimum field length required in the case of anengine failure.C) Takeoff distance will always be more than stopping distance.D) Distances will remain equal, even if engine failure speedis changed.1184. (AIR: atpl)



(Refer to figure 033-15)For a flight of 2.400 ground nautical miles the following apply:Tail wind component: 25 ktsTemperature: ISA -10 °CCruise altitude: 31.000 ftLanding mass: 52.000 kgThe trip fuel and trip time respectively are:#A) 14.200 kg; 5 hrs 30 min.B) 16.200 kg; 5 hrs 45 min.C) 13.600 kg; 6 hrs 30 min.D) 12.000k g; 5 hrs 15 min.1186. (AIR: atpl)(Refer to figure 033-19)The following apply:Tail wind component 10 ktsTemperature ISA +10 °CBrake release mass 63.000 kgTrip fuel available 20.000 kgWhat is the maximum possible trip distance?A) 3.500 NMB) 3.640 NM#C) 3.740 NMD) 3.250 NM1189. (AIR: atpl)

(Refer to figures 033-25 and 033-35)Given:Distance B-C: 1.200 NMCruise Mach 0,78 at FL300Temperature Deviation from ISA: -14 °CTailwind component: 40 ktsGross mass at B: 50.200 kgThe fuel required from B to C is:A) 5.850 kg#B) 6.150 kgC) 7.300 kgD) 7.050 kg1196. (AIR: atpl)

(Refer to figures 033-25 and 033-36)Given:Distance C-D: 540 NMCruise 300 KIAS at FL210Temperature Deviation from ISA: +20 °CHeadwind component: 50 ktsGross mass at C: 60.000 kgThe fuel required from C to D is:A) 3.680 kg#B) 4.200 kgC) 3.350 kgD) 4.620 kg1197. (AIR: atpl)

Given:Dry operating mass (DOM): 33.510 kgLoad: 7.600 kgTrip fuel (TF): 2.040 kgFinal reserve fuel: 983 kgAlternate fuel: 1.100 kgContingency fuel: 5% of trip fuelWhich of the listed estimated masses is correct?A) Estimated takeoff mass is 45.233 kg.#B) Estimated landing mass at destination is 43.295 kg.



C) Estimated landing mass at destination is 43.193 kg.D) Estimated takeoff mass is 43.295 kg.1198. (AIR: atpl)What is the purpose of decision point procedure?#A) Carry minimum fuel to increase Traffic Load.B) Increase safety of the flight.C) Reduce landing mass to avoid stressing the aircraft.D) To assist in decision making at refuelling.

033-05 JET AEROPLANES FLIGHT PLANNING52© 2008AVIATIONEXAM.com1201 (C) 1203 (D) 1204 (D) 1206 (D) 1207 (D) 1225 (C) 2181 (A) 2251 (B)1201. (AIR: atpl)Turbo-jet AC:Taxi fuel: 600 kgFuel flow cruise: 10.000 kg/hrsFuel flow hold: 8.000 kg/hrsAlternate fuel: 10.200 kgFlight time: 6 hoursVisibility at destination: 2.000 mWhat is the minimum ramp fuel?A) 80.500 kg

B) 79.200 kg#C) 77.800 kgD) 76.100 kg1203. (AIR: atpl)Given:Maximum allowable takeoff mass: 64.400 kgMaximum landing mass: 56.200 kgMaximum zero fuel mass: 53.000 kgDry operating mass: 35.500 kgEstimated load: 14.500 kgEstimated trip fuel: 4.900kgMinimum takeoff fuel: 7.400 kgFind the maximum allowable takeoff fuel:

A) 8.600 kgB) 11.400 kgC) 14.400 kg#D) 11.100 kg1204. (AIR: atpl)Following in-flight depressurisation, a turbine poweredaeroplane is forced to divert to an enroute alternate airfield.If actual flight conditions are as forecast, the minimumquantity of fuel remaining on arrival at the airfield will be:A) at least equivalent to 45 minutes flying time.B) at least equivalent to the quantity required to fly to anotheraerodrome in the event that weather conditions sorequire.

C) laid down by the operator, with the quantity being specifiedin the operating manual.#D) at least equivalent to 30 minutes flying time.1206. (AIR: atpl)(Refer to figure 033-15)For a flight of 2.400 ground nautical miles the following apply:Temperature: ISA -10 °CCruise altitude: 29.000 ftLanding mass: 45.000 kgTrip fuel available: 16.000 kg



What is the maximum headwind component which may beaccepted?A) zeroB) 15 ktsC) 70 kts#D) 35 kts1207. (AIR: atpl)(Refer to figure 033-20)Given:Distance to Alternate: 450 NMLanding mass at Alternate: 45.000 kgTailwind component: 50 ktsThe Alternate fuel required is:A) 2.900 kgB) 2.750 kgC) 3.050 kg#D) 2.500 kg1225. (AIR: atpl)Given:Maximum allowable takeoff mass: 64.400 kgMaximum landing mass: 56.200 kgMaximum zero fuel mass: 53.000 kgDry operating mass: 35.500 kgEstimated load: 14.500 kg

Estimated trip fuel: 4.900 kgMinimum takeoff fuel: 7.400 kgFind maximum additional load:A) 7.000 kgB) 4.000 kg#C) 3.000 kgD) 5.600 kg2181. (AIR: atpl)An aeroplane has the following masses:Estimated LM: 50.000 kgTrip fuel: 4.300 kgContingency fuel: 215 kgAlternate fuel (final reserve included): 2.100kg

Taxi: 500 kgBlock fuel: 7.115 kgBefore departure the captain orders to make the block fuel9 000 kg. The trip fuel in the operational flight plan shouldread:#A) 4.300 kgB) 6.185 kgC) 9.000 kgD) 6.400 kg2251. (AIR: atpl)(Refer to figure 033-12)Find the optimum altitude for the twin jet aeroplane, given:Cruise mass: 50.000 kg

MACH 0,78A) 36.200 ft.#B) 35.500 ft.C) 36.700 ft.D) maximum operating altitude.

033-05 JET AEROPLANES FLIGHT PLANNING53© 2008AVIATIONEXAM.com





Tail wind component: 45 ktsTemperature: ISA -10 °CCruise altitude: 29.000 ftLanding mass: 55.000 kgFor a flight of 2.800 ground nautical miles, the trip fuel andtrip time respectively are:A) 16.000 kg; 6 hrs 25 min.B) 18.000 kg; 5 hrs 50 min.C) 20.000 kg; 6 hrs 40 min.#D) 17.100 kg; 6 hrs 07 min.2267. (AIR: atpl)(Refer to figure 033-20)Distance to alternate: 400 NMLanding mass at alternate: 50.000kgHeadwind component: 25 ktsThe alternate fuel required is:A) 2.550 kg#B) 2.800 kgC) 2.900 kgD) 2.650 kg2272. (AIR: atpl)The quantity of fuel which is calculated to be necessaryfor a jet aeroplane to fly IFR from departure aerodrome tothe destination aerodrome is 5.352 kg. Fuel consumption

in holding mode is 6.000 kg/hrs. Alternate fuel is 4.380 kg.Contingency should be 5% of trip fuel. What is the minimumrequired quantity of fuel which should be on boardat takeoff?A) 13.370 kgB) 14.500 kg#C) 13.000 kgD) 13.220 kg2273. (AIR: atpl)(Refer to figure 033-27)Given:LRCFL330

Temp -63 °CMass 54.100 kgTime 29 minFind the fuel consumed.A) 1.207 kgB) 1.197 kg#C) 1.100 kgD) 1.000 kg2274. (AIR: atpl)The required time for final reserve fuel for turbojet aeroplaneis:A) 45 min.#B) 30 min.

C) 60 min.D) variable with wind velocity.

033-05 JET AEROPLANES FLIGHT PLANNING54© 2008AVIATIONEXAM.com2276 (D) 2277 (A) 2280 (A) 2285 (C) 2287 (D) 2294 (B) 2295 (B) 2299 (D)2276. (AIR: atpl)(Refer to figure 033-40)



Given:Diversion distance: 650 NMDiversion pressure altitude: 16.000 ftMass at point of diversion: 57.000 kgHead wind component: 20 ktsTemperature: ISA + 15 °CThe diversion fuel required and time are approximately:A) 4.400 kg; 1 hrs 35 min.B) 3.900 kg; 1 hrs 45 min.C) 6.200 kg; 2 hrs 10 min.#D) 4.800 kg; 2 hrs 03 min.2277. (AIR: atpl)(Refer to figure 033-20)In order to find alternate fuel and time to alternate, the aeroplaneoperating manual shall be entered with:#A) distance in nautical miles (NM), wind component, landingmass at alternate.B) distance in nautical air miles (NAM), wind component,landing mass at alternate.C) distance in nautical miles (NM), wind component, zero fuelmass.D) distance in nautical miles (NM), wind component, dry operatingmass plus holding fuel.2280. (AIR: atpl)

(Refer to figures 033-25 nad 033-36)Given:Distance C-D: 540 NMCruise: 300 KIAS at FL210Temperature: ISA +2 °CHeadwind component: 50 ktsGross mass at C: 60.000 kgThe fuel required from C to D is:#A) 4.200 kgB) 4.620 kgC) 3.680 kgD) 3.350 kg2285. (AIR: atpl)

The purpose of the decision point procedure is?A) To increase the safety of the flight.B) To reduce the landing weight and thus reduce the structuralstress on the aircraft.#C) To reduce the minimum required fuel and therefore be ableto increase the traffic load.D) To increase the amount of extra fuel.2287. (AIR: atpl)When using decision point procedure, you reduce the:A) holding fuel by 30%.B) contingency fuel by adding contingency only from the burnoff between the decision airport and destination.C) reserve fuel from 10% down to 5%.

#D) contingency fuel by adding contingency only from the burnoff between decision point and destination.2294. (AIR: atpl)Planning a flight from Paris (Charles de Gaulle) to London(Heathrow) for a twin - jet aeroplane. Preplanning:Maximum Takeoff Mass: 62.800 kgMaximum Zero Fuel Mass: 51.250 kgMaximum Landing Mass: 54.900 kgMaximum Taxi Mass: 63.050 kgAssume the following preplanning results:







C) 800 kg; 24 min.D) 800 kg; 40 min.2315. (AIR: atpl)(Refer to figure 033-17)Given:Cruise M 0,78FL28050.000 kg200 NMHeadwind component 30 ktsFind the fuel required.A) 1.470 kg#B) 1.740 kgC) 1.620 kgD) 1.970 kg2316. (AIR: atpl)(Refer to figures 033-23)Given:Brake release mass: 58.000 kgTemperature: ISA + 15 °CThe fuel required to climb from an airfield at elevation 4.000ft to FL300 is:A) 1.350 kgB) 1.400 kg

C) 1.450 kg#D) 1.250 kg

033-05 JET AEROPLANES FLIGHT PLANNING56© 2008AVIATIONEXAM.com2318 (C) 2320 (A) 2321 (B) 2322 (D) 2323 (A) 2324 (A) 2331 (C) 2332 (C)2334 (D) 2336 (A)2318. (AIR: atpl)The final reserve fuel for aeroplanes with turbine enginesis:A) fuel to fly for 45 minutes at holding speed at 1.000 ft (300

m) above aerodrome elevation in standard conditions.B) fuel to fly for 45 minutes at holding speed at 1.500 ft (450m) above aerodrome elevation in standard conditions.#C) fuel to fly for 30 minutes at holding speed at 1.500 ft (450m) above aerodrome elevation in standard conditions.D) fuel to fly for 60 minutes at holding speed at 1.500 ft (450m) above aerodrome elevation in standard conditions.2320. (AIR: atpl)Which of the following statements is relevant for formingroute portions in integrated range flight planning?#A) The distance from takeoff up to the top of climb has to beknown.B) No segment shall be more than 30 minutes of flight time.

C) Each reporting point requires a new segment.D) A small change of temperature (2 °C) can divide a segment.2321. (AIR: atpl)A jet aeroplane is to fly from A to B. The minimum final reservefuel must allow for:A) 20 minutes hold over alternate airfield.#B) 30 minutes hold at 1.500 ft above destination aerodromeelevation, when no alternate is required.C) 30 minutes hold at 1.500 ft above mean sea level.D) 15 minutes hold at 1.500 ft above destination aerodrome





ISA -10 °CBrake release mass: 52.000 kgCruise at FL280What are the climb fuel and time?A) 15 min, 1.100 kg.B) 12 min, 1.100 kg.C) 10 min, 1.000 kg.#D) 11 min, 1.000 kg.2336. (AIR: atpl)(Refer to figure 033-13, 033-30, 033-31 and 033-34)Given:Estimated takeoff mass: 57.000 kgGround distance: 150 NMTemperature: ISA -10 °CCruise at Mach 0,74Find cruise altitude and expected true air speed#A) 25.000 ft, 435 kts.B) 24.000 ft, 445 kts.C) 33.500 ft, 430 kts.D) 33.900 ft, 420 kts.

033-05 JET AEROPLANES FLIGHT PLANNING57© 2008

AVIATIONEXAM.com2891 (C) 2894 (B) 4283 (C) 4284 (A) 4285 (C) 4286 (A) 4287 (A) 4288 (A)2891. (AIR: atpl)(Refer to figures 033-74)The planned flight is over a distance of 440 NM. Based onthe wind charts at altitude the following components arefound:FL50: -30 ktsFL100: -50 ktsFL180: -70 ktsThe Operations Manual in appendix details the aircraft performances.Which of the following flight levels (FL) givesthe best range performance?

A) FL050B) Either FL050 or FL100#C) FL180D) FL1002894. (AIR: atpl)(Refer to figure 033-15)For a flight of 2.000 ground nautical miles, cruising at 30.000ft, within the limits of the data given, a headwind componentof 25 kts will affect the trip time by approximately:A) +5,3%#B) +7,6%C) -3,6%D) +2,3%

4283. (AIR: atpl)(Refer to figure 033-18)Given:Ground distance to destination aerodrome: 1.600 NMHeadwind component: 50 ktsFL330Cruise Mach 0,78ISA +20 °CEstimated landing weight: 55.000 kgFind simplified flight planning to determine estimated trip



fuel and trip time.A) 12.400 kg, 04 hrs 12 min.B) 11.400 kg, 04 hrs 12 min.#C) 12.400 kg, 03 hrs 55 min.D) 11.400 kg, 03 hrs 55 min.4284. (AIR: atpl)(Refer to figure 033-29)Long Range Cruise at FL350OAT: -45 °CGross mass at the beginning of the leg: 40.000 kgGross mass at the end of the leg: 39.000 kgFind: True airspeed (TAS) and cruise distance (NAM) for atwin jet aeroplane.#A) TAS 433 kts, 227 NAM.B) TAS 423 kts, 227 NAM.C) TAS 431 kts, 1.163 NAM.D) TAS 423 kts, 936 NAM.4285. (AIR: atpl)(Refer to figure 033-21)Given:Mean gross mass: 47.000 kgThe fuel required for 45 minutes holding in a racetrack patternat 5.000 ft is:A) 1.690 kg

B) 1.090 kg#C) 1.635 kgD) 1.125 kg4286. (AIR: atpl)(Refer to figure 033-15)For a flight of 1.900 ground nautical miles the followingconditions apply:Head wind component: 10 ktsTemperature: ISA -5 °CTrip fuel available: 15.000 kgLanding mass: 50.000 kgWhat is the minimum cruise level (pressure altitude) whichmay be planned?

#A) 17.000 ftB) 10.000 ftC) 14.000 ftD) 22.000 ft4287. (AIR: atpl)(Refer to figure 033-18)Using the following information, find fuel required and triptime with simplified flight planning for twin-jet aeroplane:Ground distance to destination: 1.600 NMHeadwind component: 50 ktsFL330Cruise Mach 0,78ISA Deviation +2 °C

Landing mass: 55.000 kg#A) 12.250 kg, 04 hrs 00 min.B) 11.400 kg, 04 hrs 12 min.C) 11.600 kg, 04 hrs 15 min.D) 12.000 kg, 03 hrs 51 min.4288. (AIR: atpl)(Refer to figure 033-14)Given:Estimated zero fuel mass: 50.000 kgEstimated landing mass at alternate: 52.000 kg





Alternative fuel: 1.100 kgContingency: 5% of trip fuelA) Est landing mass at destination is 43.193 kg.#B) Est landing mass at destination is 43.295 kg.C) Est takeoff mass is 43.295 kg.D) Est takeoff mass is 45.233 kg.4298. (AIR: atpl)(Refer to figure 033-33)Find the specific range for the twin jet aeroplane flying belowthe optimum altitude (range loss = 6%) and using thefollowing data:Mach 0,74 cruiseFlight level 310Gross mass: 50.000 kgISA conditionsA) 2.807 NAM / 1.000 kg.B) 187 NAM / 1.000 kg.C) 2.994 NAM / 1.000 kg.#D) 176 NAM / 1.000 kg.4299. (AIR: atpl)(Refer to figure 033-12 and 033-65)Given:Cruise weight: 56.000 kgCruise at Mach 0,78

Cruise at FL310What is the fuel penalty?A) 0%#B) 1%C) 4%D) 10%4301. (AIR: atpl)(Refer to figure 033-22)Planning an IFR-flight from Paris (Charles de Gaulle) toLondon (Heathrow) for the twin jet aeroplane. Given:Estimated Takeoff Mass (TOM): 52.000 kgAirport elevation: 387 ftFL280

W/V 280°/40 ktsISA Deviation: -10 °CAverage True Course: 340°Find time to the top of climb (TOC).A) 12 minB) 3 min#C) 11 minD) 15 min4303. (AIR: atpl)(Refer to figure 033-20)Given for the twin jet aeroplane:Dry operating mass: 35.500 kgTraffic load: 14.500 kg

Final reserve fuel: 1.200 kgDistance to alternate: 95 NMTailwind component: 10 ktsFind fuel required and trip time to alternate with simplifiedflight planning (alternate planning):A) 800 kg, 0,4 hrs.B) 1.000 kg, 40 min.C) 800 kg, 24 min.#D) 1.000 kg, 24 min.







033-20)Planning a flight from Paris Charles-de-Gaulle (49°00,9N002°36,9W) to London Heathrow (51°29,2N 000°27,9W) fora twin-jet aeroplane. The alternate airport is Manchester(53°21,4N 002°15,7W). Preplanning:The wind from London to Manchester: 250°/30 ktsThe distance from London to Manchester: 160 NMAssume the estimated landing mass at alternate is50.000 kgFind the alternate fuel and time:A) 1.200 kg and 26 minutes.B) 1.300 kg and 28 minutes.C) 1.600 kg and 36 minutes.#D) 1.450 kg and 32 minutes.4324. (AIR: atpl)(Refer to figure 033-22)Given:Brake release mass: 57.500 kgTemperature: ISA -10 °CHead wind component: 16 ktsInitial FL280Find still air distance (NAM) and ground distance (NM) forthe climb.A) 59 NAM; 62 NM.

#B) 62 NAM; 59 NM.C) 67 NAM; 71 NM.D) 71 NAM; 67 NM.4329. (AIR: atpl)(Refer to figure 033-13)Find the short distance cruise altitude for the twin jet aeroplane.Given:Brake release mass: 40.000 kgTemperature: ISA +20 °CTrip distance: 150 Nautical Air Miles (NAM)#A) 30.000 ftB) 25.000 ftC) 21.000 ft

D) 27.500 ft4333. (AIR: atpl)(Refer to figure 033-14 and 033-27)Given for the twin jet aeroplane:Zero fuel mass: 50.000 kgLanding mass at alternate: 52.000 kgFinal reserve fuel: 2.000 kgAlternate fuel: 1.000 kgFlight to destination: Distance 720 NM, TC 030°, W/V 340°/30ktsCruise: LRC, FL330, OAT -30 °CFind: Estimated trip fuel and time with simplified flightplanning.

A) 4.750 kg, 02:00.B) 4.400 kg, 02:05.#C) 4.800 kg, 01:51.D) 4.600 kg, 02:05.4334. (AIR: atpl)(Refer to figure 033-21)Given for the twin jet aeroplane:Estimated mass on arrival at the alternate: 50.000 kgEstimated mass on arrival at the destination: 52.525 kgAlternate elevation: MSL





For flight planning purposes the landing mass at alternateis taken as:A) Landing Mass at destination plus Alternate Fuel.#B) Zero Fuel Mass plus Final Reserve Fuel.C) Zero Fuel Mass plus Final Reserve Fuel and AlternateFuel.D) Zero Fuel Mass plus Final Reserve Fuel and ContingencyFuel.4352. (AIR: atpl)(Refer to figure 033-27)Given:FL330Long range cruiseOAT: -63 °CGross mass: 50.500 kgFind true airspeed (TAS).#A) 420 ktsB) 433 ktsC) 431 ktsD) 418 kts4354. (AIR: atpl)(Refer to Route Manual chart E(HI)4 or figure HI-11 and figure033-16)Planning a flight from Paris Charles de Gaulle (49°00,9N

002°36,9E) to London Heathrow (51°29,2N 000°27,9W) fora twin-jet aeroplane. Preplanning:Powersetting: Mach 0,74Planned flight level: FL280Landing Mass in the fuel graph: 50.000 kgTrip distance used for calculation: 200 NMWind from Paris to London: 280°/40 ktsFind the estimated trip fuel.A) 1.450 kgB) 1.550 kgC) 1.900 kg#D) 1.740 kg4357. (AIR: atpl)

(Refer to figure 033-21)Given for the twin jet aeroplane:Estimated mass on arrival at the alternate: 50.000 kgElevation at destination aerodrome: 3.500 ftElevation at alternate aerodrome: 30 ftFind final reserve fuel.A) 1.150 kgB) 2.360 kg#C) 1.180 kgD) 2.300 kg4358. (AIR: atpl)(Refer to figure 033-29)The aeroplane gross mass at top of climb: 61.500 kg

The distance to be flown: 385 NM at FL350OAT: -54 °CWind component: 40 kts tailwindUsing long range cruise procedure what fuel is required?A) 2.350 kgB) 2.250 kg#C) 2.150 kgD) 2.050 kg12247. (AIR: atpl)(Refer to figure 033-37)



Planning an IFR flight from Paris to London for the twin jetaeroplane. Given:Estimated Landing Mass: 49.700 kgFL280W/V 280°/40 ktsAverage True Course: 320°Procedure for descent: M0,74/250 KIASDetermine the distance from the top of descent to London(elevation 80 ft).A) 87 NMB) 97 NMC) 65 NM#D) 76 NM12249. (AIR: atpl)(Refer to figure 033-37)Planning an IFR flight from Paris to London for the twin jetaeroplane. Given:Estimated Landing Mass: 49.700 kgFL280W/V 280°/40 ktsAverage True Course: 320°Procedure for descent: M0,74/250 KIASDetermine the fuel consumption from the top of descent toLondon (elevation 80 ft).

A) 210 kgB) 320 kg#C) 273 kgD) 263 kg

033-05 JET AEROPLANES FLIGHT PLANNING62© 2008AVIATIONEXAM.com12553 (B) 12554 (C) 12555 (C) 12559 (C) 12560 (B) 12561 (A) 12562 (A) 14551 (A)14553 (B)12553. (AIR: atpl)(Refer to figure 033-19)

Given a trip time of about 9 hours, within the limits of thedata given, a temperature decrease of 30 °C will affect thetrip time by approximately:A) -10%#B) +7%C) +3%D) -4%12554. (AIR: atpl)(Refer to figure 033-19)For a flight of 3.500 ground nautical miles, the followingapply:Tail wind component: 50 ktsTemperature: ISA +10 °C

Brake release mass: 65.000 kgThe trip fuel and trip time respectively are:A) 21.800 kg, 9 hrs 25 min.B) 19.000 kg, 7 hrs 45 min.#C) 18.100 kg, 7 hrs 20 min.D) 15.800 kg, 6 hrs 00 min.12555. (AIR: atpl)(Refer to figure 033-19)For a flight of 2.400 ground nautical miles, the followingapply:



Tail wind: 25 ktsTemperature: ISA -10 °CBrake release mass: 66.000 kgThe trip fuel and trip time respectively are:A) 14.600 kg, 5 hrs 45 min.B) 15.000 kg, 6 hrs 00 min.#C) 14.000 kg, 5 hrs 35 min.D) 15.800 kg, 6 hrs 20 min.12559. (AIR: atpl)(Refer to figure 033-40)Given:Diversion fuel available: 8.500 kgDiversion cruise altitude: 10.000 ftMass at point of diversion: 62.500 kgHead wind component: 50 ktsTemperature: ISA -5 °CThe maximum diversion distance, and elapsed time alternate,are approximately:A) 760 NM, 4 hrs 30 min.B) 1.130 NM, 3 hrs 30 min.#C) 860 NM, 3 hrs 20 min.D) 1.000 NM, 3 hrs 40 min.12560. (AIR: atpl)(Refer to figure 033-39)

For the purpose of planning an extended range flight it isrequired that with a start of diversion mass of 55.000 kg adiversion of 600 nautical miles should be achieved in 90minutes. Using the above table, the only listed cruise techniqueto meet that requirement is:A) LRC#B) M 0,74 / 330 KIASC) M 0,74 / 290 KIASD) M 0,70 / 280 KIAS12561. (AIR: atpl)(Refer to figure 033-39)Using the above table, in ISA conditions and at a speed ofM 0,70/280 KIAS, in an elapsed time of 90 minutes an aircraft

with mass at point of diversion 48.000 kg could diverta distance of:#A) 584 NMB) 563 NMC) 603 NMD) 608 NM12562. (AIR: atpl)(Refer to figure 033-39)An aircraft on an extended range operation is required neverto be more than 120 minutes from an alternate, basedon 1 engine inoperative LRC conditions in ISA. Using theabove table and a given mass of 40.000 kg at the most criticalpoint, the maximum air distance to the relevant alternate

is:#A) 735 NMB) 794 NMC) 810 NMD) 875 NM14551. (AIR: atpl)(Refer to figure 033-41 and 033-42)An aircraft is planned to fly a LRC at FL350, ISA -10 °C, atan average gross cruise weight of 55.000 kg and a LandingWeight (Without Tankered Fuel) of 47.500 kg; the wind component



is -30 kts and the trip distance 1.600 NGM. Calculatethe Break Even Fuel Price Destination Airport if the FuelPrice at Departure Airport is 75 cents/US Gallon.#A) 90 centsB) 80 centsC) 95 centsD) 85 cents14553. (AIR: atpl)(Refer to figure 033-41 and 033-42)An aircraft is tasked to fly a 0,74 Mach cruise at FL310, ISA+15 °C with a Landing Weight(Without Tankered Fuel) of40.000 kg. The sector distance is 1.050 NGM, wind component+35 kts.Calculate the Break Even Fuel Price at Destination if theFuel price at Departure is 85 cents/US Gallon.A) 85 cents#B) 92 centsC) 98 centsD) 80 cents

033-05 JET AEROPLANES FLIGHT PLANNING63© 2008AVIATIONEXAM.com

17198 (B) 17199 (B) 17200 (A) 22884 (A) 22885 (A) 22886 (D) 22887 (A)17198. (AIR: atpl)(Refer to figures 033-48, 033-60, 033-62)The flight crew of a turbojet aeroplane prepares a flight usingthe following data:Flight leg ground distance: 4.000 NMFlight Level 370Long range flight regimeEffective wind at this level: 50 kts headTemperature: ISACentre of Gravity (CG): 37%Pack Flow: LOW (LO)Anti Ice: OFF

Reference Landing mass: 140.000 kgTaxi Fuel: 500 kgFinal Reserve Fuel: 2.400 kgThe fuel quantity which must be loaded on board the aircraftis:A) 41.590 kg#B) 51.860 kgC) 52.060 kgD) 46.340 kg17199. (AIR: atpl)(Refer to figure 033-43 and 033-63)A turbojet aeroplane is prepared for a 1.300 NM flight atFL350, with a true airspeed of 460 kts and a headwind of

160 kts. The takeoff runway limitation is 174.000 kg, theplanned departure mass is 160.000 kg. The departure fuelprice is equal to 0,92 times the arrival fuel price (fuel priceratio = 0,92). In order for the airline to optimize its savings,the additional fuel quantity that must be loaded onboardis:A) 0 kg#B) 14.000 kgC) 30.000 kgD) 12.000 kg



17200. (AIR: atpl)(Refer to figure 033-43 and 033-63)Assuming a departure/destination fuel price ratio of 0,91,the commander decides to optimize fuel tankering by usingthe following data:Cruise flight level: FL350Air distance to be covered: 2.500 NMPlanned takeoff mass: 200.000 kg (with the minimum prescribedfuel quantity of 38.000 kg that includes a trip fuelof 29.000 kg)Maximum landing mass: 180.000 kgMaximum takeoff mass: 205.000 kgMaximum tank capacity: 40.000 kgThe additional fuel quantity will be:#A) 0 kgB) 3.000 kgC) 2.000 kgD) 5.000 kg22884. (AIR: atpl)(Refer to figures 033-45 and 033-46)In standard atmosphere, assuming a mass of 197.000 kg, inorder to fly at FL370 and to be at the optimum altitude, yourMach number should be:#A) 0,82.

B) 0,84.C) 0,80.D) the same as for LRC (Long Range Cruise).22885. (AIR: atpl)(Refer to figures 033-47, 033-50 and 033-62)Given:Mass at brake release: 210.000 kgSelected cruise speed: Mach 0,82Flight leg distance: 3.000 NMCruise level: optimumAir conditioning: standardAnti-icing: OFFTemperature: ISA

CG: 37Assuming zero wind, the planned landing mass at destinationwill be:#A) 172.300 kgB) 170.400 kgC) 171.300 kgD) 176.100 kg22886. (AIR: atpl)(Refer to figures 033-47, 033-49 and 033-62)Given:Mass at brake release: 190.000 kgSelected cruise speed: Mach 0,82Flight leg distance: 1.500 NM

Cruise level: optimumAir conditioning: standardAnti-icing: OFFTemperature: ISACG: 37%Assuming zero wind, the planned landing mass at destinationwill be:#A) 169.200 kgB) 170.200 kgC) 174.800 kg



#D) 171.200 kg22887. (AIR: atpl)(Refer to figures 033-47, 033-49 and 033-62)Given:Mass at brake release: 190.000 kgSelected cruise speed: Mach 0,82Flight leg distance: 1.500 NMCruise level: optimumAir conditioning: standardAnti-icing: OFFTemperature: ISACG: 37%Assuming zero wind, the planned flight time from takeoff tolanding needed to complete this flight will be:#A) 209 minutesB) 191 minutesC) 198 minutesD) 203 minutes

033-05 JET AEROPLANES FLIGHT PLANNING64© 2008AVIATIONEXAM.com22888 (C) 22889 (C) 22890 (A) 22891 (B) 22892 (A) 22893 (C)

22888. (AIR: atpl)(Refer to figures 033-47, 033-50 and 033-62)Given:Mass at brake release: 210.000 kgSelected cruise speed: Mach 0,82Air distance: 3.000 NMCruise level: optimumAir conditioning: standardAnti-icing: OFFTemperature: ISACG: 37%Assuming zero wind, the planned flight time from takeoff tolanding needed to complete this flight will be:

A) 394 minutesB) 389 minutes#C) 400 minutesD) 381 minutes22889. (AIR: atpl)(Refer to figures 033-48)For a long distance flight at FL370, Long Range regime,divided into four flight legs with the following specifications:Leg 1 - Ground distance: 2.000 NM, headwind component:50 ktsLeg 2 - Ground distance: 1.000 NM, headwind component:30 ktsLeg 3 - Ground distance: 500 NM, tailwind component: 70

ktsLeg 4 - Ground distance: 1.000 NM, headwind component:20 ktsThe total air distance is approximately:A) 4.580 NMB) 4.820 NM#C) 4.800 NMD) 4.940 NM22890. (AIR: atpl)(Refer to figures 033-45)







For a long distance flight at FL390, Long Range regime,divided into four flight legs with the following characteristics:Leg 1 - Ground distance: 2.000 NM, head wind component:50 ktsLeg 2 - Ground distance: 1.000 NM, head wind component:30 ktsLeg 3 - Ground distance: 500 NM, tail wind component: 100ktsLeg 4 - Ground distance: 1.000 NM, head wind component:70 ktsThe air distance of the entire flight is approximately:A) 5.040 NM#B) 4.900 NMC) 5.120 NMD) 4.630 NM22899. (AIR: atpl)(Refer to figures 033-47, 033-49, 033-50 and 033-62)Planning a MACH 0,82 cruise at FL390, the estimated landingmass is 160.000 kg. The ground distance is2.800 NM and the mean wind is equal to zero. ISA conditions.Fuel consumption will be:A) 30.371 kg#B) 32.657 kgC) 30.117 kg

D) 27.577 kg22900. (AIR: atpl)(Refer to figures 033-47, 033-49, 033-50 and 033-62)Planning a Mach 0,82 cruise at FL390, the estimated landingmass is 160.000 kg, the ground distance is 2.800 NMand the mean tailwind is 100 kt, ISA conditions. Fuel consumptionwill be:#A) 26.950 kgB) 22.860 kgC) 24.900 kgD) 30.117 kg22901. (AIR: atpl)(Refer to figure 033-54)

A turbojet aeroplane, weighing 200.000 kg, initiates itscruise at the optimum level at M 0,84 (ISA, CG=37%, TotalAnti Ice ON). A head wind of 30 kts is experienced and, aftera distance of 500 NM, severe icing is encountered andthis requires an immediate descent. The aeroplane mass atstart of descent is:A) 193.800 kg#B) 192.500 kgC) 193.000 kgD) 193.400 kg

033-05 JET AEROPLANES FLIGHT PLANNING66

© 2008AVIATIONEXAM.com22902 (B) 22903 (A) 22904 (D) 22905 (C) 22906 (A) 22907 (A) 23735 (A)22902. (AIR: atpl)(Refer to figure 033-52, 033-58 and 033-59)Given:Takeoff mass: 150.000 kgPlanned cruise at FL350Long range MachStandard Atmosphere (ISA)



CG: 37%Covering an air distance of 2.000 NM, your trip fuel fromtakeoff to landing will be:A) 20.260 kg#B) 22.360 kgC) 19.660 kgD) 21.760 kg22903. (AIR: atpl)(Refer to figure 033-51)A turbojet aeroplane is flying using the following data:Flight level FL250, Long Range (LR) cruise, mass of 150.000kgTemperature: ISAHead wind component: 100 ktsRemaining flight time: 1 hrs 40 minThe ground distance that can be covered during the cruiseflight is:#A) 445 NMB) 612 NMC) 841 NMD) 2.031 NM22904. (AIR: atpl)(Refer to figure 033-53)A turbojet aeroplane is flying using the following data:

Optimum flight level, Mach 0,80, mass of 190.000 kgTemperature: ISATailwind component: 100 ktsThe fuel mileage and the fuel consumption per hour are:A) 105 NM / 1.000 kg; 6.515 kg/hrs.B) 86 NM / 1.000 kg; 6.515 kg/hrs.C) 71 NM / 1.000 kg; 5.330 kg/hrs.#D) 105 NM / 1.000 kg; 5.330 kg/hrs.22905. (AIR: atpl)(Refer to figures 033-49 and 033-62)Assuming the following data:Ground distance to be covered: 2.600 NMCruise flight level: FL370

Cruising speed: Mach 0,82 (true airspeed: 470 kt)Wind: zero wind during flightPlanned destination landing mass: 140.000 kgTemperature: ISA +15 °CCG: 37%Total anti-ice: ONAir conditioning: normalFuel consumption for such a flight is:A) 29.400 kgB) 27.400 kg#C) 31.500 kgD) 29.100 kg22906. (AIR: atpl)

(Refer to figures 033-49 and 033-62)Assuming the following data:Ground distance to be covered: 2.500 NMCruise flight level: FL350Cruising speed: Mach 0,82 (true airspeed: 470 kt)Tailwind component: 40 ktsPlanned destination landing mass: 150.000 kgTemperature: ISACG: 37%Total anti-ice: OFF



Air conditioning: normalFuel consumption for such a flight is:#A) 27.800 kgB) 27.000 kgC) 28.300 kgD) 29.200 kg22907. (AIR: atpl)(Refer to figures 033-49 and 033-62)Assuming the following data:Ground distance to be covered: 1.500 NMCruise flight level: FL310Cruising speed: Mach 0,82 (true airspeed: 470 kts)Head wind component: 40 ktsPlanned destination landing mass: 140.000 kgTemperature: ISA +15 °CCG: 37%Total anti-ice: ONPack flow: HIFuel consumption for such a flight is:#A) 23.500 kgB) 21.500 kgC) 21.700 kgD) 19.900 kg23735. (AIR: atpl)

(Refer to figure 033-43 and 033-63)Assuming a departure/destination fuel price ratio of 0,92,the commander decides to optimize fuel tankering by usingthe following data:Cruise flight level: FL350Air distance to be covered: 1.830 NMPlanned takeoff mass: 190.000 kg (with a minimum prescribedfuel quantity of 30.000 kg that includes a trip fuelof 22.000 kg)Maximum landing mass: 180.000 kgMaximum takeoff mass: 205.000 kgMaximum tank capacity: 40.000 kgThe additional fuel quantity will be:

#A) 10.000 kgB) 20.000 kgC) 12.000 kgD) 15.000 kg

033-05 JET AEROPLANES FLIGHT PLANNING67© 2008AVIATIONEXAM.com23736 (D) 23740 (B) 23741 (D) 23742 (D) 23743 (B) 23744 (B)23736. (AIR: atpl)(Refer to figures 033-49 and 033-62)Assuming the following data:

Ground distance to be covered: 2.000 NMCruise flight level: FL330Cruising speed: Mach 0,82 (true airspeed: 470 kts)Head wind component: 30 ktsPlanned destination landing mass: 160.000 kgTemperature: ISACG: 37%Total anti-ice: ONPack flow: HITime needed to carry out such a flight is:





case.23743. (AIR: atpl)(Refer to figure 033-56)The flight crew of a turbojet aeroplane prepares a flight usingthe following data:FL370 at Long Range (LR) cruise regimeMass at brake release: 212.800 kgFlight leg ground distance: 2.500 NMTemperatures: ISACG: 37%Headwind component: 30 ktsTotal anti-ice set on ON for the entire flightNo requested climb and descent correction of the fuel consumptionThe fuel consumption (from takeoff to landing) is:A) 30.440 kg#B) 34.430 kgC) 32.480 kgD) 28.720 kg23744. (AIR: atpl)(Refer to figure 033-44 and 033-63)The flight crew of a turbojet aeroplane prepares a flight usingthe following data:Flight leg distance: 3.500 NMFL310

True airspeed: 450 ktsHeadwind component at this level: 55 ktsInitially planned takeoff mass (without extra fuel on board):180.000 kgFuel price: 0,27 $/l at destinationThe commander may carry on board 8.000 kg more fuelthan that which is necessary. For this fuel transportoperation to be cost effective, the maximum fuel price atdeparture must be:A) 0,38 $/l#B) 0,30 $/lC) 0,24 $/lD) 0,21 $/l

033-05 JET AEROPLANES FLIGHT PLANNING68© 2008AVIATIONEXAM.com23745 (A) 23746 (D) 23888 (B) 24754 (D) 24756 (A) 24759 (C) 24770 (D) 24793 (C)23745. (AIR: atpl)(Refer to figure 033-44 and 033-63)The flight crew of a turbojet aeroplane prepares a flight usingthe following data:Flight leg distance: 3.500 NMFlight level FL310, true airspeed: 450 ktsHeadwind component at this level: 55 kts

Initially planned takeoff mass (without extra fuel on board):180.000 kgFuel price: 0,30 $/l at departureThe commander may carry a fuel quantity of 8.000 kg inaddition to that which is necessary. For this fuel transportoperation to be cost effective, the maximum fuel price atarrival must be:#A) 0,27 $/lB) 0,26 $/lC) 0,28 $/l



D) 0,33 $/l23746. (AIR: atpl)(Refer to figure 033-56)The flight crew of a turbojet aeroplane prepares a flight usingthe following data:FL370 at Long Range (LR) cruise regime(Prescribed) mass at brake release: 204.500 kgFlight leg ground distance: 2.000 NMTemperatures: ISAHeadwind component: 70 ktsTotal anti-ice set on ON for the entire flightNo requested climb and descent correction of the fuel consumptionThe fuel required from takeoff to landing is:A) 27.770 kgB) 20.900 kgC) 22.160 kg#D) 29.440 kg23888. (AIR: atpl)Given:FL370M 0,74OAT - 47 °CThe TAS is:A) 424 kts

#B) 434 ktsC) 417 ktsD) 428 kts24754. (AIR: atpl)(Refer to figures 033-25 and 033-28)Given:Long range cruise at FL340Distance C-D: 3.200 NMTemperature deviation from ISA: +12 °CTailwind component: 50 ktsGross mass at C: 55.000 kgThe fuel required from C to D is:A) 17.500 kg

B) 14.200 kgC) 17.800 kg#D) 14.400 kg24756. (AIR: atpl)(Refer to figure 033-29)Given:Long Range Cruise at FL350OAT -45 °CGross mass at the beginning of the leg: 40.000 kgGross mass at the end of the leg: 39.000 kgFind:True airspeed (TAS) and cruise distance (NAM) for atwin jet aeroplane:#A) TAS 433 kts, 227 NAM.

B) TAS 423 kts, 227 NAM.C) TAS 433 kts, 1.163 NAM.D) TAS 423 kts, 936 NAM.24759. (AIR: atpl)(Refer to figure 033-22)Given:Aerodrome at MSLCruise at FL280ISA -10 °CBrake release mass: 57.500 kg



What is the climb fuel required?A) 1.100 kgB) 1.150 kg#C) 1.138 kgD) 2.200 kg24770. (AIR: atpl)(Refer to figure 033-37 and Jeppesen Student Manual -LONDON Heathrow 10-2 STAR or figure AP-08)Given:Aircraft mass: 49.700 kgFL280Plan a descent to Heathrow elevation. What is the descenttime?A) 8 minB) 10 minC) 17 min#D) 19 min24793. (AIR: atpl)(Refer to figure 033-27)Given:Long range cruise: temp. -63 °C at FL330Initial gross mass enroute: 54.100 kgLeg flight time: 29 minFind fuel consumption for this leg:

A) 1.100 kgB) 1.107 kg#C) 1.093 kgD) 1.000 kg

033-05 JET AEROPLANES FLIGHT PLANNING69© 2008AVIATIONEXAM.com24872 (A) 24890 (A) 24893 (D) 24898 (D) 25023 (C) 25025 (D) 25032 (B) 25052 (A)25057 (A) 25072 (D) 25102 (C) 25103 (C)24872. (AIR: atpl)(Refer to figure 033-15)

Given:Trip distance: 1.900 NMFuel on board: 15.000 kgLanding weight: 50.000 kgWhat is the minimum pressure altitude for this flight?#A) 17.000 ftB) 10.000 ftC) FL370D) FL25024890. (AIR: atpl)(Refer to figure 033-20)Alternate airfield is 300 NGM, 50 kts tailwind and a landingweight of 50.000 kg, what is the fuel and time to the alternate?

#A) 1.950 kg, 48 min.B) 1.650 kg, 48 min.C) 2.100 kg, 57 min.D) 1.950 kg, 57 min.24893. (AIR: atpl)(Refer to figure 033-37)What is the time, fuel required and nautical air miles to descendfrom FL350 to sea level in turbulent air given an estimatedlanding weight of 50.000 kg?A) 20 min, 325 kg, 99 NAM.



B) 22 min, 290 kg, 108 NAM.C) 22 min, 290 kg, 105 NAM.#D) 20 min, 275 kg, 99 NAM.24898. (AIR: atpl)(Refer to figure 033-38)After suffering undercarriage and pressurISAtion problemsthe aircraft is to be flown, undercarriage down, 400 NGM atFL100 for repairs. The estimated landing weight is 30.000kg, the temperature is ISA+20 °C and a 50 kts headwind isexpected. What is the fuel and time required for the trip?A) 7.500 kg, 2 hrs.B) 6.400 kg, 2 hrs 5 min.C) 4.600 kg, 1 hrs 40 min.#D) 5.800 kg, 2 hrs.25023. (AIR: atpl)(Refer to figure 033-12)With a cruise weight of 50.000 kg, Cruising at Mach 0,78,what is the optimum altitude?A) 36.200 ftB) 35.800 ft#C) 35.400 ftD) 36.700 ft25025. (AIR: atpl)(Refer to figure 033-24)

An aircraft climbs out from an aerodrome at MSL to FL250,under ISA +20 °C conditions. If the brake release weight is60.000 kg, what is the fuel and ground distance coveredwith a 40 kts tailwind?A) 1.100 kg, 62 NGM.B) 1.100 kg, 48 NGM.C) 1.300 kg, 64 NGM.#D) 1.300 kg, 81 NGM.25032. (AIR: atpl)(Refer to figure 033-21)An aircraft weighing 56.000 kg is required to carry on an enroutestraight and level hold at FL350 for 50 minutes. Howmuch fuel will be used in the hold?

A) 2.017 kg#B) 1.917 kgC) 2.133 kgD) 2.027 kg25052. (AIR: atpl)(Refer to figure 033-29)An aircraft cruising at FL350 in light and variable windsturn at waypoint ALPHA weighing 53.500 kg and later turnswaypoint BRAVO now weighing 50.200 kg. Assuming standardconditions what is the TAS, distance and specific fuelconsumption between Alpha and BRAVO?#A) 429 kts, 627 NM, 5,26 kg/NM.B) 426 kts, 631 NM, 5,22 kg/NM.

C) 429 kts, 627 NM, 6,25 kg/NM.D) 429 kts, 573 NM, 5,24 kg/NM.25057. (AIR: atpl)(Refer to figure 033-42)The surplus burn off for tankering fuel is 20%, if the price atthe departure airfield is 100 cents/gallon, what is the breakevenprice at the destination airfield?#A) 125 cents/gallon.B) 100 cents/gallon.C) 80 cents/gallon.





C) 431 kts#D) 420 kts25125. (AIR: atpl)(Refer to figure 033-29)Given:Long range cruiseOAT -45 °CFL350Headwind component: 40 ktsStart mass: 60.000 kgEnd mass: 55.000 kgFind the TAS at the end of the leg and the distance (NGM):A) 429 kts, 864 NGM.B) 430 kts, 864 NGM.C) 440 kts, 864 NGM.#D) 440 kts, 785 NGM.25126. (AIR: atpl)(Refer to figure 033-20)Planning a flight from Paris (Charles de Gaulle) to London(Heathrow) for a twin jet aeroplane with alternate Manchester.Given:Headwind component from London to Manchester: 10 ktsDistance from London to Manchester: 160 NMAssume the Estimated Landing Mass at the alternate is

50.000 kgFind the alternate fuel and the corresponding time:A) 1.200 kg, 26 minutes.B) 1.300 kg, 28 minutes.C) 1.600 kg, 36 minutes.#D) 1.450 kg, 33 minutes.25157. (AIR: atpl)(Refer to figure 033-26)What would be the required change in fuel required if thetemperature at FL280 was -31 °C?A) + 0,3%B) - 0,3%#C) + 0,6%

D) - 0,6%25167. (AIR: atpl)(Refer to figure 033-15)Given:Cruising altitude: 29.000 ftTemperature: ISA -10 °CTailwind component: 45 ktsLanding Mass: 55.000 kgDistance: 2.800 nautical ground milesFind trip time and fuel burn:A) 6 hrs 25 min, 16.000 kg.B) 6 hrs 40 min, 20.000 kg.C) 5 hrs 50 min, 18.000 kg.

#D) 6 hrs 7 min, 17.100 kg.25169. (AIR: atpl)(Refer to figure 033-20)Given:Estimated Dry Operating Mass: 35.500 kgEstimated load: 14.500 kgFinal Reserve fuel: 1.200 kgDistance to alternate: 95 NMAverage True Track: 219°Headwind component: 10 kts



Find fuel and time to alternate:#A) 1.100 kg, 25 min.B) 1.100 kg, 44 min.C) 800 kg, 24 min.D) 800 kg, 40 min.

033-05 JET AEROPLANES FLIGHT PLANNING71© 2008AVIATIONEXAM.com25170 (B) 25172 (A) 25176 (A) 25177 (A) 25178 (B) 26300 (B) 28314 (A) 28325 (D)25170. (AIR: atpl)(Refer to figure 033-22)Given:Estimated Takeoff Mass: 52.000 kgAirport elevation: 387 ftCruise: FL280Wind velocity: 280/40Temperature: ISA -10 °CAverage Course: 340° (T)Find the ground distance to Top of Climb (TOC):A) 56 NM#B) 50 NMC) 53 NM

D) 47 NM25172. (AIR: atpl)(Refer to figures 033-23)Given:Brake release mass: 64.000 kgTemperature: ISA +10 °CAirport elevation: 3.000 ftFind time, fuel, atill air distance and TAS for an enrouteclimb at Mach 0,74/280 kts to FL350:#A) 26 min, 1.975 kg, 157 NAM, 399 kts.B) 26 min, 2.050 kg, 157 NAM, 399 kts.C) 20 min, 1.750 kg, 117 NAM, 288 kts.D) 25 min, 1.875 kg, 148 NAM, 391 kts.

25176. (AIR: atpl)(Refer to figure 033-16)Given:Cruise profile: Mach 0,74Planned flight level: FL280Estimated Landing Mass: 50.000 kgTrip distance: 200 NMWind component: 30 kts headwindFind the estimated trip fuel:#A) 1.740 kgB) 1.550 kgC) 1.900 kgD) 1.450 kg

25177. (AIR: atpl)(Refer to figure 033-26)Given:Flight time from top of climb at FL280 to the enroute pointis 48 minutesCruise procedure is long range cruiseTemperature is ISA -5 °CThe takeoff mass is 56.000 kg and climb fuel 1.100 kgFind air distance in Nautical Air Miles (NAM) for this leg andfuel consumption for this leg:



#A) 345 NAM, 1.994 kg.B) 349 NAM, 2.000 kg.C) 345 NAM, 2.000 kg.D) 345 NAM, 2.006 kg.25178. (AIR: atpl)(Refer to figure 033-22)Given:Mass at brake release: 57.500 kgTemperature: ISA -10°Headwind component: 16 ktsInitial cruise: FL280Find climb fuel:A) 1.238 kg#B) 1.138 kgC) 1.387 kgD) 1.040 kg26300. (AIR: atpl)(Refer to figure 033-12, 033-13 and 033-31)Given:Estimated takeoff mass 57.000 kgStill air distance 150 NAMOutside air temperature (OAT) ISA -10°Cruise at Mach 0,74Find cruise altitude and expected true airspeed:

A) 25.000 ft; 445 kts.##B) 25.000 ft; 435 kts.C) 22.000 ft; 441 kts.D) 22.000 ft; 451 kts.28314. (AIR: atpl)(Refer to figure 033-85)You have a decompression at your cruising altitude andfollowing information:Tailwind: 25 ktsDistance to diversion airport: 820 ktsISA: +20 °CWeight: 55.000 kgIcing conditions: No

What is your diversion fuel?A) 7.270 kgB) 7.000 kgC) 8.581 kgD) 7.480 kg28325. (AIR: atpl)(Refer to figures 033-23)Given:Brake release mass: 58.000 kgTemperature: ISA +15The fuel required to climb from an aerodrome at elevation4.000 ft to FL300 is:A) 1.350 kg

B) 1.400 kgC) 1.450 kg#D) 1.250 kg

033-05 JET AEROPLANES FLIGHT PLANNING72© 2008AVIATIONEXAM.com28327 (A) 28328 (B) 28329 (A) 28330 (D) 28331 (D) 29197 (D) 2270 (C) 2313 (C)28327. (AIR: atpl)



(Refer to figure 033-83)Given :Distance B - C: 350 NMCruise 300 KlAS at FL210Temperature: - 40 °CTailwind component: 70 ktsGross mass at B: 53.200 kgThe fuel required from B - C is:#A) 1.940 kgB) 1.810 kgC) 2.800 kgD) 2.670 kg28328. (AIR: atpl)(Refer to figure 033-21)The fuel required for 30 minutes holding, in a racetrack pattern,at PA 1.500 ft, mean gross mass 45.000 kg, is:A) 1.010 kg.#B) 1.090 kg.C) 1.310 kg.D) 2.180 kg.28329. (AIR: atpl)(Refer to figure 033-21)The fuel required for 45 minutes holding, in a racetrack pattern,at PA 5.000 ft, mean gross mass 47 000 kg, is:

#A) 1.635 kgB) 1.090 kgC) 1.690 kgD) 1.125 kg28330. (AIR: atpl)(Refer to figure 033-20)Given:Distance to alternate 450 NMLanding mass at alternate: 45.000 kgTailwind component: 50 ktsThe Alternate fuel required is:A) 2.900 kgB) 2.750 kg

C) 3.050 kg#D) 2.500 kg28331. (AIR: atpl)(Refer to figure 033-20)Given:Distance to Alternate: 400 NMLanding mass at Alternate: 50.000 kgHeadwind component: 25 ktsThe alternate fuel required is:A) 2.650 kgB) 2.550 kgC) 2.900 kg#D) 2.800 kg

29197. (AIR: atpl)(Refer to figure 033-84)You have an engine failure and a decompression at thesame time. Your data are:Tailwind: 25 ktsDistance to diversion airport: 820 ktsISA +10°Weight: 55.000 kgIcing conditions: YESWhat is your diversion fuel?



A) 8.300 kgB) 7.035 kgC) 7.000 kg#D) 8.440 kg033-05-02 Computerised flight planning2270. (AIR: atpl)Which of the following statements is (are) correct with regardto computer flight plans?1) The computer takes account of bad weather on the routeand adds extra fuel.2) The computer calculates alternate fuel sufficient for amissed approach, climb, cruise, descent and approach andlanding at the destination alternate.A) Statement 1 only.B) Both statements.C) Statement 2 only.D) Neither statement.2313. (AIR: atpl)Reference computer flight plans.Are they able to account for bad weather in calculating fuelrequired?A) Can automatically allow extra consumption for anti-icinguse.B) Can automatically divert route around forecast thunderstorms.

#C) No.D) Can automatically allow for poorly maintained engines.

033-05 JET AEROPLANES FLIGHT PLANNING73© 2008AVIATIONEXAM.com2317 (A) 2335 (A) 28323 (C)2317. (AIR: atpl)Which of the following statements is (are) correct with regardto the advantages of computer flight plans?1) The computer can file the ATC flight plan2) Wind data used by the computer is always more up-todate

than that available to the pilot#A) Statement 1 only.B) Statement 2 only.C) Both statements.D) Neither statement.2335. (AIR: atpl)Which of the following statements is (are) correct with regardto the operation of flight planning computers ?1) The computer can file the ATC flight plan.2) In the event of inflight re-routing the computer producesa new plan#A) 1 only.B) 2 only.

C) NeitherD) Both.28323. (AIR: atpl)Which of the following statements is (are) correct with regardto computer flight plans?1) The computer takes account of bad weather on the routeand adds extra fuel.2) The computer calculates alternate fuel sufficient for amissed approach, climb, cruise, descent and approach andlanding at the destination alternate.



A) 1.B) 1, 2.#C) 2.D) Neither statement.

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN74© 2008AVIATIONEXAM.com1139 (C) 1145 (A) 1161 (A) 1190 (D) 1194 (B) 1200 (C) 1291 (A) 1293 (D)2177 (D) 2183 (B)033-06-01 Extraction of data1139. (all)(Refer to figure 033-03)Given:FL75OAT +10 °CLean mixture at 2.300 RPMFind the fuel flow in gallons per hour (GPH) and TAS.A) 71,1 GPH, 143 kts.B) 11,6 GPH, 143 kts.#C) 11,6 GPH, 160 kts.D) 68,5 GPH, 160 kts.1145. (all)

(Refer to figure 033-01)Given:FL75OAT: +5 °CDuring climb: average head wind component 20 ktsTakeoff from MSL with the initial mass of 3.650 lbsFind the still air distance (NAM) and ground distance (NM)using the graph TIME, FUEL, DISTANCE TO CLIMB:#A) 18 NAM, 15 NM.B) 16 NAM, 18 NM.C) 18 NAM, 13 NM.D) 14 NAM, 18 NM.1161. (all)

(Refer to figure 033-01)Given:Takeoff mass 3.500 lbsDeparture aerodrome pressure altitude 2.500 ft, OAT+10 °CFirst cruising level: FL140, OAT -5 °CFind the time, fuel and still air distance to climb:#A) 22 min; 6,7 GAL; 45 NAM.B) 24 min; 7,7 GAL; 47 NAM.C) 16,5 min; 4,9 GAL; 34,5 NAM.D) 23 min; 7,7 GAL; 50 NAM.1190. (all)(Refer to figure 033-11)

A flight is to be made to an airport, pressure altitude 3.000ft, in a multi engine piston aeroplane (MEP1). The forecastOAT for the airport is -1 °C. The cruising level will be FL110,where OAT is -10 °C. Calculate the still air descent distancefor:145 KIASRate of descent 1.000 ft/minGear and flaps upA) 25 NMB) 29 NM





75© 2008AVIATIONEXAM.com2185 (C) 2188 (A) 2195 (B) 2201 (B) 2205 (C) 2206 (B) 2221 (D) 2233 (B)2240 (B) 2241 (C) 2257 (A)2185. (all)(Refer to Jeppesen Manual SID chart for AMSTERDAMSCHIPOL (10-3) or figure AP-06)Which statement is correct for ANDIK departures from runway19L?A) Maximum IAS 250 kts turning left at SPL 3,1 DME.B) Cross ANDIK below FL60.#C) Contact SCHIPOL DEPARTURE 119,05 passing 2.000 ftand report altitude.D) The distance to ANDIK is 25 NM.2188. (all)(Refer to Jeppesen Manual AMSTERDAM SCHIPOL - ILSDME RWY 22 (11-6) or figure AP-07)The missed approach procedure is to climb to an altitude of ___ on a track of ___.#A) 2.000 ft; 160°B) 200 ft; 223°C) 3.000 ft; 160°D) 3.000 ft; 223°

2195. (all)(Refer to Jeppesen Manual Munich SID (10-3D) or figureAP-10)Which is the correct departure via KEMPTEN from runway26L?A) KEMPTEN THREE ECHO.#B) KEMPTEN FIVE SIERRA.C) KEMPTEN THREE QUEBEC.D) KEMPTEN THREE NOVEMBER.2201. (all)(Refer to Route Manual chart STAR LONDON Heathrow(10-2) or figure AP-08)Planning a IFR flight from Paris (Charles de Gaulle) to London

(Heathrow). Find the elevation of the destination aerodrome.A) 77 ft#B) 80 ftC) 177 ftD) 100 ft2205. (all)(Refer to Jeppesen Manual - ZURICH ILS Rwy 16 (11-2) orfigure AP-11)The lowest published authorised RVR for an ILS approach,glide slope out, all other aids serviceable, aeroplane categoryA, is:A) 800 mB) 600 m

#C) 720 mD) 1.500 m2206. (all)(Refer to Jeppesen Manual - LONDON HEATHROW ILS DMERwy 09R (11-1) or figure AP-12)The Minimum Descent Altitude (MDA) for an ILS approach,glide slope out, is:A) 405 ft#B) 480 ftC) 275 ft



D) 200 ft2221. (all)(Refer to Jeppesen Manual, any SID or approach chart forLondon Heathrow or figure AP-12).Which of the following is the correct Minimum Safe Altitude(MSA) for the airport?A) East sector 2.300 ft within 50 NM.B) West sector 2.300 ft within 25 NM.C) East sector 2.100 ft within 50 NM.#D) West sector 2.100 ft within 25 NM.2233. (all)(Refer to Route Manual chart E(HI)4 or figure HI-09)An aeroplane has to fly from Abbeville (50°08,1N 001°51,3E)to Biggin (51°19,8N 00°00,2E). At Biggin you can find:141°. This is:A) the average true course of the great circle from Biggin toAbbeville.#B) the magnetic great circle course from Biggin to Abbeville.C) the radial, referenced to true north, of Biggin to fly inbound.D) the magnetic course to fly inbound to Biggin.2240. (all)(Refer to Jeppesen Manual MADRID, BARAJAS page 11-1.ILS DME RWY 33 or figure AP-15)The minimum glide slope interception altitude for a full ILS

is:A) 3.500 ft#B) 4.000 ftC) 2.067 ftD) 1.567 ft2241. (all)(Refer to Route Manual chart SID PARIS Charles-De-Gaulle(20-3) or figure AP-03)Planning a IFR flight from Paris (Charles de Gaulle) to London(Heathrow). Find the elevation of the departure aerodrome.A) 217 ftB) 268 ft#C) 387 ft

D) 2 ft2257. (all)(Refer to Jeppesen Manual Paris Charles-de-Gaulle (21-7)ILS rwy 10 or figure AP-16)What is the ILS course?#A) 088°B) 100°C) 118°D) 268°

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN76© 2008

AVIATIONEXAM.com2271 (B) 2282 (C) 2284 (C) 2286 (C) 2296 (B) 2303 (D) 2306 (D) 2308 (B)2319 (A)2271. (AIR: atpl; HELI: atpl, cpl)Given:15.000 kg total fuelReserve 1.500 kgTAS 440 ktsWind component 45 head outboundAverage fuel flow 2.150 kg/hrs



What is the distance to the point of safe return?A) 1.520 NM#B) 1.368 NMC) 1.702 NMD) 1.250 NM2282. (AIR: atpl; HELI: atpl, cpl)If CAS is 190 kts, Altitude 9.000 ft, Temp. ISA - 10 °C, TrueCourse (TC) 350°, W/V 320/40, distance from departure todestination is 350 NM, endurance 3 hours and actual timeof departure is 1105 UTC. The distance from departure toPoint of Equal Time (PET) is:A) 183 NMB) 147 NM#C) 203 NMD) 167 NM2284. (AIR: atpl; HELI: atpl, cpl)Given:Distance from A to B: 2.050 NMMean groundspeed on 440 ktsMean groundspeed back 540 ktsThe distance to the point of equal time (PET) between Aand B is:A) 920 NMB) 1.025 NM

#C) 1.130 NMD) 1.153 NM2286. (AIR: atpl; HELI: atpl, cpl)Find the time to the Point of Safe Return (PSR). Given:Maximum usable fuel: 15.000 kgMinimum reserve fuel: 3.500 kgTAS out: 425 ktsHead wind component out: 30 ktsTAS return: 430 ktsTailwind component return: 20 ktsAverage fuel flow: 2.150 kg/hrsA) 2 hrs 59 minB) 3 hrs 43 min

#C) 2 hrs 51 minD) 2 hrs 43 min2296. (AIR: atpl; HELI: atpl, cpl)Given:Course A to B: 088° (T)Distance: 1.250 NMMean TAS: 330 ktsMean W/V: 340°/60 ktsThe time from A to the PET between A and B is:A) 1 hour 54 minutes.B) 1 hour 42 minutes.#C) 1 hour 39 minutes.D) 2 hours 02 minutes.

2303. (AIR: atpl; HELI: atpl, cpl)Given:Fuel flow: 2.150 kg/hrsTotal fuel in tanks: 15.000 kgFuel reserve required on arrival: 3.500 kgTAS outbound: 420 kts, wind -30 ktsTAS home bound: 430 kts, wind +20 ktsFind the time to Point of Safe Return.A) 2 hrs 06 minB) 1 hrs 26 min



C) 3 hrs 33 min#D) 2 hrs 52 min2306. (AIR: atpl; HELI: atpl, cpl)Given:Distance A to B: 3.060 NMMean ground speed OUT: 440 ktsMean ground speed BACK: 540 ktsSafe Endurance: 10 hoursThe time to the Point of Safe Return (PSR) is:A) 5 hours 20 minutes.B) 5 hours 45 minutes.C) 3 hours 55 minutes.#D) 5 hours 30 minutes.2308. (AIR: atpl)Given:Distance X to Y: 2.700 NMMach number: 0,75Temperature: -45 °CMean wind component ON: 10 ktsTailwind Mean wind compontent BACK: 35 kts tailwindThe distance from X to the point of equal time (PET) betweenX and Y is:A) 1.350 NM#B) 1.386 NM

C) 1.313 NMD) 1.425 NM2319. (AIR: atpl; HELI: atpl, cpl)Given the following:D = flight distanceX = distance to Point of Equal TimeGSo = groundspeed outGSr = groundspeed returnThe correct formula to find distance to Point of Equal Timeis:#A) x = D x GSr / (GSo + GSr)B) x = D x GSo / (GSo + GSr)C) x = (D/2) x GSo / (GSo + GSr)

D) x = (D/2) + GSr / (GSo + GSr)

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN77© 2008AVIATIONEXAM.com2913 (D) 4291 (C) 4325 (C) 4327 (D) 4362 (D) 12246 (C) 12250 (D) 12266 (A)14161 (A)2913. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 500 NMTrue track: 090°Wind: 090°/20

TAS: 150 ktsWhat is the distance and time of the PET from the departurepoint?A) Distance: 382 NM; Time: 176 min.B) Distance: 250 NM; Time: 88 min.C) Distance: 217 NM; Time: 100 min.#D) Distance: 283 NM; Time: 131 min.4291. (AIR: atpl; HELI: atpl, cpl)Given:X = Distance A to point of equal time (PET) between A and



BE = EnduranceD = Distance A to BO = Groundspeed ONH = Groundspeed BACKThe formula for calculating the distance X to point of equaltime (PET) is:A) x = (E x O x H) / (O + H)B) x = (D x O) / (O + H)#C) x = (D x H) / (O + H)D) x = (D x O x H) / (O + H)4325. (AIR: atpl; HELI: atpl, cpl)Find the distance to the Point of Safe Return (PSR), given:Maximum usable fuel: 15.000 kgMinimum reserve fuel: 3.500 kgOUTBOUND: TAS 425 kts, head wind component 30 kts,fuel flow 2.150 kg/hrsRETURN: TAS 430 kts, tailwind component 20 kts, fuel flow2.150 kg/hrsA) 1.463 NMB) 1.143 NM#C) 1.125 NMD) 1.491 NM4327. (all)

Integrated range curves or tables are presented in the AeroplaneOperations Manuals. Their purpose is:A) to determine the optimum speed considering the fuel costas well as the time related cost of the aeroplane.B) to determine the flight time for a certain leg under considerationof temperature deviations.C) to determine the still air distance for a wind componentsvarying with altitude.#D) to determine the fuel consumption for a certain still air distanceconsidering the decreasing fuel flow with decreasingmass.4362. (AIR: atpl; HELI: atpl, cpl)A flight is planned from L to M, distance 850 NM.

Using the following data, calculate the time and distanceto PSR:Wind component out: 35 kts (TWC)TAS 450 ktsMean fuel flow out: 2.500 kg/hrsMean fuel flow inbound: 1.900 kg/hrsFuel available: 6.000 kgA) 1 hrs 30 min; 660 NM.B) 1hrs 30 min; 616 NM.C) 1 hrs 16 min; 606 NM.#D) 1 hrs 16 min; 616 NM.12246. (all)(Refer to Route Manual SID chart 20-3 for PARIS Charlesde-

Gaulle or figure AP-03)Planning an IFR-flight from Paris (Charles de Gaulle) RWY27 to London. Given:Distance from PARIS Charles-de-Gaulle to top of climb:50 NM.Determine the distance from the top of climb (TOC) to ABB116,6.A) 36,5 NMB) 31 NM#C) 24,5 NM



D) 33 NM12250. (all)(Refer to Route Manual chart E(HI)4 CAA-Edition, Instrumentapproach chart ILS DME Rwy 27R or figures HI-09;AP-08 and AP-09)Planning an IFR-flight from Paris to London (Heathrow) viainitial approach fix (IAF) Biggin VOR. The distance from topof descent (TOD) to Rwy 27R is 76 NM. Determine the distancefrom ABB 116,6 to TOD.A) 60 NMB) 100 NMC) 55 NM#D) 49 NM12266. (AIR: atpl; HELI: atpl, cpl)Find the distance from waypoint 3 (WP 3) to the criticalpoint. Given:Distance from WP 3 to WP 4: 750 NMTAS out: 430 ktsTAS return: 425 ktsTailwind component out: 30 ktsHeadwind component return: 40 kts#A) 342 NMB) 375 NMC) 408 NM

D) 403 NM14161. (AIR: all)(Refer to figure 033-09)For the MEP, if the OAT is -20 °C at 19.000 ft the TAS at 45%power is:#A) 159 knotsB) 162 knotsC) 165 knotsD) 168 knots

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN78© 2008

AVIATIONEXAM.com17201 (A) 23811 (A) 23812 (B) 23879 (C) 23890 (D) 23892 (D) 23893 (C) 23896 (D)23898 (D) 23900 (D)17201. (AIR: atpl; HELI: atpl, cpl)If CAS is 190 kts, Altitude 9.000 ft. Temp. ISA - 10 °C, TrueCourse (TC) 350°, W/V 320/40, distance from departure todestination is 350 NM, endurance 3 hours, and actual timeof departure is 1105 UTC. The Point of Equal Time (PET) isreached at:#A) 1213 UTCB) 1221 UTCC) 1233 UTCD) 1203 UTC

23811. (all)(Refer to figures 033-66, 033-67 and 033-68)What is the local time (LT) in Greece in Winter and Summer?#A) LT = UTC + 2 Hours; LT = UTC + 3 HoursB) LT = UTC - 2 Hours; LT = UTC - 3 HoursC) LT + 2 Hours = UTC; LT + 3 Hours = UTCD) LT - 3 Hours = UTC; LT - 2 Hours = UTC23812. (all)(Refer to figures 033-66, 033-67 and 033-68)What is the local time (LT) in the Netherlands in Winter and





23898. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 180 NMTrue track: 310W/V: 010/20TAS: 115 ktsWhat is the distance of the PET from the departure point?A) 92 NMB) 82 NMC) 90 NM#D) 98 NM23900. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 220 NMTrue track: 175W/V: 220/10TAS: 135 ktsWhat is the distance of the PET from the departure point?A) 136 NMB) 103 NMC) 110 NM#D) 116 NM

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN

79© 2008AVIATIONEXAM.com23902 (D) 23903 (A) 23905 (C) 23907 (D) 23909 (D) 23911 (C) 23913 (C) 23915 (D)23917 (D)23902. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 250 NMGS Out: 130 ktsGS Home: 100 ktsWhat is the distance of the PET from the departure point?A) 192 NMB) 141 NM

C) 125 NM#D) 109 NM23903. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 2.500 NMGS Out: 540 ktsGS Home: 470 ktsWhat is the time of the PET from the departure point?#A) 129 minB) 171 minC) 28 minD) 149 min23905. (AIR: atpl; HELI: atpl, cpl)

Given:Distance from departure to destination: 256 NMGS Out: 160 ktsGS Home: 110 ktsWhat is the distance of the PET from the departure point?A) 128 NMB) 152 NM#C) 104 NMD) 176 NM23907. (AIR: atpl; HELI: atpl, cpl)







W/V: 060/50TAS: 500 ktsWhat is the distance and time of the PET from the departurepoint?A) Distance: 716 NM; Time: 78 min.B) Distance: 481 NM; Time: 64 min.#C) Distance: 394 NM; Time: 43 min.D) Distance: 438 NM; Time: 53 min.23928. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 95 NMTrue track: 105°W/V: 060/15TAS: 140 ktsWhat is the distance of the PET from the departure point?A) 44 NMB) 47,5 NMC) 82 NM#D) 51 NM23929. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 950 NMGS Out: 275 ktsGS Home: 225 kts

What is the time of the PET from the departure point?A) 114 minB) 139 min#C) 93 minD) 39 min23930. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 1.100 NMTrue track: 280°W/V: 100/80TAS: 440 ktsWhat is the distance time of the PET from the departurepoint?

A) Distance: 550 NM; Time: 75 min.B) Distance: 650 NM; Time: 108 min.C) Distance: 650 NM; Time: 75 min.#D) Distance: 450 NM; Time: 52 min.23931. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 1.345 NMGS Out: 480 ktsGS Home: 360 ktsWhat is the time of the PET from the departure point?A) 128 min#B) 72 minC) 96 min

D) 50 min

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN81© 2008AVIATIONEXAM.com23932 (C) 23933 (B) 23934 (A) 23935 (C) 23936 (D) 23937 (D) 23938 (A) 23939 (B)23941 (A)23932. (AIR: atpl; HELI: atpl, cpl)Given:



Distance from departure to destination: 1.860 NMGS Out: 360 ktsGS Home: 400 ktsWhat is the time of the PET from the departure point?A) 147 minB) 132 min#C) 163 minD) 22 min23933. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 1.950 NMGS Out: 400 ktsGS Home: 300 ktsWhat is the time of the PET from the departure point?A) 223 min#B) 125 minC) 167 minD) 29 min23934. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 2.200 NMTrue track: 150°W/V: 330/50TAS: 460 kts

What is the distance and time of the PET from the departurepoint?#A) Distance: 980 NM; Time: 115 min.B) Distance: 1.120 NM; Time: 179 min.C) Distance: 1.100 NM; Time: 179 min.D) Distance: 980 NM; Time: 144 min.23935. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 2.380 NMGS Out: 420 ktsGS Home: 520 ktsWhat is the time of the PET from the departure point?A) 152 min

B) 123 min#C) 188 minD) 19 min23936. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 2.800 NMTrue track: 140°W/V: 140/100TAS: 500 ktsWhat is the distance and time of the PET from the departurepoint?A) Distance: 1.120 NM; Time: 134 min.B) Distance: 1.120 NM; Time: 114 min.

C) Distance: 1.440 NM; Time: 168 min.#D) Distance: 1.680 NM; Time: 252 min.23937. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 330 NMSafe Endurance: 5 hrsTrue Track: 170°W/V: 140/25TAS: 125 ktsWhat is the distance of the PSR from the departure point?



A) 30 NMB) 194 NMC) 150 NM#D) 303 NM23938. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 1.000 NMSafe Endurance: 4 hrsTAS: 500 ktsGround speed out: 550 ktsGround speed home: 450 ktsWhat is the distance of the PSR from the departure point?#A) 990 NMB) 450 NMC) 495 NMD) 10 NM23939. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 150 NMSafe Endurance: 2,4 hrsTrue Track: 250°W/V: 280/15TAS: 120 ktsWhat is the distance of the PSR from the departure point?

A) 83 NM#B) 142 NMC) 71 NMD) 98 NM23941. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 150 NMSafe Endurance: 3,2 hrsTAS: 90 ktsGround speed out: 100 ktsGround speed home: 80 ktsWhat is the distance and time of the PSR from the departurepoint?

#A) Distance: 142 NM; Time: 85 min.B) Distance: 67 NM; Time: 50 min.C) Distance: 71 NM; Time: 47 min.D) Distance: 8 NM; Time: 5 min.

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN82© 2008AVIATIONEXAM.com23942 (C) 23944 (D) 23946 (C) 23948 (A) 23950 (D) 23951 (A) 23953 (B) 23955 (B)23942. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 1.500 NM

Safe endurance: 4,5 hrsTAS: 450 ktsGround speed out: 480 ktsGround speed home: 410 ktsWhat is the time of the PSR from the departure point?A) 66 minB) 101 min#C) 124 minD) 63 min23944. (AIR: atpl; HELI: atpl, cpl)





23953. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 210 NMSafe endurance: 2,5 hrsTrue track: 035°W/V: 250/20TAS: 105 ktsWhat is the distance of the PSR from the departure point?A) 88 NM#B) 127 NMC) 64 NMD) 172 NM23955. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 210 NMSafe endurance: 3,5 hrsTrue track: 310°W/V: 270/30TAS: 120 ktsWhat is the distance of the PSR from the departure point?A) 125 NM#B) 200 NMC) 100 NMD) 10 NM

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN83© 2008AVIATIONEXAM.com23957 (B) 23959 (A) 23960 (B) 23962 (B) 23964 (C) 23965 (A) 23967 (B) 23968 (A)23957. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 215 NMSafe endurance: 3,3 hrsTrue track: 005°W/V: 290/15TAS: 125 kts

What is the distance of the PSR from the departure point?A) 112 NM#B) 205 NMC) 103 NMD) 9 NM23959. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 240 NMSafe endurance: 3,5 hrsTAS: 125 ktsGround speed out: 110 ktsGround speed home: 140 ktsWhat is the distance and time of the PSR from the departure

point?#A) Distance: 216 NM; Time: 118 min.B) Distance: 134 NM; Time: 58 min.C) Distance: 108 NM; Time: 52 min.D) Distance: 24 NM; Time: 13 min.23960. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 2.450 NMSafe endurance: 7,5 hrsTAS: 410 kts



Ground speed out: 360 ktsGround speed home: 460 ktsWhat is the time of the PSR from the departure point?A) 198 min#B) 252 minC) 111 minD) 156 min23962. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 260 NMSafe endurance: 4,1 hrsTrue track: 150°W/V: 100/30TAS: 110 ktsWhat is the distance of the PSR from the departure point?A) 154 NM#B) 213 NMC) 107 NMD) 47 NM23964. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 300 NMSafe endurance: 4 hrsTAS: 110 kts

Ground speed out: 120 ktsGround speed home: 100 ktsWhat is the distance of the PSR from the departure point?A) 109 NMB) 136 NM#C) 218 NMD) 82 NM23965. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 3.000 NMSafe endurance: 8 hrsTAS: 520 ktsGround speed out: 600 kts

Ground speed home: 440 ktsWhat is the time of the PSR from the departure point?#A) 203 minB) 173 minC) 277 minD) 117 min23967. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 320 NMSafe endurance: 4,3 hrsTrue track: 120°W/V: 180/40TAS: 130 kts

What is the distance of the PSR from the departure point?A) 185 NM#B) 263 NMC) 131NMD) 59 NM23968. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 330 NMSafe endurance: 5 hrsTrue track: 170°



W/V: 140/25TAS: 125 ktsWhat is the distance of the PSR from the departure point?#A) 302 NMB) 194 NMC) 150 NMD) 30 NM

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN84© 2008AVIATIONEXAM.com23970 (A) 23971 (C) 23973 (C) 23975 (B) 23976 (A) 23978 (A) 23980 (D) 23981 (B)23970. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 360 NMSafe endurance: 4,5 hrsTrue track: 345°W/V: 260/30TAS: 140 ktsWhat is the distance of the PSR from the departure point?#A) 308 NMB) 185 NMC) 154 NM

D) 52 NM23971. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 3.750 NMSafe endurance: 9,5 hrsTrue track: 360°W/V: 360/50TAS: 480 ktsWhat is the distance of the PSR from the departure point?A) 1.128 NMB) 2.070 NM#C) 2.255 NMD) 1.495 NM

23973. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 400 NMSafe endurance: 2,5 hrsTAS: 115 ktsGround speed out: 130 ktsGround speed home: 105 ktsWhat is the distance of the PSR from the departure point?A) 73 NMB) 179 NM#C) 145 NMD) 255 NM23975. (AIR: atpl; HELI: atpl, cpl)

Given:Distance from departure to destination: 410 NMSafe endurance: 3,6 hrsTrue track: 055°W/V: 180/35TAS: 120 ktsWhat is the distance of the PSR from the departure point?A) 169 NM#B) 210 NMC) 102 NM





Safe endurance: 3,6 hrsTrue track: 200°W/V: 220/15TAS: 130 ktsWhat is the distance of the PSR from the departure point?#A) 231 NMB) 305 NMC) 116 NMD) 319 NM23984. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 6.340 NMSafe endurance: 15 hrsTrue track: 090°W/V: 270/100TAS: 520 ktsWhat is the distance of the PSR from the departure point?A) 2.560 NM#B) 3.756 NMC) 1.878 NMD) 2.584 NM23985. (AIR: atpl; HELI: atpl, cpl)Given:Distance from departure to destination: 950 NM

Safe endurance: 3,5 hrsTAS: 360 ktsGround speed out: 320 ktsGround speed home: 400 ktsWhat is the distance and time of the PSR from the departurepoint?A) Distance: 528 NM; Time: 79 min.#B) Distance: 622 NM; Time: 117 min.C) Distance: 311 NM; Time: 52 min.D) Distance: 328 NM; Time: 62 min.23986. (all)Given:Fuel density: 0,78 kg/l

Dry Operating Mass: 33.500 kgTraffic load: 10.600 kgMaximum allowable takeoff mass: 66.200 kgTaxi fuel: 200 kgTank capacity: 22.500 lThe maximum possible takeoff fuel is:#A) 17.350 kgB) 22.100 kgC) 17.550 kgD) 21.900 kg24741. (AIR: atpl; HELI: atpl, cpl)Given:Track: 355° (T)

Wind velocity: 340/30 ktsTAS: 140 ktsTotal distance A to B: 350 NMWhat are the time and distance to the point of equal timebetween A and B?A) 75 mins; 211 NM.B) 75 mins; 140 NM.C) 50 mins; 140 NM.#D) 114 mins; 211 NM.24844. (AIR: atpl; HELI: atpl, cpl)



Flying from A to B, 270 NM, true track 030°, wind velocity120/35, TAS 125 kts. What are the distance and time to thePoint of Equal Time?A) 141 NM; 65 min.B) 141 NM; 68 min.#C) 135 NM; 68 min.D) 150 NM; 65 min.25021. (AIR: atpl; HELI: atpl, cpl)An aircraft is to fly from B to C. The total fuel available is50.000 kg but the aircraft must land with at least 5.000 kg.From B to C the TAS is 400 kts, wind component 30 ktsheadwind, fuel flow 7.800 kg/hrs. Should the aircraft haveto return from the PSR its TAS shall be 380 kts, wind component30 kts tailwind and fuel flow 7.500kg/hrs. What isthe distance and time to the point of safe return (PSR) fromB?A) 1.270 NM; 206 min.B) 1.250 NM; 174 min.C) 1.071 NM; 174 min.#D) 1.143 NM; 185 min.25122. (AIR: atpl; HELI: atpl, cpl)Given:X = Distance A to Point of Safe Return (PSR) between Aand B

E = EnduranceD = Distance A to BO = Ground speed on H = Ground speed back The formula for calculating the distance X to PSR is:A) X = D H / (O + H)B) X = D O / (O + H)#C) X = E O H / (O + H)D) X = D O H / (O + H)25185. (AIR: atpl; HELI: atpl, cpl)Track A to B: 088° (T)Distance: 1.250 NMMean TAS: 330 kts

Mean wind: 340/60 ktsFind the time from A to PET:#A) 1 hrs 44 minB) 1 hrs 39 minC) 2 hrs 02 minD) 1 hrs 54 min

033-06 PRACTICAL COMPLETION OF A FLIGHT PLAN86© 2008AVIATIONEXAM.com25561 (A)25561. (AIR: all)

(Refer to figures 033-72)Finish the endurance / fuel calculations and determine ATCendurance for a twin jet aeroplane, with the help of the tableprovided. Contingency is 5% of the planned trip fueland fuel flow for extra fuel is 2.400 kg/hrs:#A) ATC endurance: 04:07B) ATC endurance: 03:52C) ATC endurance: 03:37D) ATC endurance: 04:12



033-07 OFFSHORE OR REMOTE AREA OPERATION87© 2008AVIATIONEXAM.com22881 (B) 22883 (A)22881. (HELI: atpl, cpl)To carry out a VFR flight to an off-shore platform, the minimumfuel quantity on board is:A) that defined for VFR flights over land increased by 10%.#B) identical to that defined for VFR flights over land.C) at least equal to that defined for IFR flights.D) that defined for VFR flights over land increased by 5%.22883. (HELI: atpl, cpl)For a flight to an offshore platform, an alternate aerodromeis compulsory, except if:1) flight duration does not exceed two hours2) during the period from two hours before to two hoursafter the estimated landing time, the forecast conditions ofceiling and visibility are not less than one and a half timesthe applicable minima3) the platform is available and no other flight either fromor to the platform is expected between the estimated timeof departure and one half hour after the estimated landingtime

#A) 1, 2, 3B) 1, 2C) 1, 3D) 2, 3

88© 2008AVIATIONEXAM.com

PICTURE SUPLEMENTS

90© 2008

AVIATIONEXAM.com

033 PICTURE SUPPLEMENTS91© 2008AVIATIONEXAM.comTime, Fuel and Distance to Climb0 10 20 30 40TIME TO CLIMB - MINUTES-50 -40 -30 -20 -10 0 10 20 30 40 50 60OUTSIDE AIR TEMPERATURE°CFUEL TO CLIMB - GALLONS0 1 2 3 4 5 6 7 8 9 10 11

DISTANCE TO CLIMB - NAUTICAL MILES0 10 20 30 40 50 60 70 80ISA16,00014,00012,00010,000800060004000



2000PRESSUREALTITUDEFEETSL3650340030002600INITIALMASS - LBPOWER............................FULL THROTTLE, 2500 RPMFUEL DENSITY................6.0 LB/GALLMIXTURE.........................FULL RICHCOWL FLAPS..................AS REQUIREDASSOCIATED CONDITIONS:EXAMPLE:OAT AT TAKE-OFF...............................15°COAT AT CRUISE..................................-5°CAIRPORT PRESSURE ALTITUDE......5653 FTCRUISE PRESSURE ALTITUDE........11,500 FTINITIAL CLIMB MASS.........................3650 LBTIME TO CLIMB (18 - 6.5)..................11.5 MINFUEL TO CLIMB 6.0 - 2.5)..................3.5 GALDISTANCE TO CLIMB (36 - 12.5).......23.5 NMCLIMB SPEED 110 KT ALL WEIGHTS

FIGURE 033-01033 PICTURE SUPPLEMENTS92© 2008AVIATIONEXAM.comTable 2.2.2 25.0 in. Hg (or full throttle) @ 2,100 rpmOff-peak EGT Cruise lean mixture @ cruise weight 3,400 lbRecommended Cruise Power Settings (continued)NOTE 1: Full-throttle manifold pressure settings are approximate.NOTE 2: Shaded areas represent operation with full throttle.NOTE 3: Fuel ows are to be used for ight planning. Lean using the EGT.ISA

Dev.Press.Alt.IOATMan.Press.Fuel Flow AirspeedoC Feet oC oF In. Hg PPH GPH KIAS KTAS0 -3 26 25.0 63.8 10.6 148 1402,000 -7 19 25.0 66.4 11.1 149 1454,000 -11 12 25.0 68.9 11.5 149 150-20 6,000 -15 5 24.3 68.3 11.4 147 1528,000 -19 -2 22.5 63.9 10.7 139 148

10,000 -23 -9 20.8 60.1 10.0 132 14412,000 -27 -17 19.3 56.7 9.5 123 13914,000 -31 -24 17.9 54.5 9.1 113 13216,000 -35 -32 16.5 52.2 8.7 95 1140 17 62 25.0 61.9 10.3 143 1402,000 13 55 25.0 64.2 10.7 143 1454,000 9 48 25.0 66.6 11.1 144 1500 6,000 5 41 24.3 66.1 11.0 141 1528,000 1 34 22.5 61.9 10.3 134 14810,000 -3 27 20.8 58.5 9.8 126 143



12,000 -7 19 19.3 55.6 9.3 116 13614,000 -11 12 17.9 53.5 8.9 103 12516,000 - - - - - - -0 37 98 25.0 60.1 10.0 138 1402,000 33 91 25.0 62.1 10.4 138 1454,000 29 84 25.0 64.4 10.7 139 150+20 6,000 25 77 24.3 63.9 10.7 136 1518,000 21 70 22.5 60.2 10.0 128 14710,000 17 63 20.8 56.8 9.5 119 14112,000 13 55 19.3 54.5 9.1 108 13114,000 - - - - - - -16,000 - - - - - - -FIGURE 033-02

033 PICTURE SUPPLEMENTS93© 2008AVIATIONEXAM.comTable 2.2.3 23.0 in. Hg (or full throttle) @ 2,300 rpmOff-peak EGT Cruise lean mixture @ cruise weight 3,400 lbRecommended Cruise Power Settings (continued)NOTE 1: Full-throttle manifold pressure settings are approximate.NOTE 2: Shaded areas represent operation with full throttle.NOTE 3: Fuel ows are to be used for ight planning. Lean using the EGT.

ISADev.Press.Alt.IOATMan.Press.Fuel Flow AirspeedoC Feet oC oF In. Hg PPH GPH KIAS KTAS0 -3 26 23.0 67.6 11.3 152 1442,000 -7 20 23.0 69.7 11.6 152 1494,000 -11 13 23.0 72.1 12.0 153 154-20 6,000 -15 6 23.0 74.4 12.4 153 158

8,000 -18 -1 22.4 73.8 12.3 150 16010,000 -23 -9 20.7 68.4 11.4 143 15712,000 -27 -16 19.2 63.8 10.6 135 15314,000 -31 -23 17.8 60.0 10.0 127 14816,000 -35 -31 16.4 56.3 9.4 117 1410 17 62 23.0 65.4 10.9 147 1452,000 13 56 23.0 67.4 11.2 147 1494,000 9 49 23.0 69.4 11.6 148 1540 6,000 5 42 23.0 71.7 12.0 148 1598,000 2 35 22.4 71.1 11.9 145 16010,000 -3 27 20.7 66.2 11.0 137 15712,000 -7 20 19.2 61.8 10.3 129 15214,000 -11 13 17.8 58.5 9.8 120 146

16,000 -15 5 16.4 55.3 9.2 109 1370 37 98 23.0 63.2 10.5 142 1452,000 33 92 23.0 65.1 10.9 143 1494,000 29 85 23.0 67.1 11.2 143 154+20 6,000 25 78 23.0 69.0 11.5 142 1588,000 22 71 22.4 68.5 11.4 140 16010,000 17 63 20.7 64.0 10.7 132 15612,000 13 56 19.2 60.0 10.0 123 15114,000 9 48 17.8 57.1 9.5 113 14216,000 - - - - - - -



FIGURE 033-03

033 PICTURE SUPPLEMENTS94© 2008AVIATIONEXAM.comRangeSL10002000300040005000600070008000900010,00011,00012,00013,00014,000620 640 660 680 700 720 740 760 780 800 820 840 860 880 900 920RANGE - NAUTICAL MILES

NOTE: RANGE INCLUDES CRUISE CLIMB &ALLOWS FOR TAXI, RUNUP, & 45 MINUTESRESERVE FUEL AT ECONOMY CRUISE POWERFULL THROTTLE 2500 RPMFULLTHROTTLE2100RPM21INHG/2100

RPMFULLTHROTTLE2300RPM23INHG/2300RPM25 IN HG / 2100 RPMASSOCIATED CONDITIONS:

MASS.......................................FUEL........................................FUEL DENSITY........................INITIAL FUEL LOAD.................TAKE-OFF ALTITUDE..............WIND........................................3663 LB BEFORE ENGINE STARTAVIATION GASOLINE6.0 LB/GAL74 U.S. GAL (444 LB)



SEA LEVELZEROEXAMPLE:CRUISE ALTITUDE.............11,500 FTPOWER SETTING..............FULL THROTTLE 2500 RPMRANGE...............................866 NM20°C LEAN of PEAK EGT162 152160 148 140129 150 15416917025 IN HG / 2500 RPMTAS - ktISAFIGURE 033-04

033 PICTURE SUPPLEMENTS95© 2008AVIATIONEXAM.comEnduranceFULL THROTTLE 2500 RPMFULL THROTTLE 2300 RPM

FULL THROTTLE 2100 RPM25 IN HG / 2100 RPM21 IN HG / 2100 RPM23 IN HG / 2300 RPM25 IN HG / 2500 RPMSL1000200030004000500060007000

8000900010,00011,00012,00013,00014,000PRESSURE ALTITUDE - FEET3.0 3.5 4.0 4.5 5.0 5.5 6.0 6.5 7.0 7.5 8.0ENDURANCE - HOURSNOTE: ENDURANCE INCLUDES CRUISE CLIMB &ALLOWS FOR TAXI, RUNUP, & 45 MINUTESRESERVE FUEL AT ECONOMY CRUISE POWER

ASSOCIATED CONDITIONS:MASS...............................FUEL................................FUEL DENSITY................INITIAL FUEL LOAD........TAKE-OFF ALTITUDE......WIND................................3663 LB BEFORE ENGINE STARTAVIATION GASOLINE6.0 LB/GAL



74 U.S. GAL (444 LB)SEA LEVELZEROEXAMPLE:CRUISE ALTITUDE....11,500 FTPOWER SETTING......FULL THROTTLE 2500 RPMENDURANCE.............5.4 HRS (5 HRS, 24 MINS)20°C LEAN of PEAK EGT150 129140 148154 170169 160162 152TAS - ktISAFIGURE 033-05

033 PICTURE SUPPLEMENTS96© 2008AVIATIONEXAM.comClimb-40 -20 0 +20 +40 0 20 40 60 80B M I L C O T E C N A T S I D & , E M I T , L E U F C ° E R U T A R E P M E T R I

A E D I S T U OASSOCIATED CONDITIONS:4750 LB GEAR UPCOWL FLAPS CLOSED2600 RPM & 33 IN. HG. or FULL THROTTLEMIXTURE FULL RICHEXAMPLE:DEPARTURE AIRPORT ALTITUDE.............2000 ftDEAPARTURE AIRPORT OAT.....................21°CCRUISE ALTITUDE......................................16,500 ftCRUISE OAT................................................-13°CFUEL TO CLIMB...........................................15 - 2 = 13 galTIME TO CLIMB...........................................27 - 3 = 24 min

DISTANCE TO CLIMB..................................50 - 5 = 45 NM18,0008,00016,00014,00012,00010,0006,0004,0002,000SEA LEVELPRESSURE ALTITUDE - FTISA TEMP

DEPARTUREFUEL galTIME minDISTANCE NMCRUISECLIMB SPEED 120 kt IASFIGURE 033-06

033 PICTURE SUPPLEMENTS97







20,00022,00024,000PRESS. ALT - ft 75%65%45%HIGH SPEEDECONOMYLONG RANGEEXAMPLE:OAT...................................13 °CPRESSURE ALTITUDE....16,500 ftPOWER.............................55%TRUE AIRSPEED..............172 ktASSOCIATED CONDITIONS:MIXTURE FULL RICH ABOVE 75% POWERMIXTURE LEANED IN ACCORDANCE WITH SECTION 4.37COWL FLAPS CLOSEDAIRCRAFT CLEANMID CRUISE MASS (4450 lb)75%65%55%45%

100%ISA TEMPFIGURE 033-09

033 PICTURE SUPPLEMENTS100© 2008AVIATIONEXAM.comEnduranceFIGURE 033-10

033 PICTURE SUPPLEMENTS101

© 2008AVIATIONEXAM.comFuel, Time and Distance to Descend-40 -30 -20 -10 0 +10 +20 +30 +40 0 10 20 30 40 50 60 70 80OUTSIDE AIR TEMPERATURE °C FUEL, TIME & DISTANCE TO DESCENDDESTINATIONCRUISESEA LEVELISA TEMPFUEL galTIME minDISTANCE NM18,000

8,00016,00014,00012,00010,0006,0004,000000,2PRESSURE ALTITUDE - ft22,000



20,000ASSOCIATED CONDITIONS:145 kt IAS 1000 FPM DESCENTAIRCRAFT CLEANNO WINDEXAMPLE:CRUISE ALTITUDE..................16,500 ftCRUISE OAT............................-13°CDESTINATION ALT...................3000 ftDESTINATION OAT..................22°CFUEL TO DESCEND................6 - 1 = 5 galTIME TO DESCEND................16 - 3 = 13 minDISTANCE TO DESCEND.......45 - 8 = 37 NMSOLUTION:FIGURE 033-11

033 PICTURE SUPPLEMENTS102© 2008AVIATIONEXAM.comOptimum AltitudeOff-OptimumConditionFuel Mileage Penalty %

LRC or Mach 0.74 Mach 0.782,000 ft above -1 -1Optimum 0 02,000 ft below -1 -24,000 ft below -4 -48,000 ft below -10 -1112,000 ft below -15 -20Off-Optimum Fuel PenaltyFIGURE 033-12

033 PICTURE SUPPLEMENTS103© 2008

AVIATIONEXAM.comShort Distance Cruise AltitudePRESSURE ALTITUDE 1000 ft1020304045 50 55 60 65 70 40BRAKE RELEASE WEIGHT 1000 kg35TRIP DISTANCE NM100 200 300REF LINE

ISA+20°CISA+10°C&BELOWFIGURE 033-13





033 PICTURE SUPPLEMENTS105© 2008AVIATIONEXAM.comSimpli ed Flight Planning Trip Distances 1,000 NM to 3,000 NMTRIP DISTANCE NM30 40 50 60LANDING WEIGHT1000 kg 100100HEADTAILWINDkt505001000 1500 2000 2500 3000TRIP TIME hr20 10 0 -10ISA DEV °C23

4567BASED ON:280 / 0.74 CLIMB0.74 / 250 DESCENTFUEL REQUIRED 1000 kg610141822

26PRESSUREALTITUDE1000 ftREF LINEREF LINEREF LINEPRESSURE ALTITUDE 1000 FT29 & ABOVE10223733292522

181410PRESSURE ALTITUDE 1000 ft3710LONG RANGE CRUISEFIGURE 033-15

033 PICTURE SUPPLEMENTS





Simpli ed Flight Planning Trip Distances 100 NM to 600 NM1000TRIP DISTANCE NM30 40 50 60LANDING WEIGHT1000 kg 100100HEADTAILWINDkt5050200 300 400 500 600BASED ON:280 / 0.74 CLIMB0.74 / 250 DESCENTTRIP TIME hr20 10 0 -10ISA DEV °C120

PRESSUREALTITUDE1000 ftPRESSURE ALTITUDE 1000 ftPRESSURE ALTITUDE 1000 ft35 & ABOVE3331292725REF LINEREF LINE3735 & ABOVE

251500200025003000350040004500FUEL REQUIRED kgREF LINE250.78 MACH CRUISEFIGURE 033-17

033 PICTURE SUPPLEMENTS108© 2008AVIATIONEXAM.comSimpli ed Flight Planning Trip Distances 1,000 NM to 3,000 NMREF LINEPRESSUREALTITUDE1000 ft



33 & ABOVEBASED ON:280 / 0.74 CLIMB0.74 / 250 DESCENT30 40 50 60TRIP TIME hr23420 10 0 -10ISA DEV °C1000100HEADTAILWINDkt1000 1500 2000 2500 3000TRIP DISTANCE NMLANDING WEIGHT1000 kg5050

5673133 & ABOVE25681012141618

20FUEL REQUIRED 1000 kg220.78 MACH CRUISEREF LINEREF LINEPRESSURE ALTITUDE 1000 ftPRESSURE ALTITUDE 1000 ft252729312537

FIGURE 033-18

033 PICTURE SUPPLEMENTS109© 2008AVIATIONEXAM.comStep Climb Simpli ed Fuel PlanningThis chart allows the planner to optimise aeroplane performance by increasing the cruisealtitude in 4000 ft steps in order to allow for the increase in optimum altitude



as aeroplaneweight decreases.The graph is valid for altitudes with Step Climb of 4,000 ft to 2,000 ft above optimumaltitude. The graph provides trip fuel and time, at LRC or 0.74 M, from brake release totouchdown. The method of use is the same as that for the constant altitude charts exceptthat the argument of Brake Release Weight is used in place of Cruise Pressure Altitude - see example on chart.Simpli ed Flight Planning Trip Distances 1,000 NM to 4,000 NMREF LINETRIP TIME hr3420 10 0 -10ISA DEV °C1000HEADWINDkt1000 1500 2000 2500 3000

TRIP DISTANCE NM505056710152025FUEL REQUIRED 1000 kg28

910100 TAIL3500 40005VALID FOR ALL PRESSURE ALTITUDES WITH 4000 ftSTEP CLIMB TO 2000 ft ABOVE OPTIMUM ALTITUDE STEPPED CLIMB CRUISE706560554550

BRAKE RELEASE WEIGHT 1000 kgALL BRAKE RELEASE WEIGHTSREF LINEFIGURE 033-19

033 PICTURE SUPPLEMENTS110© 2008AVIATIONEXAM.comSimpli ed Flight Planning Alternate Distances to 500 NM





Weight x 1,000 kg66 64 62 60 58 56 54 52 50 48 46 44 42 40 38FUEL FLOW in kg per hour0 8 6 , 1 0 4 7 , 1 0 0 8 , 1 0 0 9 , 1 0 8 9 , 1 0 8 0 , 2 0 6 1 , 2 0 6 2 , 20 0 4 , 2 0 4 5 , 2 0 4 7 , 2 0 0 0 , 7 335,000 3,020 2,820 2,660 2,520 2,420 2,320 2,220 2,140 2,060 1,960 1,880 1,800 1,720 1,66030,000 2,840 2,740 2,660 2,560 2,480 2,400 2,300 2,220 2,140 2,060 1,960 1,880 1,800 1,740 1,68025,000 2,840 2,760 2,660 2,580 2,500 2,420 2,320 2,240 2,160 2,080 2,000 1,920 1,840 1,780 1,72020,000 2,840 2,760 2,680 2,580 2,500 2,420 2,340 2,260 2,180 2,100 2,020 1,940 1,860 1,800 1,76015,000 2,880 2,800 2,700 2,620 2,540 2,460 2,380 2,300 2,220 2,140 2,060 1,980 1,920 1,860 1,80010,000 2,920 2,820 2,740 2,660 2,580 2,500 2,420 2,340 2,260 2,180 2,100 2,020 1,980 1,920 1,8805,000 2,960 2,860 2,780 2,700 2,620 2,540 2,460 2,380 2,300 2,220 2,140 2,080 2,020 1,960 1,9201,500 3,000 2,900 2,820 2,740 2,660 2,580 2,520 2,440 2,360 2,280 2,220 2,140 2,080 2,020 1,980Holding Fuel Flow Flaps RetractedFIGURE 033-21

033 PICTURE SUPPLEMENTS112© 2008AVIATIONEXAM.comISA -6°C TO -15°CPress.Alt.ftUnitsMin/kg.NAM/KtBRAKE RELEASE WEIGHT KG68000 66000 64000 62000 60000 58000 56000 52000 48000 44000 40000

0 5 9 / 2 1 0 5 0 1 / 3 1 0 0 2 1 / 5 1 0 5 3 1 / 7 1 0 5 5 1 / 0 2 0 5 6 1 / 22 0 0 8 1 / 5 2 0 0 1 2 / 0 3 l e u F / e mi T 0 0 0 7 37 7 3 / 4 6 8 7 3 / 3 7 9 7 3 / 5 8 1 8 3 / 8 9 3 8 3 / 7 1 1 5 8 3 / 0 3 1 7 83 / 8 4 1 1 9 3 / 4 8 1 S A T / t s i D0 0 9 / 1 1 0 0 1 1 / 3 1 0 5 1 1 / 4 1 0 0 3 1 / 6 1 0 5 4 1 / 9 1 0 5 5 1 / 02 0 5 6 1 / 2 2 0 0 8 1 / 4 2 0 5 0 2 / 8 2 l e u F / e mi T 0 0 0 6 35 7 3 / 0 6 6 7 3 / 9 6 7 7 3 / 9 7 8 7 3 / 1 9 0 8 3 / 6 0 1 1 8 3 / 5 1 1 3 83 / 7 2 1 5 8 3 / 2 4 1 8 8 3 / 6 6 1 S A T / t s i D35000 Time/Fuel 32/2350 27/2000 24/1850 22/1700 20/1600 19/1500 17/1400 15/125013/1100 12/1000 11/900Dist/TAS 195/390 156/385 139/383 125/381 114/380 105/378 97/377 85/376 74/375 65/374 57/37334000 Time/Fuel 26/2000 23/1850 21/1700 20/1600 19/1500 17/1400 16/1350 14/1200

13/1100 11/950 10/850Dist/TAS 152/383 136/381 123/379 113/378 105/376 97/375 90/375 79/373 70/372 61/371 54/37133000 Time/Fuel 23/1850 21/1750 20/1650 19/1550 17/1450 16/1350 15/1300 14/115012/1050 11/950 10/850Dist/TAS 133/378 121/376 112/375 104/374 97/373 90/372 84/372 74/371 66/370 58/369 51/36832000 Time/Fuel 21/1750 20/1650 19/1550 17/1500 16/1400 16/1300 15/1250 13/115012/1000 11/900 9/800Dist/TAS 120/374 111/373 103/372 96/371 90/370 84/369 79/369 70/368 62/367 55/36



6 48/36631000 Time/Fuel 20/1700 19/1600 18/1500 17/1400 16/1350 15/1300 14/1200 13/110011/1000 10/900 9/800Dist/TAS 110/370 102/369 95/368 89/367 84/367 79/366 74/366 66/365 58/364 52/364 46/36330000 Time/Fuel 19/1600 18/1550 17/1450 16/1350 15/1300 14/1250 13/1200 12/105011/950 10/850 9/800Dist/TAS 101/366 95/365 89/1364 83/364 78/363 74/363 70/362 62/362 55/361 49/361 43/36029000 Time/Fuel 17/1550 16/1450 16/1400 15/1300 14/1250 13/1200 13/1150 11/105010/950 9/850 8/750Dist/TAS 92/361 87/360 81/360 77/359 72/359 68/358 64/358 57/357 51/357 46/357 41/35628000 Time/Fuel 16/1450 15/1400 15/1300 14/1250 13/1200 13/1150 12/1100 11/100010/900 9/800 8/750Dist/TAS 84/356 79/356 75/355 70/355 67/355 63/354 59/354 53/353 48/353 42/353 38/35227000 Time/Fuel 15/1400 14/1350 14/1250 13/1200 12/1150 12/1100 11/1050 10/950 9/850 8/800 8/700Dist/TAS 77/352 73/351 69/351 65/351 61/350 58/350 55/1350 49/349 44/349 39/34935/34826000 Time/Fuel 14/1350 14/1250 13/1200 12/1150 12/1100 11/1050 11/1000 10/900 9/850 8/750 7/700Dist/TAS 71/348 67/347 63/347 60/347 57/347 54/346 51/346 46/346 41/345 37/345 3

3/34525000 Time/Fuel 13/1300 13/1200 12/1150 12/1100 11/1050 11/1000 10/950 9/900 8/800 8/750 7/650Dist/TAS 65/344 61/343 58/343 55/343 52/343 50/343 47/342 42/342 38/342 34/342 30/34124000 Time/Fuel 13/1200 12/1150 11/1100 11/1050 10/1000 10/950 10/950 9/850 8 /750 7/700 6/650Dist/TAS 60/340 56/340 54/340 51/339 48/339 46/339 43/339 39/339 35/338 32/338 28/33823000 Time/Fuel 12/1150 11/1100 11/1050 10/1000 10/1000 9 / 950 9/900 8/800 7/750 7/700 6/600Dist/TAS 55/336 52/336 49/336 47/336 44/336 42/335 40/335 36/335 33/335 29/335 26/335

22000 Time/Fuel 11/1100 11/1050 10/1000 10/1000 9/950 9/900 9/850 8/800 7/700 6/650 6/600Dist/TAS 50/333 48/333 45/333 43/332 41/332 39/332 37/332 33/332 30/332 27/332 24/33121000 Time/Fuel 10/1050 10/1000 10/1000 9/950 9/900 8/850 8/800 7/750 7/700 6/650 6/550Dist/TAS 46/330 44/329 42/329 40/329 38/329 36/329 34/329 31/329 28/328 25/328 22/32820000 Time/Fuel 10/1000 9/950 9/950 9/900 8/850 8/800 8/800 7/700 6/650 6/600 5/550Dist/TAS 42/326 40/326 38/326 36/326 35/326 33/326 31/326 28/326 26/325 23/325 21/32519000 Time/fuel 9/950 9/950 8/900 8/850 8/800 7/800 7/750 7/700 6/650 6/600 5/50

0Dist/TAS 39/323 37/323 35/323 33/323 32/323 30/323 29/323 26/323 24/322 21/322 19/32218000 Time/Fuel 9/900 8/900 8/850 8/800 7/800 7/750 7/700 6/650 6/600 5/550 5/500Dist/TAS 35/320 34/320 32/320 31/320 29/320 28/320 26/320 24/320 22/320 19/319 17/31917000 Time/Fuel 8/900 8/850 8/800 7/800 7/750 7/700 6/700 6/650 5/600 5/550 5/500Dist/TAS 32/317 31/317 29/317 28/317 27/317 25/317 24/317 22/317 20/317 18/317 1



6/31716000 Time/Fuel 8/850 7/800 7/750 7/750 7/700 6/700 6/650 6/600 5/550 5/500 4/450Dist/TAS 29/314 28/314 27/314 25/314 24/314 23/314 22/314 20/314 18/314 16/314 15/31415000 Time/Fuel 7/800 7/750 7/750 6/700 6/700 6/650 6/650 5/600 5/550 4/500 4/450Dist/TAS 26/312 25/312 24/312 23/311 22/311 21/311 20/311 18/311 16/311 15/311 13/31114000 Time/Fuel 7/750 6/700 6/700 6/650 6/650 6/600 5/600 5/550 5/500 4/450 4/400Dist/TAS 24/309 23/309 22/309 21/309 20/309 19/309 18/309 16/309 15/309 13/309 12/30913000 Time/Fuel 6/700 6/700 6/650 6/650 5/600 5/600 5/550 5/500 4/500 4/450 4/400Dist/TAS 21/306 20/306 19/306 19/306 18/306 17/306 16/306 15/306 13/306 12/306 11/30612000 Time/Fuel 6/650 6/650 5/600 5/600 5/600 5/550 5/550 4/500 4/450 4/400 3/400Dist/TAS 19/304 18/304 17/304 17/304 16/304 15/304 14/304 13/304 12/304 11/304 10/30411000 Time/Fuel 5/650 5/600 5/600 5/550 5/550 5/500 4/500 4/450 4/450 3/400 3/350Dist/TAS 17/301 16/301 15/301 15/301 14/301 13/301 13/301 12/301 11/301 10/301 9

/30110000 Time/Fuel 5/600 5/550 5/550 5/550 4/500 4/500 4/500 4/450 4/400 3/350 3/350Dist/TAS 15/299 14/299 13/299 13/299 12/299 12/299 11/299 10/299 9/299 8/299 7/2998000 Time/Fuel 4/500 4/500 4/500 4/450 4/450 4/450 3/400 3/400 3/350 3/350 3/300 Dist/TAS 11/294 10/294 10/294 9/294 9/294 9/294 8/294 7/294 7/294 6/294 6/2946000 Time/Fuel 4/450 3/400 3/400 3/400 3/400 3/350 3/350 3/350 3/300 2/300 2/250 Dist/TAS 7/290 7/290 6/290 6/290 6/290 6/290 5/290 5/290 5/290 4/290 4/2901500 Time/Fuel 2/250 2/250 2/250 2/250 2/250 2/250 2/250 2/200 2/200 2/200 1/150

Fuel Adjustment for high elevation airportsEffect on time and distance is negligible Fuel Adjustment -50 -100 -150En-route Climb 280/.742000 4000 6000 8000 10000 12000-250 -300 -350Airport ElevationFIGURE 033-22

033 PICTURE SUPPLEMENTS113© 2008AVIATIONEXAM.comISA +6°C TO +15°C

Press.Alt.ftUnitsMin/kg.NAM/KtBRAKE RELEASE WEIGHT KG68000 66000 64000 62000 60000 58000 56000 52000 48000 44000 400000 0 0 1 / 2 1 0 5 1 1 / 4 1 0 0 3 1 / 6 1 0 0 5 1 / 8 1 0 0 7 1 / 2 2 0 5 8 1 /4 2 0 0 0 2 / 7 2 0 5 3 2 / 3 3 l e u F / e mi T 0 0 0 7 3



3 9 3 / 2 7 4 9 3 / 2 8 6 9 3 / 5 9 7 9 3 / 1 1 1 0 0 4 / 2 3 1 2 0 4 / 7 4 1 40 4 / 9 6 1 9 0 4 / 2 1 2 S A T / t s i D0 0 0 1 / 2 1 0 0 1 1 / 3 1 0 5 2 1 / 5 1 0 0 4 1 / 7 1 0 0 6 1 / 0 2 0 0 7 1 /1 2 0 5 6 1 / 3 2 0 0 0 2 / 6 2 0 5 2 2 / 0 3 l e u F / e mi T 0 0 0 6 31 9 3 / 8 6 2 9 3 / 7 7 3 9 3 / 9 8 5 9 3 / 2 0 1 7 9 3 / 9 1 1 8 9 3 / 0 3 1 00 4 / 3 4 1 2 0 4 / 1 6 1 5 0 4 / 9 8 1 S A T / t s i D35000 Time/Fuel 35/2600 29/2250 26/2050 23/1900 21/1750 20/1650 19/1550 16/135014/1200 13/1100 11/950Dist/TAS 224/407 180/402 157/399 141/397 129/396 119/395 110/394 95/392 83/391 73/390 64/38934000 Time/Fuel 28/2250 25/2050 23/1900 21/1800 20/1650 19/1550 18/1500 16/130014/1200 12/1050 11/950Dist/TAS 173/400 154/397 140/395 128/394 118/393 110/392 102/391 89/389 78/388 69/387 61/38633000 Time/Fuel 25/2100 23/1950 21/1800 20/1700 19/1600 18/1500 17/1450 15/130013/1150 12/1050 10/900Dist/TAS 151/394 138/393 127/391 118/390 109/389 102/388 95/388 84/386 74/385 65/385 58/38432000 Time/Fuel 23/1950 21/1850 20/1750 19/1650 18/1550 17/1450 16/1400 14/125013/1100 11/1000 10/900Dist/TAS 136/390 126/389 117/388 109/387 102/386 95/385 89/384 79/383 70/383 62/382 55/38131000 Time/Fuel 22/1850 20/1750 19/1650 18/1550 17/1500 16/1400 15/1350 13/120012/1100 11/1000 10/900

Dist/TAS 125/386 116/385 108/384 101/383 95/382 89/382 84/381 74/380 66/380 59/379 52/37830000 Time/Fuel 20/1800 19/1700 18/1600 17/1500 16/1450 15/1350 14/1300 13/115012/1050 10/950 9/850Dist/TAS 115/382 108/381 101/380 .95/379 89/379 84/378 77/378 70/377 62/376 56/376 49/37529000 Time/Fuel 19/1700 18/1600 17/1550 16/1450 15/1400 14/1300 14/1250 12/115011/1000 10/900 9/850Dist/TAS 105/376 98/376 92/375 87/374 82/374 77/374 73/373 65/373 58/372 52/37246/37128000 Time/Fuel 17/1600 17/1550 16/1450 15/1400 14/1300 13/1250 13/1200 12/110010/1000 9/900 8/800Dist/TAS 95/371 90/371 84/370 80/370 75/369 71/369 67/369 60/368 54/368 48/367 4

2/36727000 Time/Fuel 16/1550 15/1450 15/1400 14/1350 13/1250 13/1200 12/1150 11/105010/950 9/850 8/750Dist/TAS 87/366 82/366 77/366 73/365 69/365 66/365 62/364 56/364 50/363 44/363 39/36326000 Time/Fuel 15/1450 15/1400 14/1350 13/1250 13/1200 12/1150 11/1100 10/10009/900 8/800 8/750Dist/TAS 80/362 75/362 71/361 67/361 64/361 60/360 57/360 51/360 46/359 41/359 37/35925000 Time/Fuel 14/1400 14/1350 13/1250 12/1200 12/1150 11/1100 11/1050 10/950 9/850 8/800 7/700Dist/TAS 73/356 69/357 65/357 62/'357 59/367 56/356 53/356 47/356 43/356 38/35534/355

24000 Time/Fuel 13/1350 13/1250 12/1200 12/1150 11/1100 11/1050 10/1000 9/900 8/850 8/750 7/700Dist/TAS 67/354 63/353 60/353 57/353 54/353 51/353 49/352 44/352 39/352 35/352 32/35123000 Time/Fuel 13/1250 12/1200 11/1150 11/1100 10/1050 10/1000 10/950 9/900 8/800 7/750 7/650Dist/TAS 61/350 58/350 55/349 53/349 50/349 47/349 45/349 41/348 37/348 33/348 29/34822000 Time/Fuel 12/1200 11/1150 11/1100 10/1050 10/1000 9/950 9/950 8/850 8/7507/700 6/650



Dist/TAS 56/346 54/346 51/346 48/346 46/345 44/345 42/345 37/345 34/345 30/345 27/34421000 Time/Fuel 11/1150 11/1100 10/1050 10/1000 9/950 9/950 9/900 8/800 7/750 6/700 6/600Dist/TAS 52/343 49/342 47/342 44/342 42/342 40/342 38/342 35/342 31/341 28/341 25/34120000 Time/Fuel 10/1100 10/1050 10/1000 9/950 9/950 8/900 8/850 7/800 7/700 6/650 6/600Dist/TAS 47/339 45/339 43/339 41/339 39/339 37/338 35/338 32/338 29/338 26/338 23/33819000 Time/Fuel 10/1050 9/1000 9/950 9/950 8/900 8/850 8/800 7/750 6/700 6/600 5/550Dist/TAS 43/336 41/336 39/335 37/335 36/335 34/335 32/335 29/335 26/335 24/335 21/33518000 Time/Fuel 9/1000 9/950 8/900 8/900 8/850 7/800 7/800 7/700 6/650 6/600 5/550Dist/TAS 39/332 38/332 36/332 34/332 33/332 31/332 30/332 27/332 24/332 22/332 19/33217000 Time/Fuel 9/950 8/900 8/900 8/850 7/800 7/750 7/750 6/700 6/600 5/550 5/500Dist/TAS 36/329 34/329 33/329 31/329 30/329 28/329 27/329 24/329 22/329 20/329 18/32916000 Time/Fuel 8/900 8/850 7/850 7/800 7/750 7/750 6/700 6/650 5/600 5/550 4/500

Dist/TAS 33/326 31/326 30/326 28/326 27/326 26/326 25/326 22/326 20/326 18/326 16/32615000 Time/Fuel 8/850 7/800 7/800 7/750 6/750 6/700 6/650 5/600 5/550 5/500 4/450Dist/TAS 29/323 28/323 27/323 26/323 24/323 23/323 22/323 20/323 18/323 16/323 15/32314000 Time/Fuel 7/800 7/800 7/750 6/700 6/700 6/650 6/650 5/600 5/550 4/500 4/450Dist/TAS 26/321 25/321 24/321 23/320 22/320 21/320 20/320 18/320 17/320 15/320 13/32013000 Time/Fuel 7/750 6/750 6/700 6/700 6/650 5/650 5/600 5/550 4/500 4/450 4/450Dist/TAS 24/318 23/318 22/318 21/318 20/318 19/318 18/318 16/318 15/318 13/318 1

2/31812000 Time/Fuel 6/700 6/700 6/650 5/650 5/600 5/600 5/550 5/500 4/500 4/450 4/400Dist/TAS 21/315 20/315 19/315 18/315 18/315 17/315 16/315 15/315 13/315 12/315 11/31511000 Time/Fuel 6/650 5/650 5/600 5/600 5/600 5/550 5/550 4/500 4/450 4/400 3/400Dist/TAS 19/313 18/313 17/313 16/313 16/313 15/312 14/312 13/312 12/312 11/312 9/31210000 Time/Fuel 5/600 5/600 5/600 5/550 5/550 4/500 4/500 4/450 4/450 3/400 3/350Dist/TAS 16/310 16/310 15/310 14/310 14/310 13/310 12/310 11/310 10/310 9/310 8/310

8000 Time/Fuel 4/550 4/500 4/500 4/500 4/450 4/450 4/450 3/400 3/350 3/350 3/300 Dist/TAS 12/305 11/305 11/305 10/305 10/305 10/305 9/305 8/305 8/305 7/305 6/305 6000 Time/Fuel 4/450 4/450 3/400 3/400 3/400 3/400 3/350 3/350 3/300 2/300 2/250 Dist/TAS 8/301 8/301 7/301 7/301 7/301 6/301 6/301 6/301 5/301 5/301 4/3011500 Time/Fuel 2/250 2/250 2/250 2/250 2/250 2/250 2/250 2/200 2/200 2/200 1/150 Fuel Adjustment for high elevation airports



Effect on time and distance is negligible Fuel Adjustment -50 -100 -200En-route Climb 280/.746000 8000 10000 12000 2000 4000-250 -300 -400Airport ElevationFIGURE 033-23

033 PICTURE SUPPLEMENTS114© 2008AVIATIONEXAM.comISA +16°C TO +25°CPress.Alt.ftUnitsMin/kg.NAM/KtBRAKE RELEASE WEIGHT KG68000 66000 64000 62000 60000 58000 56000 52000 48000 44000 400000 5 1 1 / 5 1 0 0 3 1 / 7 1 0 5 4 1 / 9 1 0 5 6 1 / 2 2 0 5 9 1 / 7 2 0 5 1 2 /1 3 0 5 5 2 / 7 3 l e u F / e mi T 0 0 0 7 32 0 4 / 8 8 3 0 4 / 1 0 1 5 0 4 / 8 1 1 7 0 4 / 0 4 1 0 1 4 / 2 7 1 3 1 4 / 8 91 7 1 4 / 6 4 2 S A T / t s i D

0 0 1 1 / 4 1 0 5 2 1 / 6 1 0 0 4 1 / 8 1 0 0 6 1 / 1 2 0 5 8 1 / 4 2 0 0 0 2 /7 2 0 0 2 2 / 0 3 0 5 4 2 / 5 3 l e u F / e mi T 0 0 0 6 39 9 3 / 2 8 0 0 4 / 5 9 2 0 4 / 0 1 1 4 0 4 / 8 2 1 6 0 4 / 3 5 1 8 0 4 / 0 7 11 1 4 / 2 9 1 4 1 4 / 7 2 2 S A T / t s i D35000 Time/Fuel 42/2950 34/2500 30/2200 27/2050 25/1900 23/1750 20/1550 17/135015/1200 13/1050Dist/TAS 281/418 220/412 190/409 169/406 153/405 140/403 119/401 103/399 90/39878/39734000 Time/Fuel 40/2850 34/2500 30/2250 27/2100 25/1950 23/1800 21/1700 19/150016/1300 14/1150 13/1050Dist/TAS 260/414 215/409 188/406 169/404 153/403 141/401 130/400 112/398 97/39785/396 74/39533000 Time/Fuel 33/2500 30/2300 27/2100 25/1950 23/1850 21/1700 20/1600 18/1450

16/1300 14/1150 12/1000Dist/TAS 210/407 186/404 168/402 153/400 141/399 130/398 121/397 105/395 92/39480/393 70/39232000 Time/Fuel 30/2350 27/2150 25/2000 23/1900 22/1750 20/1650 19/1550 17/140015/1250 13/1100 12/1000Dist/TAS 185/401 167/399 153/398 141/396 130/395 121/394 113/394 98/392 86/391 76/390 67/38931000 Time/Fuel 27/2200 25/2050 23/1900 22/1800 20/1700 19/1600 18/1500 16/135014/1200 13/1100 11/950Dist/TAS 166/396 152/395 141/394 130/393 121/392 113/391 106/390 93/389 82/388 72/387 63/38730000 Time/Fuel 25/2100 24/1950 22/1850 21/1750 19/1650 18/1550 17/1450 15/130014/1150 12/1050 11/950

Dist/TAS 152/392 140/391 130/389 121/389 113/388 106/387 99/387 87/385 77/385 68/384 60/38329000 Time/Fuel 23/1950 22/1850 20/1750 19/1650 18/1550 17/1450 16/1400 14/125013/1100 12/1000 10/900Dist/TAS 136/386 126/385 118/384 110/383 106/383 97/382 91/382 80/381 71/380 63/379 56/37928000 Time/Fuel 21/1850 20/1750 19/1650 18/1550 17/1500 16/1400 15/1350 14/120012/1100 11/950 10/850Dist/TAS 123/380 114/379 107/379 100/378 94/378 89/377 83/377 74/376 66/375 58/375 52/375



27000 Time/Fuel 20/1750 19/1650 18/1550 17/1500 16/1400 15/1350 14/1250 13/115011/1050 10/950 9/850Dist/TAS 111/375 104/374 98/374 92/373 86/373 81/372 77/372 68/371 61/371 54/371 48/37026000 Time/Fuel 18/1650 17/1550 16/1500 16/1400 15/1350 14/1300 13/1200 12/110011/1000 10/900 9/800Dist/TAS 101/370 95/370 89/369 84/369 79/368 75/368 70/368 63/367 56/367 50/36644/36625000 Time/Fuel 17/1550 16/1500 15/1400 15/1350 14/1300 13/1200 13/1150 11/105010/950 9/850 8/750Dist/TAS 92/365 86/365 81/365 77/364 73/364 69/364 65/363 58/363 52/363 46/362 41/36224000 Time/Fuel 16/1500 15/1400 14/1350 14/1300 13/1200 12/1150 12/1100 11/100010/900 9/850 8/750Dist/TAS 84/361 79/361 75/360 70/360 67/360 63/360 60/359 53/359 48/359 43/358 38/35823000 Time/Fuel 15/1400 14/1350 13/1300 13/1250 12/1150 12/1100 11/1050 10/950 9/900 8/800 7/700Dist/TAS 77/357 72/357 68/356 65/356 61/356 58/356 55/356 49/355 44/355 39/355 35/35522000 Time/Fuel 14/1350 13/1300 13/1250 12/1150 11/1100 11/1050 10/1000 9/900 9/850 8/750 7/700Dist/TAS 70/353 66/353 63/352 59/352 56/352 53/352 50/352 45/351 41/351 36/351 32/351

21000 Time/Fuel 13/1300 12/1200 12/1150 11/1100 11/1050 10/1000 10/950 9/900 8/800 7/750 7/650Dist/TAS 64/349 60/349 57/349 54/349 52/348 49/348 46/348 42/348 37/348 34/348 30/34720000 Time/Fuel 12/1200 12/1150 11/1100 11/1050 10/1000 10/950 9/950 8/850 8/750 7/700 6/650Dist/TAS 58/345 55/345 52/345 50/345 47/345 45/345 43/345 38/344 34/344 31/344 28/34419000 Time/Fuel 11/1150 11/1100 10/1050 10/1000 9/950 9/900 9/900 8/800 7/750 7/650 6/600Dist/TAS 53/342 50/342 48/342 45/342 43/342 41/341 39/341 35/341 32/341 28/341 25/34118000 Time/Fuel 11/1100 10/1050 10/1000 9/950 9/900 9/900 8/850 7/750 7/700 6/65

0 6/600Dist/TAS 48/339 46/339 44/338 42/338 39/338 38/338 36/338 32/338 29/338 26/338 23/33817000 Time/Fuel 10/1050 10/1000 9/950 9/900 8/850 8/850 8/800 7/750 6/650 6/6005/550Dist/TAS 44/335 42/335 40/335 38/335 36/335 34/335 33/335 29/335 27/335 24/335 21/33516000 Time/Fuel 9/1000 9/950 9/900 8/850 8/850 7/800 7/750 7/700 6/650 5/600 5/550Dist/TAS 40/332 38/332 36/332 34/332 33/332 31/332 30/332 27/332 24/332 22/332 19/33215000 Time/Fuel 9/950 8/900 8/850 8/800 7/800 7/750 7/700 6/650 6/600 5/550 5/500

Dist/TAS 36/329 34/329 33/329 31/329 30/329 28/329 27/329 24/329 22/329 20/329 18/32914000 Time/Fuel 8/850 8/650 7/800 7/750 7/750 7/700 6/700 6/650 5/550 5/500 4/500Dist/TAS 32/326 31/326 29/326 28/326 27/326 25/326 24/326 22/326 20/326 18/326 16/32613000 Time/Fuel 7/800 7/800 7/750 7/750 6/700 6/650 6/650 5/600 5/550 5/500 4/450Dist/TAS 29/323 28/323 26/323 25/323 24/323 23/323 22/323 20/323 18/323 16/323 14/323



12000 Time/Fuel 7/750 7/750 6/700 6/700 6/650 6/650 5/600 5/550 5/500 4/450 4/450Dist/TAS 26/321 25/321 23/321 22/321 21/321 20/321 19/321 18/321 16/320 14/320 13/32011000 Time/Fuel 6/700 6/700 6/650 6/650 5/600 5/600 5/550 5/500 4/500 4/450 4/400Dist/TAS 23/318 22/318 21/318 20/318 19/318 18/318 17/318 16/318 14/318 13/318 11/31810000 Time/Fuel 6/650 6/650 5/600 5/600 5/550 5/550 5/550 4/500 4/450 4/400 3/400Dist/TAS 20/315 19/315 18/315 17/315 16/315 16/315 15/315 14/315 12/315 11/315 10/3158000 Time/Fuel 5/550 5/550 5/550 4/500 4/500 4/500 4/450 4/400 3/400 3/350 3/350 Dist/TAS 14/310 14/310 13/310 13/310 12/310 11/310 11/310 10/310 9/310 8/310 7/3106000 Time/Fuel 4/450 4/450 4/450 4/450 3/400 3/400 3/400 3/350 3/350 3/300 2/300 Dist/TAS 10/306 9/306 9/306 8/306 8/306 8/306 7/306 7/306 6/306 5/306 5/3061500 Time/Fuel 2/250 2/250 2/250 2/250 2/250 2/250 2/250 2/200 2/200 2/200 1/150 Fuel Adjustment for high elevation airportsEffect on time and distance is negligible Fuel Adjustment -50 -150 -200 -300En-route Climb 280/.74

-350 -400Airport Elevation 2000 4000 6000 8000 10000 12000FIGURE 033-24

033 PICTURE SUPPLEMENTS115© 2008AVIATIONEXAM.comWind Range Correction Graph300400500600

0100200300400500600700800HEADWIND TAILWINDGROUND DISTANCE NM700800

600500450400350300250200150100



5015020010050050100150200WINDVELOCITYktM A N E C N A T S I D R I A t k S A T E S I U R C E G A R E V AFIGURE 033-25

033 PICTURE SUPPLEMENTS116© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 28,000 ft LONG RANGE CRUISEGROSS 0 100 200 300 400 500 600 700 800 900WT. kg TAS CRUISE DISTANCE NAUTICAL AIR MILES

35000 376 0 20 41 62 83 104 125 145 166 18736000 380 208 229 249 270 290 311 332 352 373 39337000 384 414 434 455 475 495 516 536 557 577 59738000 388 618 638 658 678 698 718 738 759 779 79939000 392 819 839 859 879 898 918 938 958 978 99840000 396 1018 1037 1057 1077 1096 1116 1136 1155 1175 119541000 399 1214 1234 1253 1273 1292 1312 1331 1350 1370 138942000 403 1409 1428 1447 1466 1486 1505 1524 1543 1563 158243000 406 1601 1620 1639 1658 1677 1696 1715 1734 1753 177244000 409 1791 1810 1829 1848 1866 1885 1904 1923 1942 196045000 413 1979 1998 2016 2035 2054 2072 2091 2109 2128 214746000 416 2165 2184 2202 2220 2239 2257 2275 2294 2312 233147000 419 2349 2367 2385 2404 2422 2440 2458 2476 2495 2513

48000 422 2531 2549 2567 2585 2603 2621 2639 2657 2675 269349000 425 2711 2729 2747 2764 2782 2800 2818 2836 2853 287150000 427 2889 2907 2924 2942 2960 2977 2995 3013 3030 304851000 429 3065 3083 3100 3118 3135 3153 3170 3188 3205 322252000 432 3240 3257 3274 3292 3309 3326 3344 3361 3378 339553000 434 3413 3430 3447 3464 3481 3498 3515 3532 3549 356754000 436 3584 3601 3617 3634 3651 3668 3685 3702 3719 373655000 437 3753 3770 3786 3803 3820 3837 3853 3870 3887 390456000 439 3920 3937 3953 3970 3987 4003 4020 4036 4053 406957000 440 4086 4102 4119 4135 4152 4168 4184 4201 4217 423458000 441 4250 4266 4282 4299 4315 4331 4347 4364 4380 439659000 442 4412 4428 4444 4460 4476 4492 4509 4525 4541 455760000 442 4573 4589 4605 4620 4636 4652 4668 4684 4700 4716

61000 442 4732 4747 4763 4779 4795 4810 4826 4842 4858 487362000 442 4889 4905 4920 4936 4951 4967 4983 4998 5014 502963000 443 5045 5060 5076 5091 5106 5122 5137 5153 5168 518464000 443 5199 5214 5229 5245 5260 5275 5290 5306 5321 533665000 443 5351 5367 5382 5397 5412 5427 5442 5457 5472 548766000 443 5502 5517 5532 5547 5562 5577 5592 5607 5622 563767000 443 5652 5666 5681 5696 5711 5725 5740 5755 5770 5784NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMITA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMITB) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMIT



C) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMITNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISALong Range Cruise Pressure Altitude 28,000 ftFIGURE 033-26

033 PICTURE SUPPLEMENTS117© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 33,000 ft LONG RANGE CRUISEGROSS 0 100 200 300 400 500 600 700 800 900WT. kg TAS CRUISE DISTANCE NAUTICAL AIR MILES35000 400 0 23 46 69 92 115 138 161 184 20736000 405 230 252 275 298 320 343 366 389 411 43437000 408 457 479 502 524 547 569 591 614 636 65938000 412 681 703 725 747 770 792 814 836 858 88039000 415 902 924 946 968 990 1012 1034 1055 1077 109940000 419 1121 1143 1164 1186 1207 1229 1251 1272 1294 131541000 421 1337 1358 1380 1401 1422 1444 1465 1486 1508 1529

42000 424 1550 1571 1593 1614 1635 1656 1677 1698 1719 174043000 426 1761 1782 1803 1823 1844 1865 1886 1907 1928 194844000 428 1969 1990 2010 2031 2051 2072 2092 2113 2134 215445000 430 2175 2195 2215 2235 2256 2276 2296 2317 2337 235746000 432 2377 2397 2417 2437 2458 2478 2498 2518 2538 255847000 433 2578 2597 2617 2637 2657 2677 2696 2716 2736 275648000 433 2775 2795 2814 2834 2854 2873 2893 2912 2932 295149000 433 2971 2990 3009 3029 3048 3067 3087 3106 3125 314450000 433 3164 3183 3202 3221 3240 3259 3278 3297 3316 333551000 433 3354 3373 3392 3411 3429 3448 3467 3486 3505 352352000 433 3542 3561 3579 3598 3617 3635 3654 3672 3691 370953000 433 3728 3746 3765 3783 3801 3819 3838 3856 3874 389354000 433 3911 3929 3947 3965 3983 4001 4019 4038 4056 4074

55000 433 4092 4110 4127 4145 4163 4181 4199 4216 4234 425256000 433 4270 4287 4305 4323 4340 4358 4375 4393 4410 442857000 433 4445 4463 4480 4497 4515 4532 4549 4567 4584 460158000 433 4619 4636 4653 4670 4687 4704 4721 4738 4755 477259000 433 4789 4806 4823 4840 4856 4873 4890 4907 4924 494060000 433 4957 4974 4990 5007 5024 5040 5057 5073 5090 510661000 433 5123 5139 5155 5172 5188 5204 5221 5237 5253 527062000 433 5286 5302 5318 5334 5350 5366 5382 5398 5414 543063000 433 5446 5462 5478 5493 5509 5525 5541 5557 5572 558864000 433 5604 5619 5635 5650 5666 5681 5697 5712 57,28 574365000 433 5759 5774 5789 5804 5820 5835 5850 5865 5880 589666000 433 5911 5926 5941 5956 5970 5985 6000 6015 6030 604567000 433 6060 6075 6089 6104 6118 6133 6148 6162 6177 6191

NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 58,200 kgA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMITB) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMITC) THRUST LIMITED WEIGHT FOR ISA +20 IS 66,400 kgNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISALong Range Cruise Pressure Altitude 33,000 ft



FIGURE 033-27

033 PICTURE SUPPLEMENTS118© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 34,000 ft LONG RANGE CRUISEGROSS 0 100 200 300 400 500 600 700 800 900WT. kg TAS CRUISE DISTANCE NAUTICAL AIR MILES35000 405 0 23 46 70 93 117 140 164 187 21036000 409 234 257 280 303 326 350 373 396 419 44237000 413 465 488 511 534 557 579 602 625 648 67138000 416 694 716 739 761 784 806 829 851 874 89639000 419 919 941 963 986 1008 1030 1053 1075 1097 111940000 422 1142 1164 1186 1207 1229 1251 1273 1295 1317 133941000 424 1361 1383 1405 1426 1448 1470 1492 1513 1535 155742000 427 1578 1600 1621 1643 1664 1685 1707 1728 1750 177143000 428 1792 1814 1835 1856 1877 1898 1919 1940 1961 198344000 430 2004 2025 2045 2066 2087 2108 2129 2150 2171 219145000 431 2212 2233 2253 2274 2295 2315 2336 2356 2377 239846000 431 2418 2438 2459 2479 2499 2520 2540 2560 2581 260147000 431 2621 2641 2661 2682 2702 2722 2742 2762 2782 280248000 431 2822 2842 2862 2881 2901 2921 2941 2960 2980 3000

49000 431 3020 3039 3059 3078 3098 3118 3137 3157 3176 319650000 431 3215 3234 3254 3273 3292 3311 3331 3350 3369 338951000 431 3408 3427 3446 3465 3484 3503 3522 3541 3560 357952000 431 3598 3616 3635 3654 3673 3691 3710 3729 3747 376653000 431 3785 3803 3822 3840 3859 3877 3896 3914 3932 395154000 431 3969 3987 4006 4024 4042 4060 4078 4096 4115 413355000 431 4151 4169 4187 4205 4223 4240 4258 4276 4294 431256000 431 4330 4348 4365 4383 4400 4418 4436 4453 4471 448957000 431 4506 4524 4541 4558 4576 4593 4610 4628 4645 466258000 431 4680 4697 4714 4731 4748 4765 4782 4799 4816 483359000 431 4851 4867 4884 4901 4918 4934 4951 4968 4985 500260000 431 5018 5035 5051 5068 5084 5101 5117 5134 5150 516761000 431 5183 5200 5216 5232 5248 5264 5281 5297 5313 5329

62000 431 5345 5361 5377 5393 5409 5425 5441 5457 5472 548863000 431 5504 5520 5535 5551 5566 5582 5598 5613 5629 564464000 431 5660 5675 5690 5706 5721 5736 5751 5766 5782 579765000 430 5812 5827 5842 5857 5872 5886 5901 5916 5931 594666000 430 5961 5975 5990 6004 6019 6033 6048 6062 6077 609167000 430 6106 6120 6134 6148 6162 6176 6190 6204 6219 6233NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 55,500 kgA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER IS 67,100 kgB) THRUST LIMITED WEIGHT FOR ISA +15 IS 65,700 kgC) THRUST LIMITED WEIGHT FOR ISA +20 IS 64,000 kgNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISA

C) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISALong Range Cruise Pressure Altitude 34,000 ftFIGURE 033-28

033 PICTURE SUPPLEMENTS119© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C Auto



PRESSURE ALTITUDE 35,000 ft LONG RANGE CRUISEGROSS 0 100 200 300 400 500 600 700 800 900WT. kg TAS CRUISE DISTANCE NAUTICAL AIR MILES35000 410 0 23 47 71 95 119 143 167 191 21436000 414 238 262 285 309 333 356 380 403 427 45037000 417 474 497 521 544 567 590 614 637 660 68338000 420 707 730 753 776 798 821 844 867 890 91339000 422 936 959 982 1004 1027 1050 1072 1095 1117 114040000 425 1163 1185 1207 1230 1252 1275 1297 1319 1342 136441000 426 1386 1408 1430 1452 1474 1496 1519 1541 1563 158542000 428 1607 1628 1650 1672 1694 1715 1737 1759 1781 180243000 429 1824 1845 1867 1888 1910 1931 1953 1974 1996 201744000 429 2039 2060 2081 2102 2123 2144 2165 2187 2208 222945000 429 2250 2271 2292 2313 2334 2355 2375 2396 2417 243846000 429 2459 2480 2500 2521 2541 2562 2582 2603 2624 264447000 429 2665 2685 2705 2726 2746 2766 2787 2807 2827 284848000 429 2868 2888 2908 2928 2948 2968 2988 3008 3028 304849000 429 3068 3088 3107 3127 3147 3166 3186 3206 3226 324550000 429 3265 3284 3304 3323 3343 3362 3381 3401 3420 344051000 429 3459 3478 3497 3516 3536 3555 3574 3593 3612 363152000 429 3650 3669 3688 3707 3726 3744 3763 3782 3801 382053000 429 3838 3857 3875 3894 3913 3931 3950 3968 3987 400554000 429 4024 4042 4060 4078 4097 4115 4133 4151 4170 418855000 430 4206 4224 4242 4260 4278 4296 4314 4331 4349 4367

56000 430 4385 4403 4420 4438 4456 4473 4491 4509 4526 454457000 430 4561 4579 4596 4613 4631 4648 4665 4682 4700 471758000 429 4734 4751 4768 4785 4802 4819 4836 4853 4870 488759000 429 4904 4921 4937 4954 4971 4987 5004 5021 5037 505460000 429 5070 5087 5103 5119 5136 5152 5168 5184 5201 521761000 429 5233 5249 5265 5281 5297 5313 5329 5345 5361 537762000 429 5393 5408 5424 5439 5455 5470 5486 5501 5517 553263000 428 5548 5563 5578 5593 5608 5623 5638 5654 5669 568464000 428 5699 5714 5728 5743 5758 5772 5787 5802 5817 583165000 427 5846 5860 5874 5889 5903 5917 5932 5946 5960 5974NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 53,000 kgA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER IS 64,500 kgB) THRUST LIMITED WEIGHT FOR ISA +15 IS 63,100 kg

C) THRUST LIMITED WEIGHT FOR ISA +20 IS 61,600 kgNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISALong Range Cruise Pressure Altitude 35,000 ftFIGURE 033-29

033 PICTURE SUPPLEMENTS120© 2008AVIATIONEXAM.com

All Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 24,000 ft MACH 0.74 CRUISE TAS 447 ktGROSS 0 100 200 300 400 500 600 700 800 900WT. kg CRUISE DISTANCE NAUTICAL AIR MILES35000 0 16 33 49 66 83 99 116 133 14936000 166 183 199 216 232 249 266 282 299 31537000 332 349 365 382 398 415 431 448 465 48138000 498 514 531 547 564 580 597 613 630 64639000 663 679 696 712 729 745 762 778 795 81140000 828 844 860 877 893 910 926 942 959 975



41000 992 1008 1024 1041 1057 1074 1090 1106 1123 113942000 1155 1172 1188 1204 1221 1237 1253 1269 1286 130243000 1318 1335 1351 1367 1383 1399 1416 1432 1448 146444000 1481 1497 1513 1529 1545 1561 1578 1594 1610 162645000 1642 1658 1675 1691 1707 1723 1739 1755 1771 178746000 1803 1819 1835 1851 1867 1883 1899 1915 1932 194847000 1964 1980 1995 2011 2027 2043 2059 2075 2091 210748000 2123 2139 2155 2171 2187 2202 2218 2234 2250 226649000 2282 2298 2313 2329 2345 2361 2377 2392 2408 242450000 2440 2455 2471 2487 2503 2518 2534 2550 2565 258151000 2597 2612 2628 2644 2659 2675 2691 2706 2722 273752000 2753 2769 2784 2800 2815 2831 2846 2862 2877 289353000 2908 2924 2939 2955 2970 2986 3001 3017 3032 304754000 3063 3078 3094 3109 3124 3140 3155 3170 3186 320155000 3216 3232 3247 3262 3277 3293 3308 3323 3338 335456000 3369 3384 3399 3414 3430 3445 3460 3475 3490 350657000 3521 3536 3551 3566 3581 3596 3611 3626 3641 365658000 3671 3686 3701 3716 3731 3746 3761 3776 3791 380659000 3821 3836 3851 3866 3881 3896 3910 3925 3940 399560000 3970 3985 4000 4014 4029 4044 4059 4073 4088 410361000 4118 4132 4147 4162 4176 4191 4206 4220 4235 425062000 4264 4279 4294 4308 4323 4337 4352 4366 4381 439663000 4410 4425 4439 4454 4468 4483 4497 4511 4526 454064000 4555 4569 4584 4598 4612 4627 4641 4655 4670 4684

65000 4698 4713 4727 4741 4756 4770 4784 4798 4813 482766000 4841 4855 4869 4884 4898 4912 4926 4940 4954 496867000 4983 4997 5011 5025 5039 5053 5067 5081 5095 5109NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMITA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMITB) THRUST LIMITED WEIGHT FOR IS A +15 EXCEEDS STRUCTURAL LIMITC) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMITNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISAMach 0.74 Cruise Pressure Altitude 24,000 ft

FIGURE 033-30

033 PICTURE SUPPLEMENTS121© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 25,000 ft MACH 0.74 CRUISE TAS 445 ktGROSS 0 100 200 300 400 500 600 700 800 900WT. kg CRUISE DISTANCE NAUTICAL AIR MILES35000 0 17 34 51 69 86 103 120 138 15536000 172 189 206 224 241 258 275 293 310 32737000 344 361 378 396 413 430 447 464 481 499

38000 516 533 550 567 584 601 618 635 652 67039000 687 704 721 738 755 772 789 806 823 84040000 857 874 891 908 925 942 959 976 993 101041000 1027 1044 1061 1076 1094 1111 1128 1145 1162 117942000 1196 1213 1230 1246 1263 1280 1297 1314 1331 134743000 1364 1381 1398 1414 1431 1448 1465 1482 1498 151544000 1532 1548 1565 1582 1599 1615 1632 1649 1665 168245000 1699 1715 1732 1748 1765 1782 1798 1815 1831 184846000 1865 1881 1898 1914 1931 1947 1964 1980 1997 201347000 2030 2046 2063 2079 2096 2112 2128 2145 2161 2178



48000 2194 2210 2227 2243 2259 2276 2292 2308 2325 234149000 2358 2374 2390 2406 2422 2439 2455 2471 2487 250450000 2520 2536 2552 2568 2585 2601 2617 2633 2649 266551000 2681 2698 2714 2730 2746 2762 2778 2794 2810 282652000 2842 2858 2874 2890 2906 2922 2938 2954 2970 298653000 3002 3017 3033 3049 3065 3081 3097 3113 3128 314454000 3160 3176 3192 3207 3223 3239 3255 3270 3286 330255000 3318 3333 3349 3365 3380 3396 3411 3427 3443 345856000 3474 3490 3505 3521 3536 3552 3567 3583 3598 361457000 3630 3645 3660 3676 3691 3707 3722 3738 3753 376858000 3784 3799 3815 3830 3845 3861 3876 3891 3906 392259000 3937 3952 3968 3983 3998 4013 4028 4044 4059 407460000 4089 4104 4119 4135 4150 4165 4180 4195 4210 422561000 4240 4255 4270 4285 4300 4315 4330 4345 4360 437562000 4390 4405 4420 4435 4450 4465 4479 4494 4509 452463000 4539 4554 4568 4583 4598 4613 4628 4642 4657 467264000 4687 4701 4716 4731 4745 4760 4774 4789 4804 481865000 4833 4848 4862 4877 4891 4906 4920 4935 4949 496466000 4978 4993 5007 5022 5036 5050 5065 5079 5094 510867000 5122 5137 5151 5165 5180 5194 5208 5222 5237 5251NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMITA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMITB) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMITC) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMIT

NOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISAMach 0.74 Cruise Pressure Altitude 25,000 ftFIGURE 033-31

033 PICTURE SUPPLEMENTS122© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C Auto

PRESSURE ALTITUDE 28,000 ft MACH 0.74 CRUISE TAS 440 ktGROSS 0 100 200 300 400 500 600 700 800 900WT. kg CRUISE DISTANCE NAUTICAL AIR MILES35000 0 19 38 57 76 95 114 134 153 17236000 191 210 229 248 267 286 305 324 343 36237000 382 401 419 438 457 476 495 514 533 55238000 571 590 609 628 647 666 684 703 722 74139000 760 779 797 816 835 854 873 891 910 92940000 948 966 985 1004 1022 1041 1060 1078 1097 111641000 1134 1153 1171 1190 1209 1227 1246 1264 1283 130142000 1320 1338 1357 1375 1394 1412 1431 1449 1467 148643000 1504 1523 1541 1559 1578 1596 1614 1633 1651 166944000 1688 1706 1724 1742 1760 1779 1797 1815 1833 1851

45000 1870 1888 1906 1924 1942 1960 1978 1996 2014 203246000 2050 2068 2086 2104 2122 2140 2158 2176 2194 221247000 2230 2248 2265 2283 2301 2319 2337 2355 2372 239048000 2408 2426 2443 2461 2479 2497 2514 2532 2550 256749000 2585 2603 2620 2638 2655 2673 2690 2708 2726 274350000 2761 2778 2795 2813 2830 2848 2865 2883 2900 291751000 2935 2952 2969 2987 3004 3021 3039 3056 3073 309052000 3108 3125 3142 3159 3176 3193 3211 3228 3245 326253000 3279 3296 3313 3330 3347 3364 3381 3398 3415 343254000 3449 3466 3483 3500 3517 3533 3550 3567 3584 3601



55000 3618 3634 3651 3668 3685 3701 3718 3735 3751 376856000 3785 3801 3818 3835 3851 3868 3884 3901 3917 393457000 3951 3967 3983 4000 4016 4033 4049 4065 4082 409858000 4115 4131 4147 4164 4180 4196 4212 4229 4245 426159000 4277 4293 4310 4326 4324 4358 4374 4390 4406 442260000 4438 4454 4470 4486 4502 4518 4534 4550 4566 458261000 4598 4614 4630 4645 4661 4677 4693 4709 4724 474062000 4756 4772 4787 4803 4818 4834 4850 4865 4881 489763000 4912 4928 4943 4959 4974 4990 5005 5021 5036 505264000 5067 5082 5098 5113 5128 5144 5159 5174 5190 520565000 5220 5235 5250 5266 5281 5296 5311 5326 5341 535766000 5372 5387 5402 5417 5432 5447 5462 5477 5492 550767000 5522 5536 5551 5566 5581 5596 5611 5625 5640 5655NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMITA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMITB) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMITC) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMITNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISAMach 0.74 Cruise Pressure Altitude 28,000 ftFIGURE 033-32

033 PICTURE SUPPLEMENTS123© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 31,000 ft MACH 0.74 CRUISE TAS 434 ktGROSS 0 100 200 300 400 500 600 700 800 900WT. kg CRUISE DISTANCE NAUTICAL AIR MILES35000 0 21 42 63 84 105 126 147 168 18936000 210 231 252 273 294 315 336 357 378 39937000 420 440 461 482 503 524 544 565 586 60738000 628 648 669 689 710 731 751 772 793 813

39000 834 854 875 895 916 936 957 977 998 101840000 1039 1059 1079 1100 1120 1140 1161 1181 1201 122241000 1242 1262 1282 1303 1323 1343 1363 1383 1403 142342000 1444 1464 1484 1504 1524 1544 1564 1584 1604 162443000 1644 1663 1683 1703 1723 1743 1763 1782 1802 182244000 1842 1862 1881 1901 1921 1940 1960 1979 1999 201945000 2038 2058 2077 2097 2116 2136 2155 2175 2194 221446000 2233 2252 2272 2291 2310 2330 2349 2368 2388 240747000 2426 2445 2464 2483 2503 2522 2541 2560 2579 259848000 2617 2636 2655 2674 2693 2712 2731 2750 2769 278849000 2807 2825 2844 2863 2882 2900 2919 2938 2956 297550000 2994 3013 3031 3050 3068 3087 3105 3124 3142 316151000 3179 3198 3216 3235 3253 3271 3290 3308 3326 3345

52000 3363 3381 3399 3417 3436 3454 3472 3490 3508 352653000 3545 3563 3580 3598 3616 3634 3652 3670 3688 370654000 3724 3742 3760 3777 3795 3813 3831 3848 3866 388455000 3902 3919 3937 3954 3972 3989 4007 4024 4042 406056000 4077 4094 4112 4129 4146 4164 4181 4198 4216 423357000 4251 4268 4285 4302 4319 4336 4353 4370 4388 440558000 4422 4439 4456 4473 4490 4507 4523 4540 4557 457459000 4591 4608 4625 4641 4658 4675 4691 4708 4725 474260000 4758 4775 4791 4808 4824 4841 4857 4874 4890 490761000 4923 4940 4956 4972 4989 5005 5021 5038 5054 5070



62000 5086 5103 5119 5135 5151 5167 5183 5199 5215 523163000 5247 5263 5279 5295 5311 5327 5343 5358 5374 539064000 5406 5422 5437 5453 5469 5484 5500 5516 5531 554765000 5563 5578 5594 5609 5624 5640 5655 5671 5686 570266000 5717 5732 5748 5763 5778 5793 5809 5824 5839 585467000 5870 5885 5900 5915 5930 5945 5960 5975 5990 6005NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 63,500 kgA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMITB) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMITC) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMITNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISAMach 0.74 Cruise Pressure Altitude 31,000 ftFIGURE 033-33

033 PICTURE SUPPLEMENTS124© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 34,000 ft MACH 0.74 CRUISE TAS 428 kt

GROSS 0 100 200 300 400 500 600 700 800 900WT. kg CRUISE DISTANCE NAUTICAL AIR MILES35000 0 22 45 68 91 114 137 160 183 20636000 229 252 275 297 320 343 365 388 411 43437000 456 479 502 524 547 569 592 614 637 65938000 682 704 726 749 771 793 816 838 860 88339000 905 927 949 971 993 1015 1037 1060 1082 110440000 1126 1148 1170 1191 1213 1235 1257 1279 1301 132341000 1344 1366 1388 1409 1431 1453 1474 1496 1517 153942000 1561 1582 1603 1625 1646 1668 1689 1710 1732 175343000 1775 1796 1817 1838 1859 1880 1902 1923 1944 196544000 1986 2007 2028 2049 2070 2091 2112 2132 2153 217445000 2195 2216 2236 2257 2278 2298 2319 2340 2360 2361

46000 2402 2422 2442 2463 2483 2504 2524 2544 2565 258547000 2606 2626 2646 2666 2686 2706 2726 2747 2767 278748000 2807 2827 2847 2867 2886 2906 2926 2946 2966 298649000 3006 3025 3045 3064 3084 3104 3123 3143 3163 318250000 3202 3221 3240 3260 3279 3298 3318 3337 3356 337651000 3395 3414 3433 3452 3471 3491 3510 3529 3548 356752000 3586 3605 3624 3642 3661 3680 3699 3718 3736 375553000 3774 3792 3811 3830 3848 3867 3885 3904 3922 394154000 3959 3978 3996 4014 4032 4051 4069 4087 4105 412455000 4142 4160 4178 4196 4214 4232 4250 4268 4286 430456000 4322 4339 4357 4375 4393 4410 4428 4446 4464 448157000 4499 4516 4534 4551 4569 4586 4604 4621 4639 465658000 4673 4691 4708 4725 4742 4759 4777 4794 4811 4828

59000 4845 4862 4879 4896 4913 4930 4947 4963 4980 499760000 5014 5031 5047 5064 5081 5097 5114 5130 5147 516461000 5180 5196 5213 5229 5245 5262 5278 5294 5311 532762000 5343 5359 5375 5391 5407 5423 5439 5455 5471 548763000 5503 5519 5534 5550 5566 5581 5597 5613 5828 564464000 5660 5675 5690 5705 5721 5736 5751 5767 5782 579765000 5812 5827 5842 5857 5872 5887 5902 5917 5932 594766000 5962 5976 5991 6005 6020 6034 6049 6063 6078 609367000 6107 6121 6135 6150 6164 6178 6192 6206 6220 6234NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 55,500 kg



A) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER IS 67,100 kgB) THRUST LIMITED WEIGHT FOR ISA +15 IS 65,700 kgC) THRUST LIMITED WEIGHT FOR ISA +20 IS 64,000 kgNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISAMach 0.74 Cruise Pressure Altitude 34,000 ftFIGURE 033-34

033 PICTURE SUPPLEMENTS125© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 30,000 ft MACH 0.78 CRUISE TAS 460 ktGROSS 0 100 200 300 400 500 600 700 800 900WT. kg CRUISE DISTANCE NAUTICAL AIR MILES35000 0 19 38 57 77 96 115 135 154 17336000 193 212 231 250 269 289 308 327 346 36637000 385 404 423 442 461 480 499 519 538 55738000 576 595 614 633 652 671 690 709 728 74739000 766 785 804 823 842 860 879 898 917 936

40000 955 974 993 1011 1030 1049 1068 1086 1105 112441000 1143 1161 1180 1199 1217 1236 1255 1273 1292 131142000 1329 1348 1366 1385 1403 1422 1440 1459 1477 149643000 1514 1533 1551 1569 1588 1606 1624 1643 1661 167944000 1698 1716 1734 1752 1771 1789 1807 1825 1844 186245000 1880 1898 1916 1934 1952 1970 1988 2006 2024 204246000 2061 2078 2096 2114 2132 2150 2168 2186 2204 222247000 2239 2257 2275 2293 2310 2328 2346 2363 2381 239948000 2417 2434 2452 2469 2487 2504 2522 2539 2557 257449000 2592 2609 2627 2644 2661 2679 2696 2713 2731 274850000 2765 2783 2800 2817 2834 2851 2868 2886 2903 292051000 2937 2954 2971 2988 3005 3022 3039 3056 3073 309052000 3107 3123 3140 3157 3174 3191 3207 3224 3241 3258

53000 3274 3291 3308 3324 3341 3357 3374 3390 3407 342354000 3440 3456 3473 3489 3506 3522 3538 3555 3571 358755000 3604 3626 3636 3652 3668 3684 3701 3717 3733 374956000 3765 3781 3797 3813 3829 3845 3861 3877 3893 390957000 3925 3940 3956 3972 3988 4003 4019 4035 4050 406658000 4082 4097 4113 4128 4144 4160 4175 4191 4206 422259000 4237 4252 4268 4283 4298 4314 4329 4344 4360 437560000 4390 4405 4421 4436 4451 4466 4481 4496 4511 452661000 4541 4556 4571 4586 4601 4616 4631 4646 4661 467662000 4691 4705 4720 4735 4749 4764 4779 4794 4808 482363000 4838 4852 4867 4881 4896 4910 4925 4939 4954 496864000 4983 4997 5011 5025 5040 5054 5068 5083 5097 511165000 5125 5140 5154 5168 5182 5196 5210 5224 5238 5252

66000 5266 5280 5294 5308 5322 5335 5349 5363 5377 539167000 5405 5418 5432 5446 5459 5473 5487 5500 5514 5528NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE IS 64,200 kgA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMITB) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMITC) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMITNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURESA) INCREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.6 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISA



D) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISAMach 0.78 Cruise Pressure Altitude 30,000 ftFIGURE 033-35

033 PICTURE SUPPLEMENTS126© 2008AVIATIONEXAM.comAll Engines Maximum Cruise Thrust Limits A/C AutoPRESSURE ALTITUDE 21,000 ft LOW-LEVEL CRUISE TAS 406 ktGROSS 0 100 200 300 400 500 600 700 800 900WT. kg CRUISE DISTANCE NAUTICAL AIR MILES35000 0 16 33 49 66 82 99 115 132 14836000 165 181 198 214 231 247 264 280 297 31337000 330 346 363 379 396 412 429 445 461 47838000 494 511 527 543 560 576 592 609 625 64239000 658 674 691 707 723 739 756 772 788 80540000 821 837 853 870 886 902 918 935 951 96741000 983 999 1016 1032 1048 1064 1080 1096 1112 112942000 1145 1161 1177 1193 1209 1225 1241 1257 1273 128943000 1305 1321 1337 1353 1369 1385 1401 1417 1433 144944000 1465 1481 1497 1513 1529 1545 1561 1577 1593 160945000 1624 1640 1656 1672 1688 1704 1719 1735 1751 176746000 1783 1798 1814 1830 1846 1861 1877 1893 1909 1924

47000 1940 1956 1971 1987 2003 2018 2034 2050 2065 208148000 2096 2112 2128 2143 2159 2174 2190 2205 2221 223649000 2252 2267 2283 2298 2314 2329 2345 2360 2376 239150000 2407 2422 2437 2453 2468 2483 2499 2514 2530 254551000 2560 2576 2591 2606 2621 2637 2652 2667 2682 269852000 2713 2728 2743 2758 2774 2789 2804 2819 2834 284953000 2865 2880 2895 2910 2925 2940 2955 2970 2985 300054000 3015 3030 3045 3060 3075 3090 3105 3120 3135 315055000 3165 3180 3195 3209 3224 3239 3254 3269 3284 329956000 3313 3328 3343 3358 3373 3387 3402 3417 3432 344657000 3461 3476 3490 3505 3520 3534 3549 3564 3578 359358000 3608 3622 3637 3651 3666 3681 3695 3710 3724 373959000 3753 3768 3782 3797 3811 3826 3840 3854 3869 3883

60000 3898 3912 3926 3941 3955 3969 3984 3998 4012 402761000 4041 4055 4070 4084 4098 4112 4126 4141 4155 416962000 4183 4197 4212 4226 4240 4254 4268 4282 4296 431063000 4324 4338 4352 4366 4381 4395 4409 4423 4437 445164000 4465 4478 4492 4506 4520 4534 4548 4562 4576 459065000 4604 4617 4631 4645 4659 4672 4686 4700 4714 472866000 4741 4755 4769 4782 4796 4810 4823 4837 4851 486467000 4878 4892 4905 4919 4932 4946 4959 4973 4987 5000NOTE 1: OPTIMUM WEIGHT FOR PRESSURE ALTITUDE EXCEEDS STRUCTURAL LIMITA) THRUST LIMITED WEIGHT FOR ISA +10 AND COLDER EXCEEDS STRUCTURAL LIMITB) THRUST LIMITED WEIGHT FOR ISA +15 EXCEEDS STRUCTURAL LIMITC) THRUST LIMITED WEIGHT FOR ISA +20 EXCEEDS STRUCTURAL LIMITNOTE 2: ADJUSTMENTS FOR OPERATION AT NON-STANDARD TEMPERATURES

A) INCREASE FUEL REQUIRED BY 0.5 PERCENT PER 10 DEGREES C ABOVE ISAB) DECREASE FUEL REQUIRED BY 0.5 PERCENT PER 10 DEGREES C BELOW ISAC) INCREASE TAS BY 1 KNOT PER DEGREE C ABOVE ISAD) DECREASE TAS BY 1 KNOT PER DEGREE C BELOW ISALow-Level Cruise Pressure Altitude 21,000 ftFIGURE 033-36




AVIATIONEXAM.com0.74 M/250 KIAS (Economy) DescentEconomy DescentPRESS.ALT.ftTIMEminFUELkgAIR DISTANCE TRAVELLED NMLANDING WEIGHT kg35,000 45,000 55,000 65,000 75,00037,000 23 295 98 109 114 114 11035,000 22 290 94 105 110 110 10633,000 21 285 89 99 103 103 10131,000 20 280 83 93 97 98 9529,000 19 275 78 87 91 91 8927,000 19 270 73 81 85 85 8325,000 18 260 68 75 79 79 7723,000 16 255 63 69 72 73 7121,000 15 245 58 64 66 67 6619,000 14 235 53 58 60 61 6017,000 13 225 48 52 54 55 54

15,000 12 215 43 46 48 49 4810,000 9 185 30 32 33 34 335,000 6 140 18 18 18 18 183,700 5 130 14 14 14 14 140.70 M/280/250 KIAS (Turbulence Penetration) DescentTurbulence Penetration DescentPRESS.ALT.ftTIMEminFUELkg

AIR DISTANCE TRAVELLED NMLANDING WEIGHT kg35,000 45,000 55,000 65,000 75,00037,000 21 280 88 100 107 110 10935,000 20 275 84 96 102 105 10533,000 20 275 80 91 98 101 10131,000 19 270 76 86 93 96 9629,000 18 265 72 82 88 91 9227,000 17 260 69 78 84 87 8725,000 17 255 64 73 78 80 8123,000 16 250 60 67 72 74 7421,000 15 240 55 62 66 68 6819,000 14 230 51 57 60 62 62

17,000 13 225 46 52 55 56 5615,000 12 215 42 46 49 50 5010,000 9 185 30 32 33 34 335,000 6 140 18 18 18 18 183,700 5 130 14 14 14 14 14FIGURE 033-37




AVIATIONEXAM.comNon-Normal Operation Gear Down Ferry FlightREF LINEREF LINEPRESSUREALTITUDE1000 ftBASED ON:220 KIAS CLIMB220 KIAS DESCENT30 40 50 60TRIP TIME hr0123420 10 0 -10ISA DEV °CTRIP DISTANCE NMLANDING WEIGHT1000 kg03

456789 FUEL REQUIRED 1000 kg121011121514

131000100HEADTAILWINDkt5050200 400 600 800 1000 0282420

161412108282420161412108288PRESSURE ALTITUDE 1000 ftPRESSURE ALTITUDE 1000 ftREF LINEFIGURE 033-38



033 PICTURE SUPPLEMENTS129© 2008AVIATIONEXAM.comSpeedM/KIASDiv. Wt1000 kgTIME MINUTES60 70 80 90 100 110 120 130 140 150 160 170 180 190 20035 406 472 539 605 672 738 805 871 938 1004 1071 1137 1204 1271 133740 402 467 533 598 663 729 794 860 925 990 1056 1121 1187 1252 131845 397 462 526 590 654 718 782 846 910 975 1039 1103 1167 1231 1295.70/280 50 392 454 517 580 642 705 768 830 893 956 1018 1081 1144 1207 126955 385 446 507 568 630 691 752 813 875 936 997 1058 1119 1181 124260 377 437 497 557 616 676 736 796 855 915 975 1035 1094 1154 121465 369 427 486 544 602 660 718 776 835 893 951 1009 1067 1125 118370 363 419 476 532 589 645 702 758 815 871 928 985 1041 1098 115435 412 478 545 612 678 745 811 878 945 1011 1078 1145 1211 1278 134540 409 474 540 606 672 737 803 869 935 1000 1066 1132 1198 1263 132945 404 469 533 598 663 727 792 856 921 986 1050 1115 1180 1244 1309.74/290 50 400 463 526 590 653 717 780 844 907 970 1034 1097 1161 1224 128855 393 455 517 579 641 704 766 828 890 952 1014 1077 1139 1201 126360 386 447 508 568 629 690 751 812 872 933 994 1055 1116 1176 1237

65 378 437 497 556 615 675 734 793 853 912 971 1031 1090 1149 120970 372 430 488 546 603 661 719 777 835 893 950 1008 1066 1124 118235 415 482 548 615 681 748 814 881 948 1014 1081 1147 1214 1280 134740 413 479 545 611 677 743 810 876 942 1008 1074 1140 1206 1272 133845 410 476 541 607 672 737 803 868 933 999 1064 1130 1195 1260 1326.74/310 50 407 472 536 601 665 730 794 859 923 988 1052 1116 1181 1245 131055 402 466 529 592 656 719 783 846 908 973 1036 1100 1163 1226 129060 397 459 521 583 646 708 770 833 895 957 1019 1082 1144 1206 126965 391 452 513 574 635 696 757 818 879 940 1002 1063 1124 1185 124670 385 445 505 565 625 685 744 804 864 924 984 1044 1103 1163 122335 416 482 548 614 680 746 811 877 943 1009 1075 1141 1207 1273 133940 415 481 547 613 678 744 810 875 941 1007 1072 1138 1204 1270 133545 414 480 545 610 676 741 806 871 937 1002 1067 1133 1198 1263 1328

.74/330 50 412 477 542 607 671 736 801 865 930 995 1059 1124 1189 1254 131855 408 472 536 600 664 728 792 856 920 984 1048 1112 1176 1240 130460 404 467 530 593 656 719 783 846 909 972 1035 1098 1161 1224 128765 399 461 523 586 648 710 772 834 896 958 1020 1082 1144 1207 126970 395 457 518 579 640 701 762 823 884 945 1006 1067 1128 1190 125135 368 428 488 548 608 668 728 787 847 906 965 1024 1083 1141 120040 372 433 493 554 614 674 735 794 854 914 973 1032 1092 1151 120945 376 437 497 558 619 679 739 799 859 919 979 1038 1097 1157 1216LRC 50 379 440 501 561 622 682 742 803 862 922 982 1041 1101 1160 121955 380 441 502 562 623 683 743 803 863 922 982 1041 1100 1159 121860 381 442 503 563 624 684 744 804 863 923 982 1041 1100 1159 121865 381 442 503 563 623 683 742 802 861 921 980 1038 1097 1156 121470 383 444 504 564 623 683 742 802 860 919 978 1036 1094 1152 1210

ISABASED ON DRIFTDOWN STARTING AT OR NEAR OPTIMUM ALTITUDEArea of Operation Diversion Distance One Engine InoperativeFIGURE 033-39

033 PICTURE SUPPLEMENTS130© 2008AVIATIONEXAM.comIn-Flight Diversion (LRC) One Engine Inoperative



20 10 0 -10ISA DEV °C1000100HEADTAILWINDkt5050DISTANCE FROM POINT OF DIVERSION TO ALTERNATE NM0 400 800 1200 160030 40 50 60 70WEIGHT AT POINT OFDIVERSION 1000 kgINCLUDESAPU FUEL BURNBASED ON0.74 / 250 DESCENT2468

101214FUEL REQUIRED 1000 kgREF LINEREF LINE012345DIVERSION TIME hr

2622181410626221814106266PRESSUREALTITUDE1000 ft

ONE ENGINE INOPERATIVEREF LINEPRESSURE ALTITUDE 1000 ftPRESSURE ALTITUDE 1000 ftFIGURE 033-40




Fuel Tankering (LRC and 0.74 M)29333537SURPLUS FUEL BURN %5 10 15 20 25 0010002000TRIP DISTANCE NM3000LANDING WEIGHT(WITHOUT TANKERED FUEL)75859510511535404550lb kg

1000LONG RANGE CRUISEREF LINEPRESSURE ALTITUDE 1000 ft5 10 15 20 25 0010002000TRIP DISTANCE NM3000LANDING WEIGHT(WITHOUT TANKERED FUEL)75

859510511535404550lb kg1000REF LINE2933

3537PRESSURE ALTITUDE 1000 ft0.74 MACHSURPLUS FUEL BURN %FIGURE 033-41




Fuel Price Differential0 5 10 15 20 25 30SURPLUS FUEL BURNOFF %5075100125150175200BREAK-EVEN FUEL PRICE DESTINATION AIRPORTCENTS / GALLON1751501251007550FUELPRICEATDEPARTUREAIRPORTCENTS/GALLON

FIGURE 033-42033 PICTURE SUPPLEMENTS133© 2008AVIATIONEXAM.comOptimum Aircraft WeightAir Distance Fuel Price Ratio500 NM1000 NM1500 NM2000 NM2500 NM

3000 NM3500 NM4000 NM4500 NM5000 NM160 170 180 190 200 210360 380 400 420 440 460 (1000 lbs)(1000 kg)0.980.970.960.950.94

0.930.920.910.900.890.880.870.860.850.84



0.83FL350FIGURE 033-43

033 PICTURE SUPPLEMENTS134© 2008AVIATIONEXAM.comOptimum Aircraft WeightAir Distance Fuel Price Ratio500 NM1000 NM1500 NM2000 NM2500 NM3000 NM3500 NM4000 NM4500 NM5000 NM160 170 180 190 200 210360 380 400 420 440 460 (1000 lbs)(1000 kg)0.99

0.980.970.950.940.930.920.910.900.890.880.870.860.96

FL310FIGURE 033-44

033 PICTURE SUPPLEMENTS135© 2008AVIATIONEXAM.com410390370350330160 170 180 190 200 210 220 230 240

360 380 400 420 440 460 480 500 520FLWEIGHT (x 1000 kg)M.80(x 1000 lbs)410390370350330



160 170 180 190 200 210 220 230 240360 380 400 420 440 460 500 520FLWEIGHT (x 1000 kg)(x 1000 lb) 310MAX ALT (ISA+10)MAX ALT (ISA+20)OPT ALT ALL TEMP.MAX ALT (ISA+15)n = 1.4gn = 1.3gMAX AND OPT ALT (ISA+20)OPT ALT (. ISA+15)MAX ALT (ISA+15)MAX ALT (. ISA+10)n = 1.4gn = 1.3g480M.80FIGURE 033-45


AVIATIONEXAM.com410390370350330160 170 180 190 200 210 220 230 240FLWEIGHT (x 1000 kg)(x 1000 lb)310LONG RANGE410

390370350330160 170 180 190 200 210 220 230 240FLWEIGHT (x 1000 kg)(x 1000 lb) 310M.84MAX AND OPT ALT (ISA+20)MAX ALT (ISA+15)OPT ALT ALL TEMP.n=1.3g

n=1.4gMAX ALT (.ISA+10)OPT ALT(ISA+10)(ISA+15)MAX ALT (.ISA+10)MAX ALT (ISA+15)MAX ALT (ISA+20)360 380 400 420 440 460 480 500 520360 380 400 420 440 460 480 500 520FIGURE 033-46



033 PICTURE SUPPLEMENTS137© 2008AVIATIONEXAM.comGROUNDDIST(NM) +150 +100 +50 0 ..50 ..100 ..15010 8 8 9 10 11 13 1520 15 17 18 20 22 25 2930 23 25 27 30 34 38 4440 30 33 36 40 45 51 5950 38 41 45 50 56 63 73100 76 83 90 100 112 127 146200 152 165 181 200 224 254 293300 228 248 271 300 335 381 439400 304 330 362 400 447 507 586500 380 413 452 500 559 634 7321000 759 825 904 1000 1118 1268 14651500 1139 1238 1357 1500 1677 1903 21972000 1518 1651 1809 2000 2237 2537 29302500 1898 2063 2261 2500 2796 3171 36623000 2277 2476 2713 3000 3355 3805 43953500 2657 2889 3165 3500 3914 4439 5127

4000 3036 3302 3617 4000 4473 5073 58604500 3416 3714 4070 4500 5032 5708 65925000 3795 4127 4522 5000 5591 6342 73245500 4175 4540 4974 5500 6151 6976 80576000 4555 4952 5426 6000 6710 7610 87896500 4934 5365 5878 6500 7269 8244 95227000 5314 5778 6330 7000 7828 8878 102547500 5693 6190 6783 7500 8387 9513 109878000 6073 6603 7235 8000 8946 10147 117198500 6452 7016 7687 8500 9506 10781 124519000 6832 7428 8139 9000 10065 11415 131849500 7211 7841 8591 9500 10624 12049 1391610000 7591 8254 9043 10000 11183 12683 14649

M.82AIR..DISTANCE..(NM)TAIL..WIND HEAD..WIND WIND..COMPONENT..(KTS)FIGURE 033-47

033 PICTURE SUPPLEMENTS138© 2008AVIATIONEXAM.comGROUNDDIST(NM) +150 +100 +50 0 ..50 ..100 ..15010 8 8 9 10 11 13 15

20 15 16 18 20 22 25 2930 23 25 27 30 34 38 4440 30 33 36 40 45 51 5950 38 41 45 50 56 64 74100 76 82 90 100 112 127 147200 151 165 181 200 224 254 295300 227 247 271 300 336 382 442400 303 330 361 400 448 509 589500 379 412 452 500 560 636 7361000 757 824 903 1000 1120 1272 1473



1500 1136 1236 1355 1500 1680 1908 22092000 1514 1648 1807 2000 2240 2544 29452500 1893 2059 2258 2500 2799 3180 36813000 2271 2471 2710 3000 3359 3817 44183500 2650 2883 3162 3500 3919 4453 51544000 3028 3295 3613 4000 4479 5089 58904500 3407 3707 4065 4500 5039 5725 66275000 3785 4119 4517 5000 5599 6361 73635500 4164 4531 4968 5500 6159 6997 80996000 4542 4943 5420 6000 6719 7633 88366500 4921 5354 5872 6500 7279 8269 95727000 5299 5766 6324 7000 7839 8905 103087500 5678 6178 6775 7500 8398 9541 110448000 6056 6590 7227 8000 8958 10177 117818500 6435 7002 7679 8500 9518 10814 125179000 6813 7414 8130 9000 10078 11450 132539500 7192 7826 8582 9500 10638 12086 1399010000 7570 8238 9043 10000 11198 12722 14726LONG..RANGE..CRUISE..ABOVE..FL250AIR..DISTANCE..(NM)TAIL..WIND WIND..COMPONENT..(KTS) HEAD..WINDFIGURE 033-48


139© 2008AVIATIONEXAM.comDIS.FL310 FL350 FL390FL330 FL370 FL4103537 3531 110.39 0.394764 4684 4622 4579 4555 4548 13 16 180.51 0.52 0.52 0.52 0.52 0.525993 5840 5711 5609 5536 5489 16 18 221.04 1.04 1.04 1.05 1.05 1.057225 6998 6803 6642 6519 6434 18 21 25

1.16 1.17 1.17 1.17 1.17 1.178460 8160 7898 7679 7506 7383 20 24 291.29 1.29 1.30 1.30 1.30 1.309698 9323 8996 8718 8496 8335 22 27 321.41 1.42 1.43 1.43 1.43 1.4310938 10490 10096 9759 9490 9291 25 29 361.54 1.55 1.55 1.56 1.56 1.5612180 11659 11199 10804 10486 10251 27 32 402.06 2.07 2.08 2.08 2.09 2.0913425 12831 12305 11851 11485 11213 29 35 442.19 2.20 2.21 2.21 2.21 2.2114673 14005 13413 12901 12487 12180 32 38 482.31 2.32 2.33 2.34 2.34 2.34

15924 15182 14525 13954 13492 13149 34 41 512.44 2.45 2.46 2.47 2.47 2.4717178 16363 15640 15010 14501 14123 37 44 552.56 2.58 2.59 3.00 3.00 3.0018434 17546 16758 16070 15514 15101 39 47 593.09 3.10 3.12 3.12 3.12 3.1219693 18732 17879 17132 16530 16083 42 50 643.21 3.23 3.24 3.25 3.25 3.2520955 19921 19003 18197 17550 17069 45 53 683.34 3.36 3.37 3.38 3.38 3.38



22221 21114 20129 19266 18574 18060 47 56 723.46 3.48 3.50 3.51 3.51 3.5123489 22310 21260 20337 19601 19054 50 59 773.59 4.01 4.03 4.04 4.04 4.0424761 23508 22394 21412 20632 20052 53 63 824.11 4.13 4.15 4.16 4.16 4.1626035 24710 23531 22491 21667 21067 56 66 874.24 4.26 4.28 4.29 4.29 4.2927311 25914 24671 23573 22707 22078 58 69 924.37 4.39 4.41 4.42 4.42 4.4228591 27122 25814 24658 23750 23093 61 73 974.49 4.51 4.53 4.55 4.55 4.5529875 28333 26960 25746 24796 24113 64 76 1025.02 5.04 5.06 5.07 5.08 5.0831161 29546 28110 26837 25846 25136 67 79 1075.14 5.16 5.19 5.20 5.20 5.2032450 30764 29263 27932 26920 26165 70 82 1135.27 5.29 5.32 5.33 5.33 5.3333742 31985 30419 29030 27982 27198 73 86 1185.39 5.42 5.44 5.46 5.46 5.4635038 33209 31577 30131 29047 28237 75 90 1225.52 5.54 5.57 5.59 5.59 5.59AIR CORRECTION ONFLIGHT LEVEL

ANTI ICING OFF CG = 37,0 % TIME (H.MIN)NORMAL AIR CONDITIONINGFLIGHT PLANNING FROM BREAKE RELEASE TO LANDINGCLIMB: 250KTS/300KTS/M.80 - CRUISE: M.82 - DESCENT: M.82/300KTS/250KTSIMC PROCEDURE: 240 KG (6 MIN)REF. LANDING WEIGHT = 140.000 KG ISA FUEL CONSUMED (KG)FUEL CONSUMPTION(KG/1.000 KG)(NM)14001500200300

400500600310 330 350 370 390 410160017001800700800900100011001200

130019002000210022002300..FUEL..=..+1,5..% ..FUEL = +7 %TOTAL ANTI ICE ONICE..ON2400



2500CARGO COOL ON..FUEL = -0,4 % ..FUEL = +1 %26002700PACK FLOW LO PACK FLOW HI OR/AND ENGINE..ANTIFIGURE 033-49

033 PICTURE SUPPLEMENTS140© 2008AVIATIONEXAM.comDIS.FL310 FL350 FL390FL330 FL370 FL41036336 34437 32738 31237 30117 29281 78 94 1276.04 6.07 6.10 6.11 6.11 6.1237638 35668 33903 32372 31191 30330 82 97 1326.17 6.20 6.23 6.24 6.24 6.2438942 36902 35072 33487 32269 31386 85 103 1376.29 6.32 6.35 6.37 6.37 6.3740249 38139 36243 34607 33351 32446 88 105 1436.42 6.45 6.48 6.50 6.50 6.5041560 39379 37453 35730 34439 33511 93 109 149

6.54 6.57 7.01 7.03 7.03 7.0342874 40622 38634 36857 35532 34584 96 114 1557.07 7.10 7.13 7.15 7.15 7.1544192 41911 39819 37988 36628 35663 100 116 1617.19 7.23 7.26 7.28 7.28 7.2845514 43166 41008 39122 37729 36746 106 120 1687.32 7.35 7.39 7.41 7.41 7.4146839 44426 42201 40260 38835 37835 107 124 1747.44 7.48 7.52 7.54 7.54 7.5448219 45690 43398 41403 39944 38929 111 128 1837.57 8.01 8.04 8.07 8.07 8.0749556 46958 44600 42549 41060 40029 112 133 1918.09 8.13 8.17 8.19 8.19 8.19

50897 48230 45805 43702 42181 41137 115 137 1998.22 8.26 8.30 8.32 8.32 8.3252241 49505 47014 44863 43306 42250 119 142 2078.34 8.38 8.43 8.45 8.45 8.4553588 50785 48228 46028 44438 43370 122 146 2158.47 8.51 8.55 8.58 8.58 8.5854940 52068 49446 47198 45577 44524 126 151 2238.59 9.04 9.08 9.11 9.11 9.10*56296 53355 50667 48374 46721 45690 130 156 2309.12 9.16 9.21 9.23 9.23 9.23*57657 54647 51892 49555 47872 46862 133 161 2399.24 9.29 9.34 9.36 9.36 9.36*59022 55943 53121 50739 49028 48040 137 166 247

9.37 9.41 9.46 9.49 9.49 9.49*60391 57242 54355 51929 50190 49223 140 171 2559.49 9.54 9.59 10.02 10.02 10.02*61766 58545 55593 53123 51357 50411 144 176 26210.02 10.07 10.12 10.15 10.15 10.14*63144 59851 56836 54322 52530 51604 148 181 27010.14 10.19 10.24 10.27 10.27 10.27*64525 61162 58083 55527 53707 52803 152 186 27710.27 10.32 10.37 10.40 10.40 10.40*65911 62478 59335 56737 54917 54006 156 191 283



10.39 10.45 10.50 10.53 10.53 10.53*67301 63798 60592 57952 56112 55217 160 196 29110.52 10.57 11.03 11.06 11.06 11.06*68696 65121 61854 59173 57312 56433 164 201 30011.04 11.10 11.15 11.19 11.19 11.18*70095 66449 63121 60400 58519 57654 167 207 30911.17 11.23 11.28 11.31 11.31 11.31*AIRCORRECTION..ONFLIGHT..LEVELANTI..ICING..OFF CG..=..37,0..% TIME..(H.MIN)NORMAL..AIR..CONDITIONINGFLIGHT..PLANNING..FROM..BREAKE..RELEASE..TO..LANDINGCLIMB:..250KTS/300KTS/M.80......CRUISE:..M.82......DESCENT:..M.82/300KTS/250KTSIMC..PROCEDURE:..240..KG..(6..MIN)REF...LANDING..WEIGHT..=..140.000..KG ISA FUEL..CONSUMED..(KG)FUEL..CONSUMPTION(KG/1.000..KG)(NM)40004100280029003000

31003200310 330 350 370 390 4104200430044003300340035003600370038003900

45004600470048004900..FUEL..=..+1,5..% ..FUEL..=..+7..%TOTAL..ANTI..ICE..ONICE..ON50005100CARGO..COOL..ON..FUEL..=....0,4..% ..FUEL..=..+1..%5200

5300PACK..FLOW..LO PACK..FLOW..HI..OR/AND ENGINE..ANTIFIGURE 033-50

033 PICTURE SUPPLEMENTS141© 2008AVIATIONEXAM.comWEIGHT TAS(1000 KG) (KTS)



0 18 35 53 70 88 105 123 140 157 3560 3 6 9 12 15 18 21 23 26175 192 210 227 245 262 279 297 314 331 35929 32 35 38 41 44 47 50 53 55349 366 383 400 418 435 452 469 487 504 36158 61 64 67 70 73 75 78 81 84521 538 556 573 590 607 624 641 658 676 36287 90 93 95 98 101 104 107 110 113693 710 727 744 761 778 795 812 829 846 362115 118 121 124 127 129 132 135 138 141863 880 897 914 931 948 965 982 999 1016 363144 146 149 152 155 158 160 163 166 1691033 1050 1067 1084 1100 1117 1134 1151 1168 1185 364172 174 177 180 183 185 188 191 194 1971202 1218 1235 1252 1269 1269 1302 1319 1336 1352 365199 202 205 208 210 213 216 219 221 2241369 1386 1403 1419 1436 1453 1469 1486 1503 1519 366227 230 232 235 238 241 243 246 249 2511536 1553 1569 1586 1602 1619 1636 1652 1669 1685 366254 257 260 262 265 268 271 273 276 2791702 1718 1735 1751 1768 1784 1801 1817 1834 1850 367281 284 287 289 292 295 298 300 303 3061867 1883 1899 1916 1932 1949 1965 1981 1998 2014 368308 311 314 316 319 322 324 327 330 332

2031 2047 2063 2080 2096 2112 2128 2145 2161 2177 369335 338 340 343 346 348 351 354 356 3592194 2210 2226 2242 2258 2275 2291 2307 2323 2339 369361 364 367 369 372 375 377 380 383 3852356 2372 2388 2404 2420 2436 2452 2469 2485 2501 370388 390 393 396 398 401 403 406 409 4113517 2533 2549 2565 2581 2597 2613 2629 2645 2661 371414 416 419 422 424 427 429 432 435 4372677 2693 2709 2725 2741 2757 2773 2789 2805 2821 371440 442 445 448 450 453 455 458 460 4633837 2853 2868 2884 2900 2916 2932 2948 2964 2979 372466 468 471 473 476 478 481 483 486 4892995 3011 3027 3043 3058 3074 3090 3106 3121 3137 373

491 494 496 499 501 504 506 509 511 5143153 3169 3184 3200 3216 3231 3247 3263 3278 3294 373516 519 521 524 527 529 532 534 537 5393310 3325 3341 3357 3372 3388 3403 3419 3434 3450 374542 544 547 549 552 554 557 559 562 5643466 3481 3497 3512 3528 3543 3559 3574 3590 3605 375567 569 572 574 577 579 582 584 586 5893621 3636 3652 3667 3682 3698 3713 3729 3744 3760 375591 594 596 599 601 604 606 609 611 6143775 3790 3806 3821 3836 3852 3867 3882 3898 3913 376616 618 621 623 626 628 631 633 636 638..FUEL..=..+6..% ..FUEL..=....0,4..%PACK..FLOW..HI..OR/

AND..CARGO..COOL..ON..FUEL..=..+1..%ENGINE..ANTI..ICE..ON..FUEL..=..+1,5..%INTEGRATED CRUISELR FL 250PACK..FLOW..LO TOTAL..ANTI..ICE..ONDISTANCEISACG = 30,0 % ANTI-ICING OFF



MAX. CRUISE THRUST LIMITSNORMAL AIR CONDITIONING1.2 1.4 1.6 1.8TIME (MIN)(NM)0 .2 .4 .6 .8 1.0136126128130132134158138140142144146148150152154156172

160162164166168170FIGURE 033-51

033 PICTURE SUPPLEMENTS142© 2008AVIATIONEXAM.comWEIGHT TAS

(1000 KG) (KTS)0 22 43 65 87 108 130 151 173 194 3770 3 7 10 14 17 21 24 27 31216 237 259 280 302 323 344 366 387 408 38534 37 41 44 47 51 54 57 60 64430 451 472 493 514 536 557 578 599 620 39267 70 73 77 80 83 86 89 93 96641 662 683 704 725 746 767 788 809 829 40099 102 105 108 112 115 118 121 124 127850 871 892 913 933 954 975 995 1016 1037 411130 133 136 139 142 145 148 151 154 1571057 1078 1099 1119 1140 1160 1181 1201 1222 1242 418160 163 166 169 172 175 178 180 183 186

1263 1283 1304 1324 1345 1365 1385 1406 1426 1446 420189 192 195 198 201 204 207 210 213 2151467 1487 1507 1528 1548 1568 1589 1609 1629 1649 421218 221 224 227 230 233 236 239 241 2441669 1690 1710 1730 1750 1770 1790 1810 1830 1850 423247 250 253 256 259 261 264 267 270 2731870 1890 1910 1930 1950 1970 1990 2010 2030 2050 425276 278 281 284 287 290 292 295 298 3012070 2090 2109 2129 2149 2169 2189 2208 2228 2248 427304 306 309 312 315 318 320 323 326 329



2268 2287 2307 2327 2346 2366 2385 2405 2425 2444 429331 334 337 340 342 345 348 351 353 3562464 2483 2503 2522 2542 2561 2581 2600 2619 2639 431359 361 364 367 370 372 375 378 380 3832658 2678 2697 2716 2736 2755 2774 2793 2813 2832 434386 388 391 394 396 399 402 404 407 4102851 2870 2889 2909 2928 2947 2966 2985 3004 3023 437412 415 418 420 423 425 428 431 433 4363042 3062 3081 3100 3119 3138 3157 3175 3194 3213 439439 441 444 446 449 452 454 457 459 4623232 3251 3270 3289 3308 3327 3345 3364 3383 3402 441464 467 470 472 475 477 480 482 485 4873421 3439 3458 3477 3495 3514 3533 3551 3570 3589 442490 493 495 498 500 503 505 508 510 5133607 3626 3645 3663 3682 3700 3719 3737 3756 3774 444515 518 520 523 525 528 530 533 535 5383793 3811 3830 3848 3866 3885 3903 3922 3940 3958 446540 543 545 548 550 553 555 558 560 5633977 3995 4013 4031 4050 4068 4086 4104 4123 4141 448565 567 570 572 575 577 580 582 585 5874159 4177 4195 4213 4232 4250 4268 4286 4304 4322 450589 592 594 597 599 601 604 606 609 6114340 4358 4376 4394 4412 4430 4448 4466 4484 4502 451614 616 618 621 623 625 628 630 633 635

4520 4538 4555 4573 4591 4609 4627 4645 4662 4680 453637 640 642 644 647 649 652 654 656 659..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+6..%168170172PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON TOTAL..ANTI..ICE..ONAND..CARGO..COOL..ON166144146148150

1521541561581601621641.81261281301321.0 1.2

1421.4 1.61341361381400 .2 .4 .6 .8INTEGRATED CRUISEMAX. CRUISE THRUST LIMITS DISTANCELR FL 350 NORMAL AIR CONDITIONING ISA (NM)



ANTI-ICING OFF CG = 37,0 % TIME (MIN)FIGURE 033-52

033 PICTURE SUPPLEMENTS143© 2008AVIATIONEXAM.comWEIGHT TAS(1000 KG) (KTS)5088 5107 5126 5144 5163 5182 5200 5219 5238 5256 459665 668 670 673 675 678 680 682 685 6875275 5293 5312 5330 5349 5367 5385 5404 5422 5441 459690 692 695 697 699 702 704 707 709 7115459 5477 5496 5514 5532 5551 5569 5587 5605 5623 459714 716 719 721 723 726 728 731 733 7355642 5660 5678 5696 5714 5732 5750 5768 5786 5804 459738 740 742 745 747 750 752 754 757 7595822 5840 5858 5875 5893 5911 5929 5947 5964 5982 459761 764 766 768 771 773 775 778 780 7826000 6018 6035 6053 6071 6088 6105 6119 6133 6151 459785 787 789 791 794 796 798 800 802 8046168 6186 6203 6220 6238 6255 6273 6290 6307 6325 459807 809 811 813 816 818 820 822 825 8276342 6359 6377 6394 6411 6429 6446 6463 6480 6497 459

829 832 834 836 838 841 843 845 847 8506515 6532 6549 6566 6583 6600 6617 6635 6652 6669 459852 854 856 859 861 863 865 868 870 8726686 6703 6720 6737 6754 6771 6788 6805 6821 6838 459874 876 879 881 883 885 888 890 892 8946855 6872 6889 6906 6923 6940 6956 6973 6990 7007 459896 899 901 903 905 907 910 912 914 9167023 7040 7057 7073 7090 7107 7123 7140 7157 7173 459918 921 923 925 927 929 931 934 936 9387190 7206 7223 7239 7256 7272 7289 7305 7322 7338 459940 942 944 947 949 951 953 955 957 9607354 7371 7387 7403 7420 7436 7452 7468 7485 7501 459962 964 966 968 970 972 974 977 979 981

7517 7533 7549 7566 7582 7598 7614 7630 7646 7662 459983 985 987 989 991 993 996 998 1000 10027678 7694 7708 7720 7735 7751 7766 7782 7798 7814 4591004 1006 1008 1010 1011 1013 1016 1018 1020 10227830 7846 7861 7877 7893 7909 7925 7940 7956 7972 4611024 1026 1028 1030 1032 1034 1036 1038 1040 10427988 8003 8019 8035 8050 8066 8081 8097 8113 8128 4611044 1046 1048 1050 1052 1054 1057 1059 1061 10638144 8159 8175 8191 8206 8222 8237 8253 8268 8284 4611065 1067 1069 1071 1073 1075 1077 1079 1081 10838299 8315 8330 8345 8361 8376 8392 8407 8422 8438 4611085 1087 1089 1091 1093 1095 1097 1099 1101 11038453 8468 8484 8499 8514 8529 8545 8560 8575 8590 461

1105 1107 1109 1111 1113 1115 1117 1119 1121 11238606 8621 8636 8651 8666 8681 8696 8712 8727 8742 4611125 1127 1129 1131 1133 1135 1137 1138 1140 11428757 8772 8787 8802 8817 8832 8847 8862 8877 8892 4611144 1146 1148 1150 1152 1154 1156 1158 1160 1162..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+7..%216218PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON TOTAL..ANTI..ICE..ONAND..CARGO..COOL..ON



2141921941961982002022042062082102121.81741761781801.0 1.21901.4 1.6182184186188

0 .2 .4 .6 .8INTEGRATED CRUISEMAX. CRUISE THRUST LIMITS DISTANCEM.80 OPT FL NORMAL AIR CONDITIONING ISA (NM)ANTI-ICING OFF CG = 37,0 % TIME (MIN)FIGURE 033-53

033 PICTURE SUPPLEMENTS144© 2008AVIATIONEXAM.comWEIGHT TAS(1000 KG) (KTS)

4710 4724 4738 4755 4772 4789 4806 4823 4840 4857 482587 588 590 592 594 596 599 601 603 6054874 4891 4908 4925 4942 4959 4975 4992 5009 5026 482607 609 611 613 615 618 620 622 624 6265043 5059 5076 5093 5109 5126 5143 5159 5176 5193 482628 630 632 634 636 638 640 643 645 6475209 5226 5242 5259 5276 5292 5309 5325 5342 5358 482649 651 653 655 657 659 661 663 665 6675375 5391 5407 5424 5440 5457 5473 5489 5505 5522 482669 671 673 675 677 680 682 684 686 6885538 5554 5571 5587 5603 5619 5635 5652 5668 5684 482690 692 694 696 698 700 702 704 706 7085700 5716 5732 5748 5764 5780 5796 5812 5828 5844 482

710 712 714 716 718 720 722 724 726 7705860 5876 5892 5907 5923 5939 5955 5971 5986 6002 482730 732 734 736 738 740 742 744 746 7476018 6034 6049 6065 6081 6096 6112 6127 6143 6159 482749 751 753 755 757 759 761 763 765 7676174 6189 6202 6215 6230 6245 6261 6276 6292 6307 482769 771 772 774 776 778 780 782 783 7856322 6338 6353 6368 6384 6399 6414 6430 6445 6460 484787 789 791 793 795 797 799 801 802 8046476 6491 6506 6521 6536 6552 6567 6582 6597 6612 484



806 808 810 812 814 816 818 819 821 8236627 6642 6657 6673 6688 6703 6718 6733 6748 6763 484825 827 829 831 833 834 836 838 840 8426778 6793 6808 6823 6838 6852 6867 6882 6897 6912 484844 846 847 849 851 853 855 857 858 8606927 6942 6956 6971 6986 7001 7016 7030 7045 7060 484862 864 866 868 870 871 873 875 877 8797074 7089 7104 7118 7133 7148 7162 7177 7191 7206 484880 882 884 886 888 890 891 893 895 8977221 7235 7249 7264 7278 7293 7307 7322 7336 7351 484899 900 902 904 906 908 909 911 913 9157365 7379 7394 7408 7422 7437 7451 7465 7479 7494 484916 918 920 922 924 925 927 929 931 9327508 7522 7536 7550 7565 7577 7589 7601 7615 7629 484934 936 938 939 941 943 944 946 947 9497643 7657 7671 7685 7699 7713 7727 7741 7755 7769 489951 953 954 956 958 960 961 963 965 9667783 7797 7811 7825 7839 7853 7867 7881 7895 7908 489968 970 972 973 975 977 978 980 982 9837922 7936 7950 7964 7978 7991 8005 8019 8033 8046 489985 987 989 990 992 994 995 997 999 10008060 8074 8088 8101 8115 8129 8142 8156 8170 8183 4891002 1004 1005 1007 1009 1011 1012 1014 1016 1017AND..CARGO..COOL..ON

..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+7..%TOTAL..ANTI..ICE..ON204206208210212214216218PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON202180

1821841861881901921941961982001.4 1.6 1.8174176

178CG = 37,0 % TIME (MIN)0 .2 .4 .6 .8 1.0 1.2INTEGRATED CRUISEMAX. CRUISE THRUST LIMITS DISTANCEM.84 OPT FL NORMAL AIR CONDITIONING ISA (NM)ANTI-ICING OFFFIGURE 033-54




145© 2008AVIATIONEXAM.comWEIGHT TAS(1000 KG) (KTS)0 22 45 67 89 112 134 156 178 200 4180 3 6 10 13 16 19 22 26 29223 245 267 289 311 333 355 377 399 42 41932 35 38 41 45 48 51 54 57 60443 465 487 509 531 553 575 597 619 640 42163 67 70 73 76 79 82 85 88 91662 684 706 727 749 771 793 814 836 857 42495 98 101 104 107 110 113 116 119 122879 901 922 944 965 987 1008 1030 1051 1073 426125 128 131 134 137 140 143 146 149 1521094 1115 1137 1158 1180 1201 1222 1243 1265 1286 428155 158 161 164 167 170 173 176 179 1821307 1328 1349 1371 1392 1413 1434 1455 1476 1497 431185 188 191 194 197 200 203 206 209 2111518 1539 1560 1581 1602 1623 1644 1665 1686 1707 434214 217 220 223 226 229 232 235 238 2401728 1748 1769 1790 1811 1831 1852 1873 1894 1914 436243 246 249 252 255 258 260 263 266 2691935 1956 1976 1997 2017 2038 2059 2079 2100 2120 439

272 275 277 280 283 286 289 291 294 2972141 2161 2181 2202 2222 2243 2263 2283 2304 2324 441300 303 305 308 311 314 316 319 322 3252344 2365 2385 2405 2425 2446 2466 2486 2506 2526 443327 330 333 336 338 341 344 347 349 3522547 2567 2587 2607 2627 2647 2667 2687 2707 2727 445355 357 360 363 366 368 371 374 376 3792747 2767 2787 2807 2827 2846 2866 2886 2906 2926 447382 384 387 390 392 395 398 400 403 4062946 2965 2985 3005 3025 3044 3064 3084 3103 3123 449408 411 414 416 419 422 424 427 429 4323143 3162 3182 3201 3221 3240 3260 3279 3299 3318 451435 437 440 442 445 448 450 453 455 458

3338 3357 3377 3396 3416 3435 3454 3474 3493 3512 452461 463 466 468 471 473 476 479 481 4843532 3551 3570 3590 3609 3628 3647 3666 3686 3705 454486 489 491 494 496 499 501 504 507 5093724 3743 3762 3781 3800 3820 3839 3858 3877 3896 456512 514 517 519 522 524 527 529 532 5343915 3934 3953 3972 3991 4009 4028 4047 4066 4085 458537 539 542 544 547 549 551 554 556 5594104 4123 4141 4160 4179 4198 4217 4235 4254 4273 459561 564 566 569 571 574 576 579 581 5834291 4310 4329 4347 4366 4385 4403 4422 4440 4459 460586 588 591 593 596 598 600 603 605 6084477 4496 4514 4533 4551 4570 4588 4607 4625 4643 461

610 612 615 617 620 622 625 627 629 6324662 4680 4699 4717 4735 4753 4772 4790 4808 4826 462634 636 639 641 644 646 648 651 653 655..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+8..%168170172PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON TOTAL..ANTI..ICE..ONAND..CARGO..COOL..ON166



1441461481501521541561581601621641.81261281301321.0 1.21421.4 1.61341361381400 .2 .4 .6 .8

INTEGRATED CRUISEMAX. CRUISE THRUST LIMITS DISTANCELR FL 370 NORMAL AIR CONDITIONING ISA (NM)ANTI-ICING OFF CG = 37,0 % TIME (MIN)FIGURE 033-55

033 PICTURE SUPPLEMENTS146© 2008AVIATIONEXAM.comWEIGHT TAS(1000 KG) (KTS)4845 4863 4881 4899 4917 4936 4954 4972 4990 5008 463

658 660 662 665 667 670 672 674 677 8795026 5044 5062 5080 5098 5116 5134 5152 5170 5188 464881 684 686 688 691 693 695 698 700 7025206 5224 5241 5259 5277 5295 5313 5331 5348 5366 465705 707 709 711 714 716 718 721 723 7255384 5402 5419 5437 5455 5473 5490 5508 5525 5543 465728 730 732 734 737 739 741 743 746 7485561 5578 5596 5613 5631 5649 5666 5684 5701 5719 466750 753 755 757 759 762 764 766 768 7745756 5753 5771 5788 5806 5823 5840 5858 5875 5892 466773 775 777 780 782 784 786 789 791 7936010 5927 5944 5962 5879 5996 6013 6031 6048 6065 466795 797 800 802 804 806 809 811 813 815

6082 6099 6116 6133 6151 6168 6185 6202 6219 6236 467817 820 822 824 826 828 831 833 835 8376253 6270 6287 6304 6321 6338 6355 6372 6388 6405 467839 842 844 846 848 850 852 855 857 8596422 6439 6456 6473 6490 6506 6523 6540 6557 6573 467861 863 865 869 870 872 874 876 878 8816590 6607 6623 6640 6857 6673 6690 6707 6723 6740 468883 885 887 889 891 893 895 898 900 9026757 6773 6790 6806 6823 6839 6856 6872 6888 6905 468904 906 908 910 912 915 917 919 921 923



6921 6930 6954 6070 6987 7003 1011 7035 7052 7068 468925 927 929 931 933 936 938 940 942 9447084 7100 7117 7133 7149 7165 7181 7197 7213 7219 469946 948 950 952 954 956 958 960 962 9647245 7261 7277 7293 7309 7325 7341 7357 7373 7389 470967 969 971 973 975 977 979 981 983 9857405 7420 7436 7452 7468 7484 7490 7515 7531 7546 471987 989 991 993 995 997 999 1001 1003 10057562 7578 7593 7609 7624 7640 7656 7671 7687 7702 4711007 1009 1011 1013 1015 1017 1019 1021 1023 10257718 7733 7749 7764 7779 7795 7810 7825 7841 7856 4711027 1029 1031 1033 1035 1037 1039 1041 1042 10447871 7887 7902 7917 7932 7948 7963 7978 7993 8008 4711046 1048 1050 1052 1054 1056 1058 1060 1062 10648023 8038 8053 8068 8083 8098 8113 8128 8143 8158 4711066 1068 1070 1071 1073 1075 1077 1079 1081 10838173 8188 8203 8217 8232 8747 8262 8271 8291 8306 4711085 1087 1089 1090 1092 1094 1096 1098 1100 11028321 8335 8350 8365 8379 4711104 1105 1107 1109 1111AND..CARGO..COOL..ON..FUEL..=....0,4..% ..FUEL..=..+1..% ..FUEL..=..+1,5..% ..FUEL..=..+6..%TOTAL..ANTI..ICE..ON204

206208210212214216218PACK..FLOW..LO PACK..FLOW..HI..OR/ ENGINE..ANTI..ICE..ON202180182184186

1881901921941961982001.4 1.6 1.8174176178CG = 37,0 % TIME (MIN)0 .2 .4 .6 .8 1.0 1.2

INTEGRATED CRUISEMAX. CRUISE THRUST LIMITS DISTANCELR FL 370 NORMAL AIR CONDITIONING ISA (NM)ANTI-ICING OFFFIGURE 033-56




WEIGHT TAS(1000 KG) (KTS)4555 4572 4589 4607 4624 4641 4658 4675 4692 4710 444672 674 677 679 681 684 686 688 690 6934727 4744 4761 4778 4795 4812 4829 4846 4863 4880 446695 697 700 702 704 707 709 711 713 7164897 4914 4931 4948 4965 4982 4999 5016 5033 5050 448718 720 723 725 727 729 732 734 736 7385067 5084 5101 5117 5134 5151 5168 5185 5201 5218 449741 743 745 747 750 752 754 756 759 7615235 5252 5268 5285 5302 5319 5335 5352 5369 5385 451763 765 768 770 772 774 776 779 781 7835402 5419 5435 8452 5468 5485 5501 5518 5535 5551 453785 787 790 792 794 796 798 801 803 8055568 5584 5601 5617 5634 5650 5666 5683 5699 5716 454807 809 812 814 816 818 820 822 825 8275732 5749 5765 5781 5798 5814 5830 5847 5863 5879 456829 831 833 835 837 840 842 844 846 8485895 5912 5928 5944 5960 5977 5993 6009 6025 6042 457850 852 855 857 859 861 863 865 867 8696058 6074 6090 6106 6122 6138 6154 6171 6187 6203 458872 874 876 878 880 882 884 886 888 8916219 6235 6251 6267 6283 6299 6315 6331 6347 6363 460893 895 897 899 901 903 905 907 909 911

6379 6395 6411 6427 6442 6458 6474 6490 6506 6522 461914 916 918 920 922 924 926 928 930 9326538 6553 6569 6585 6601 6617 6632 6648 6664 6680 463934 936 938 940 942 944 946 948 950 9536695 6711 6727 6743 6758 6774 6790 6805 6821 6836 464955 957 959 961 963 965 967 969 971 9736852 6868 6883 6899 6914 6930 6946 6961 6977 6992 465975 977 979 981 983 985 987 989 991 9937008 7023 7039 7054 7070 7085 7100 7116 7131 7147 466995 997 999 1001 1003 1005 1007 1009 1011 10137162 7177 7193 7208 7224 7239 7254 7269 7285 7300 4671015 1017 1019 1021 1023 1025 1027 1029 1030 10327315 7331 7346 7361 7376 7392 7407 7422 7437 7452 468

1034 1036 1038 1040 1042 1044 1046 1048 1050 10527467 7483 7498 7513 7528 7543 7558 7573 7588 7603 4681054 1056 1058 1060 1062 1064 1066 1067 1069 10717618 7633 7648 7664 7679 7694 7708 7723 7738 7753 4691073 1075 1077 1079 1081 1083 1085 1087 1089 10917768 7783 7798 7813 7828 7843 7858 7873 7887 7902 4701092 1094 1096 1098 1100 1102 1104 1106 1108 11107917 7932 7947 7962 7976 7991 8006 8021 8035 8050 4701111 1113 1115 1117 1119 1121 1123 1125 1126 11288065 8080 8094 8109 8124 8138 8153 8168 8182 8197 4711130 1132 1134 1136 1138 1140 1141 1143 1145 1147AND CARGO COOL ON.FUEL = -0,4 % .FUEL = +1 % .FUEL = +1,5 % .FUEL = +6 %

TOTAL ANTI ICE ON204206208210212214216218PACK FLOW LO PACK FLOW HI OR/ ENGINE ANTI ICE ON



2021801821841861881901921941961982001.4 1.6 1.8174176178CG = 37,0 % TIME (MIN)0 .2 .4 .6 .8 1.0 1.2INTEGRATED CRUISEE C N A T S I D S T I M I L T S U R H T E S I U R C . X A MLR FL 330 NORMAL AIR CONDITIONING ISAANTI-ICING OFF(NM)FIGURE 033-57

033 PICTURE SUPPLEMENTS148© 2008AVIATIONEXAM.comtime140 150 160 170 180 190 200 210 220 230 240 correction410 2.3 2.4 2.6 2.7 2.7 - - - - - - 5 min390 2.2 2.3 2.5 2.6 2.8 2.9 - - - - - 5 min370 2.1 2.2 2.4 2.5 2.7 2.8 2.9 - - - - 5 min350 2.0 2.1 2.2 2.4 2.5 2.7 2.8 2.9 3.0 3.1 - 6 min330 1.9 2.0 2.1 2.3 2.4 2.5 2.7 2.8 2.9 3.0 3.1 6 min310 1.8 1.9 2.0 2.2 2.3 2.4 2.5 2.7 2.8 2.8 3.0 5 min

290 1.7 1.8 1.9 2.0 2.1 2.3 2.4 2.5 2.6 2.8 2.9 5 min270 1.8 1.7 1.8 1.9 2.0 2.1 2.2 2.4 2.5 2.6 2.7 5 min250 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.4 2.5 4 min200 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 3 min150 1.0 1.1 1.1 1.2 1.3 1.4 1.5 1.5 1.6 1.7 1.8100 0.7 0.8 0.8 0.9 0.9 1.0 1.0 1.1 1.1 1.2 1.3 3 mintime SPEED 140 150 160 170 180 190 200 210 220 230 240 correctionLRC 2.3 2.4 2.6 2.7 2.8 2.8 2.8 3.0 3.0 3.0 3.0 6 minM.80 2.3 2.4 2.6 2.6 2.7 2.8 2.8 3.0 3.0 3.0 3.0 6 minM.82 2.2 2.4 2.6 2.6 2.6 2.8 2.8 2.9 3.0 3.0 3.0 6 minM.84 2.2 2.3 2.4 2.5 2.5 2.5 2.6 2.7 2.8 2.8 2.8 7 minFL WEIGHT AT BRAKE RELEASE (1000 kg)CORRECTION ON FUEL CONSUMPTION (1000 kg)

WEIGHT AT BRAKE RELEASE (1000 kg)CORRECTION ON FUEL CONSUMPTION (1000 kg)CLIMB CORRECTIONThe planner must correct the values for the fuel and the time obtained from theintegrated cruisetables with the numbers given in the following tables. The tables which are established for M.80,M.82, M.84 and long range speed take into account climbing from the brake release point at250KT/300KT/M.80.



CLIMB TO OPTIMUM FLSTEP CLIMB CORRECTIONWhen the flight includes one or more step climbs (2000 feet below FL290, 4000 feet above), applya correction of 160 kg per step climb to the fuel consumption.3 minFIGURE 033-58

033 PICTURE SUPPLEMENTS149© 2008AVIATIONEXAM.comtime130 140 150 160 170 180 190 correction290and 0.6 0.7 0.7 0.8 0.9 1.0 1.1 10 minabove270 0.6 0.7 0.7 0.8 0.9 0.9 1.0250 0.6 0.6 0.7 0.7 0.8 0.8 0.9200 0.5 0.6 0.6 0.7 0.7 0.8 0.8 8 min150 0.5 0.5 0.6 0.6 0.6 0.7 0.7100 0.4 0.4 0.4 0.5 0.5 0.5 0.5FLWEIGHT OVERHEAD DESTINATION (1000 kg)

CORRECTION ON FUEL CONSUMPTION (1000 kg)DESCENT CORRECTIONCorrect the fuel and the time values determined in the integrated cruise tablesas follows totake into account the descent down to 1500 feet followed by 6 min IFR approach and landing.LONG RANGE CRUISELRC, M.80, M.82, M.84 FROM OPTIMUM FLtime130 140 150 160 170 180 190 correction0.6 0.7 0.8 0.9 1.0 1.0 1.1 11 minWEIGHT OVERHEAD DESTINATION (1000 kg)CORRECTION ON FUEL CONSUMPTION (1000 kg)

FIGURE 033-59

033 PICTURE SUPPLEMENTS150© 2008AVIATIONEXAM.comDIS.FL310 FL350 FL390FL330 FL370 FL41032826 31906 30946 30195 29491 28976 137 139 1457.37 6.47 6.38 6.27 6.18 6.1434032 33058 32067 31285 30555 30024 141 142 1517.30 7.00 6.51 6.40 6.31 6.27

35244 34211 33245 32379 31624 31077 150 147 1577.44 7.14 7.04 6.53 6.44 5.4036570 35370 34378 33478 32698 32135 155 149 1547.54 7.29 7.17 7.06 6.57 6.6337607 36603 35517 34584 33778 33198 160 153 1708.07 7.47 7.30 7.16 7.10 7.0539050 37728 36661 35694 34864 34269 159 158 1775.20 7.55 7.43 7.32 7.23 7.1840300 38957 37810 36810 35956 35346 154 163 1848.33 8.09 7.67 7.45 7.35 7.31



41559 40142 38965 37931 37054 36430 158 167 1918.45 8.22 8.10 7.58 7.48 7.4442921 41333 40125 39057 38157 37518 173 172 2005.58 8.36 8.23 8.10 8.01 7.5744069 42528 41291 40189 39265 38613 178 177 2089.10 8.49 8.36 8.23 8.14 8.0945322 43734 42464 41327 40380 39714 183 182 2159.23 9.03 8.49 8.36 8.27 8.2246580 44946 43640 42471 41502 40823 187 187 2239.35 9.16 9.02 8.49 8.39 8.3547844 46165 44820 43618 42629 41938 191 193 2319.48 9.29 9.15 9.01 8.52 8.4849114 47389 46006 44764 43763 43090 194 198 23810.00 9.42 9.28 9.14 9.05 9.00*50391 48620 47198 45915 44900 44238 198 203 24610.12 9.55 9.41 9.27 9.17 9.13*51673 49857 48396 47021 46042 45391 201 208 25410.24 10.08 9.53 9.40 9.30 9.26*52961 51100 49600 48233 47191 46550 205 214 26110.36 10.22 10.06 9.53 9.43 9.39*54256 52349 50810 49401 48348 47715 208 220 26910.48 10.35 10.19 10.05 9.56 9.52*55557 53604 52026 50574 49511 48886 213 225 27711.00 10.47 10.32 10.18 10.08 10.05*

56860 54867 53248 51752 50680 50063 217 231 28311.12 11.00 10.45 10.31 10.21 10.18*58152 56135 54477 52936 51856 51245 222 237 29011.26 11.13 10.57 10.43 10.34 10.31*59449 57407 55713 54126 53037 52432 227 243 29711.39 11.26 11.10 10.56 10.46 10.44*60751 58682 56955 55323 54265 53626 232 249 30411.52 11.39 11.23 11.09 10.59 10.56*62059 59963 58196 56525 55467 54826 237 256 31212.06 11.52 11.36 11.21 11.12 11.09*63371 61250 59442 57736 56675 56033 242 263 32112.19 12.05 11.48 11.34 11.24 11.22*64689 62544 60694 58962 57890 57245 247 273 327

12.33 12.17 12.01 11.47 11.37 11.35*330 350 370 390 4103500360037003800310.FUEL = -0,4 %51004000410042004300

44004500460047005300FLIGHT LEVELCORRECTION ONFUEL CONSUMPTION(KG/1.000 KG)5200



48004900500039003300280029003000310032003400FLIGHT PLANNING FROM BREAKE RELEASE TO LANDINGCLIMB: 250KTS/300KTS/M.80 - LONG RANGE CRUISE - DESCENT: M.80/300KTS/250KTSIMC PROCEDURE: 240 KG (6 MIN)TOTAL ANTI ICE ON PACK FLOW LOAIR(NM)TIME (H.MIN)FUEL CONSUMED (KG) ISACG = 37,0 %REF. LANDING WEIGHT = 140.000 KGNORMAL AIR CONDITIONINGANTI ICING OFF.FUEL = +5 %

ENGINE ANTI.FUEL = +1,5 %PACK FLOW HI OR/AND.FUEL = +1 %CARGO COOL ON ICE ONFIGURE 033-60

033 PICTURE SUPPLEMENTS151© 2008AVIATIONEXAM.com< <) < <

< <) < << << << << << << << << <FLIGHT PLANPLAN DE VOLPRIORITY

PrioritéADDRESSEE(S)Destinataire(s)FLIGHT TIMEHeure de dépôtORIGINATORExpéditeurSPECIFIC IDENTIFICATION OF ADDRESSEE(S) AND/OR ORIGINATORIdentification précise du(des) destinataire(s) et/ou de l'expéditeur3 MESSAGE TYPE



Type de message7 AIRCRAFT IDENTIFICATIONIdentification de l'aéronefTYPE OF AIRCRAFTType de l'aéronef(FPL4 FLIGHT RULESRegles de volTYPE OF FLIGHTType de vol10 EQUIPMENTÉquipmentWAKE TURBULENCE CAT.Cat. de turbulence de sillage9 NUMBERNombre13 DEPARTURE AERODROMEAérodrome de départTIMEHeure15 CRUISING SPEEDVitesse croisiereLEVELNiveau

ROUTERoute16 DESTINATION AERODROMEAérodrome de destinationTOTAL FEETDurée totale estiméeHR. MIN.ALTN AERODROMEAérodrome de dégagement2ND ALTN AERODROME2eme aérodrome de dégagement18 OTHER INFORMATIONRenseignements divers

SUPPLEMENTARY INFORMATION (NOT TO BE TRANSMITTED IN FPL MESSAGES)Renseignements complémentaires (A NE PAS TRANSMETTRE DANS LES MESSAGES DE PLAN DEVOL DÉPOSÉ)19 ENDURANCEAutonomieEHR. MIN.PERSONS ON BOARDPersonnes a bordP RUHF VHF ELBAJACKETS / Gilets de sauvetageLIGHT

LampesFLUORESFluores UHF VHFSURVIVAL EQUIPMENT / Équipement de surviePOLARPolaireDESERTDésertMARITIMEMaritime



JUNGLEJungleDINGHIES/CanotsNUMBERNombreCAPACITYCapacitéCOVERCouvertureCOLOURCouleurAIRCRAFT COLOUR AND MARKINGS / Couleur et marques de l'aéronefREMARKS / RemarquesPILOT IN COMMAND / Pilote commandant de bordFILED BY / Deposé parSPACE RESERVED FOR ADDITIONAL REQUIREMENTSEspace reserve a des tins supplémentaires

S P D M JD CNCAJ L F UU V EVFF< <

FIGURE 033-61

033 PICTURE SUPPLEMENTS152© 2008AVIATIONEXAM.comINTRODUCTIONThe following flight planning tables allow the planner to determine trip fuel consumption andtrip time required to cover a given air distance.These tables are established for:- Takeoff- Climb profile: 250 kts/300 kts/M.80

- Cruise mach number: M.80, M.82, M.84, LR- Descent profile: Cruise Mach number/300 kts/250 kts- Approach and landing: 240 kg 6 minute IFR- ISA- CG = 37%- Normal air conditioning- Anti ice OFFNote:1. In the tables, the asterisk (*) means that a step climb of 4.000 feet must be flown to



reach the corresponding FL.2. To obtain a flight plan at optimum cruise level, the highest flight level desired withinthe flight has to be selected in the table.3. For each degree Celsius above ISA temperature apply fuel correction0,010(kg/°C/NM) x . ISA(°C) x Air Distance (NM).CORRECTION FOR DEVIATION FROM REFERENCE LANDING WEIGHTThe fuel consumption must be corrected when the actual landing weight is different from thereference landing weight. If it is lower (or greater) than the reference landing weight, subtract(or add) the value given in the correction part of the table per 1000 kg below (or above) thereference landing weight.EXAMPLEThe following is an example of a complete flight plan based on the assumptions:- Zero fuel weight (OWE + PAYLOAD): 160.000 kg = landing weight at alternate airport- Cruise M.82 at FL390- Ground distance from departure to destination: 2.500 NM- Average wind during flight: -50 kts (headwind)- ISA conditions- Enroute reserve: 5 %- Ground distance from destination to alternate: 200 NM, no wind at FL200

To calculate the flight plan, a reverse calculation is needed, i.e. start with the landing weightat alternate.FIGURE 033-62

033 PICTURE SUPPLEMENTS153© 2008AVIATIONEXAM.comFUEL TANKERINGGENERALFuel tanking graphs allow to determine the Optimum fuel quantity to be tanked as a function of the fuel

price ratio between departure and destination airports. The following pages present for one flight levelper page the Optimum aircraft takeoff weight depending on the fuel price ratio (departure fuel pricedivided by destination fuel price) and on the air distance to fly.The computed optimum takeoff weight is based on the additional fuel consumptionneeded for thetransport of the extra (tanked) fuel and it is the weight at which the maximum profit can be achieved. Thequantity of extra fuel that can be loaded is calculated as the difference between the Optimum takeoffweight (including extra fuel) and the planned takeoff weight (without fuel tanking).

The graphs are established for:FL290, 310, 330, 350, 370, 390Air distances from 500 to 5.000 NMFlight profile:Climb 250 kts/300kts/M.80Cruise M.80Descent M.80/300 kts/250 ktsNote:1. If necessary, step climbs are performed to reach the indicated flight levels.



2. The crew/operator has to verify that the found aircraft weight complies withbasic aircraftlimitations (e.g. max fuel capacity) as well as with mission dependent restrictions (e.g. MLWat destinations).EXAMPLES1.Fuel price ratio = 0.930Cruising Altitude = FL310Planned TOW = 200.000 kg (mission weight without fuel tanking)Air Distance = 2500 NMEnter graphFor the given air distance, the optimum fuel tanking weight is 187.000 kg, which is lower than theplanned takeoff weight, no fuel tanking recommended.2. Fuel price ratio = 0.890Cruising Altitude = FL350Planned TOW = 190.000 kg (mission weight without fuel tanking)Air Distance = 3.250 NMEnter graphFor the given air distance, the optimum fuel tanking weight is 198.000 kg, which is 8.000 kg higher thanthe planned takeoff weight, optimum quantity of extra fuel is 8.000 kg.Check:a) New TOW less or wqual MTOW from departure airport.

b) Total fuel to be loaded less or equal maximum fuel capacity.c) MLW at destination.FIGURE 033-63

033 PICTURE SUPPLEMENTS154© 2008AVIATIONEXAM.comNGM = NAM x(TAS +/- WIND)TASDETAILED FUEL PLANNINGEn-route Climb

Tables are provided for a range of temperature deviations from ISA -15°C to ISA +25°CFuel and time given in these tables are from brake release and distance from 1.500 ft.With a climb airspeed schedule 280 KIAS / 0,74 Mach.The stated TAS is the average for the climb and should be used to correct the still airdistance shown.Off-OptimumConditionFuel Mileage Penalty %LRC or Mach 0.74 Mach 0.782,000 ft above -1 -1

Optimum 0 02,000 ft below -1 -24,000 ft below -4 -48,000 ft below -10 -1112,000 ft below -15 -20Off-Optimum Fuel PenaltyAscension Island Ghana Irish Republic *+ Morocco Sierra LeoneBurkina-Faso Great Britain + Ivory Coast Portugal *+ Togo RepublicCanary Islands * Guinea-Bissau Liberia Principe Tristan da CunhaChannel Islands + Guinea Republic Madeira * St. Helena



Faeroes *, The Iceland Mali Sao TomeGambia, The Ireland, Northern + Mauritania Senegal+ The European Union directive states that Summer Time, one hour in advance of UTC, is kept from2001 March 25th 01h to October 28th 01h UTC.STANDARD TIMES (Corrected to November 1999)LIST II - PLACES NORMALLY KEEPING UTC* Summer time may be kept in these places.FIGURE 033-64FIGURE 033-65FIGURE 033-66

033 PICTURE SUPPLEMENTS155© 2008AVIATIONEXAM.comSTANDARD TIMES (Corrected to November 1999)LIST I PLACES FAST ON UTC (mainly those EAST OF GREENWICH)The times given below should be added to UTC to give Standard Time subtracted from Standard Time to give UTC.h m h mAdmiralty Islands 10 Denmark *+ 01Afghanistan 04 30 Djibouti 03Albania * 01

Algeria 01 Egypt, Arab Republic of * 02Amirante Islands 04 Equatorial Guinea, Republic of 01Andaman Islands 05 30 Eritrea 03Angola 01 Estonia * 02Armenia * 04 Ethiopia 03AustraliaAustralian Capital Territory * 10 Fiji * 12New South Wales 1 * 10 Finland *+ 02Northern Territory 09 30 France *+ 01Queensland 10South Australia * 09 30 Gabon 01Tasmania * 10 Georgia * 04Victoria * 10 Germany *+ 01

Western Australia 08 Gibraltar * 01Whitsunday Islands 10 Greece *+ 02Austria *+ 01 Guam 10Azerbaijan * 04Hong Kong 08Hungary * 01Bahrain 03Balearic Islands * 01 India 05 30Bangladesh 06 Indonesia, Republic ofBelarus * 02 Bangka, Billiton, Java, West andBelgium *+ 01 Central Kalimantan, Madura, Sumatra 07Benin 01 Bali, Flores, South and EastBosnia and Herzegovina * 01 Kalimantan, Lombok, Sulawesi,

Botswana, Republic of 02 Sumba, Sumbawa, Timor, 08Brunei 08 Aru, Irian Jaya, Kai, Moluccas,Bulgaria * 02 Tanimbar 09Burma (Myanmar) 06 30 Iran * 03 30Burundi 02 Iraq * 03Israel * 02Italy *+ 01Cambodia 07Cameroon Republic 01 Jan Mayen Island 01Japan 09



Jordan * 02Caroline Islands 2 10Kazakhstan *Central African Republic 01Western, Aktau, Uralsk, Atyrau 04Chad 01Central, Aktyubinsk, Kzyl-Orda 05Chagos Archipelago 05Eastern 06Chatham Islands * 12 45Kenya 03China, Peoples Republic of 08Kiribati RepublicChristmas Island, Indian Ocean 07Gilbert Islands 12Cocos (Keeling) Islands 06 30Phoenix Islands 13Comoro Islands (Comoros) 03Line Islands 3 14Congo, Democratic RepublicKorea, North 09Kinshasa, Mbandaka 01Republic of (South) 09Haut-Zaire, Kasai, Kivu, Shaba 02

Kuril Islands 11Congo Republic 01Kuwait 03Corsica * 01Kyrgyzstan * 05Crete * 02Croatia * 01Laccadive Islands 05 30Cyprus, Ercan *, Larnaca * 02Laos 07Czech Republic 01Latvia * 02* Summer time may be kept in these places. + For Summer time dates see List II

1 Except Broken Hill Area which keeps 09h 30m.2 Except Pohnpei, Pingelap and Kosrae which keep 11h.3 The Line Islands that are not part of the Kiribati Republic keep 10h slow on UTC.*FIGURE 033-67

033 PICTURE SUPPLEMENTS156© 2008AVIATIONEXAM.comSTANDARD TIMES (Corrected to November 1999)LIST I (continued)

h m h mLebanon * 02 Russia (continued)Lesotho 02 Zone 7 Bratsk, Irkutsk, Ulan-Ude 08Libya 02 Zone 8 Yakutsk, Chita, Tiksi 09Liechtenstein * 01 Zone 9 Vladivostok, Khabarovsk,Lithuania * 02 Okhotsk 10Lord Howe Island * 10 30 Zone 10 Magadan, Yuzhno 11Luxembourg *+ 01 Zone 11 Petropavlovsk, Pevek 12Rwanda 02Macau 08 Ryukyu Islands 09



Macedonia * former Yugoslav Republic 01Macias Nguema (Fernando Póo) 01 Sakhalin Island * 10Madagascar, Democratic Republic of 03 Santa Cruz Islands 11Malawi 02 Sardinia * 01Malaysia, Malaya, Sabah, Sarawak 08 Saudi Arabia 03Maldives, Republic of The 05 Schouten Islands 10Malta * 01 Serbia * 01Mariana Islands 10 Seychelles 04Marshall Islands 112 Sicily * 01Mauritius 04 Singapore 08Moldova * 02 Slovakia * 01Monaco * 01 Slovenia * 01Mongolia 08 Socotra 03Mozambique 02 Solomon Islands 11Somalia Republic 03Namibia * 01 South Africa, Republic of 02Nauru 12 Spain *+ 01Nepal 05 45 Spanish Possessions in North Africa * 01Netherlands, The *+ 01 Spitsbergen (Svalbard) * 01New Caledonia 11 Sri Lanka 06New Zealand * 12 Sudan, Republic of 02Nicobar Islands 05 30 Swaziland 02Niger 01 Sweden *+ 01

Nigeria, Republic of 01 Switzerland * 01Norfolk Island 11 30 Syria (Syrian Arab Republic) * 02Norway * 01Novaya Zemlya 03 Taiwan 08Tajikistan 05Okinawa 09 Tanzania 03Oman 04 Thailand 07Tonga * 13Pagalu (Annobon Islands) 01 Tunisia 01Pakistan 05 Turkey * 02Palau Islands 09 Turkmenistan 05Papua New Guinea 10 Tuvalu 12Pescadores Islands 08

Philippine Republic 08 Uganda 03Poland * 01 Ukraine * 02United Arab Emirates 04Qatar 03 Uzbekistan 05Reunion 04 Vanuatu, Republic of 11Romania * 02 Vietnam, Socialist Republic of 07Russia 2*Zone 1 Kaliningrad 02 Yemen 03Zone 2 Moscow, St. Petersburg, Yugoslavia *, Federal Republic of 01Arkhangelsk, Astrakhan 03Zone 3 Samara, Izhevsk 04 Zambia, Republic of 02Zone 4 Perm, Amderna, Novy Port 05 Zimbabwe 02

Zone 5 Omsk, Novosibirsk 06Zone 6 Norilsk, Kyzyl, Dikson 07* Summer time may be kept in these places. + For Summer time dates see List II1 Except the Ebon Atol which keeps time 24h slow on that of the rest of the islands.2 The boundaries between the zones are irregular, listed are chief towns in each zone.FIGURE 033-68




157© 2008AVIATIONEXAM.comMETAR/TAFPARIS/CHARLES-DE-GAULLELFPG/CDGSA1330 121330Z 27004KT 9999 SCT011 BKN050 09/08 Q1001 NOSIG=FC1100r 120800Z 1200918 30005KT 3500 BR BKN003 BECMG 0911 6000SCT011 SCT050 BECMG 1113 9999 SCT020 BECMG TEMPO 13178000 SHRA SCT025TCU BKN030 T08/12Z T09/15Z=FT1000 121000Z 121812 27008KT 9999 BKN025 BECMG 1821 20005KT SCT030BECMG 2124 6000 BECMG 0002 20008KT 2000 BR BKN005 TEMPO 020820004KT 0500 BCFG OVC001 BECMG 0810 18012KT 9999 SCT012BECMG 1012 SCT020=BORDEAUX/MERIGNACLFBD/BODSA1330 121330Z 21005KT 9000 FEW030TCU FEW033CB SCT040 BKN100 09/08Q1005 TEMPO 25015G25KT 3000 TSRA SCT005 BKN015CB=FC1100r 121100Z 121221 28010KT 9999 RA SCT020 FEW025CB SCT040TEMPO 1218 25015G25KT 6000 SHRA SCT008 SCT020CB BKN033 PROB30TEMPO 1218 28020G30KT 3000 TSRA SCT005 BKN015CB BKN030 BECMG1821 22004KT 8000 NSW FEW006 BKN030=FT1000 122000Z 121812 30010KT 9999 SCT020 FEW025CB BKN040BECMG 1822 22004KT 8000 FEW006 BKN030 BECMG 0306 24005KT 6000

SCT007 SCT015 BKN090 BECMG 1012 RA=LYON/SATOLASLFLL/LYSSA1330 121330Z 14007KT 9000 TSRA FEW020CB SCT033TCU BKN046 09/07Q1003 NOSIG=FC1100r 121100Z 121221 VRB03KT 9999 FEW010 SCT020 BKN040 BECMG 182133006KT TEMPO 1221 VRB15G20KT 4000 SHRA SCT008 BKN015=FT1000 121000Z 121812 33004KT 9999 SCT025 BKN060 BECMG 2224 VRB02KT8000 SCT010 SCT020 BECMG 0204 1500 BR BKN003 TEMPO 0407 0800 FGOVC002 BECMG 0810 33006KT 9999 SCT015 BKN030=FIGURE 033-69


158© 2008AVIATIONEXAM.comMETAR/TAFBALE/MULHOUSELFSB/MLHSA1330 121330Z 23008KT 9999 RA FEW020 SCT030 BKN066 06/05 Q1001 NOSIG=FC1100r 121100Z 121221 18005KT 9000 RA FEW015 BKN030 BKN060TEMPO 1216 NSW BECMG 1517 9999 FEW030 BKN040 BKN080TEMPO 1621 SHRA=DUBAIOMDB/DXBFT1000 121212 33015KT 9999 SCT030 BKN090 TEMPO 1209 5000 SHRA PROB40

TEMPO 1424 VRB40KT 1000 TSSS SCT025CB BECMG 1618 05010KTBECMG 0608 33013G23KT=JOHANNESBURG/JAN SMUTSFAJS/JNBFT0900 120900Z 121212 36010KT 9999 FEW030CB FEW035 PROB40 TEMPO 1318VRB15KT 3000 TSRA SCT030CB BKN080 FM2000 03005KT CAVOKBECMG 0204 SCT008 SCT100 PROB30 0305 3000 BCFG BKN004FM0800 34012KT 9999 SCT025 T25/12Z T15/03Z T27/12Z=TUNIS/CARTHAGEDTTA/TUN



SA1330 121330Z 24008KT 6000 FU FEW023 BKN200 24/08 Q1007=LONDON/HEATHROWEGLL/LHRSA1330 121330Z 28008KT 7500 SCT021 BKN050 04/03 Q1008 NOSIG=FT1000 121000Z 121812 27008KT 9999 BKN025 BECMG 1821 20005KT SCT030BECMG 2024 5000 BECMG 0002 VRB06KT 2200 BR BKN 005 TEMPO 020820003KT 1500 BR OVC002 BECMG 0810 VRB02KT 5500 BKN012BECMG 1012 SCT020 9999=TRUE TRACK / FUELPOSITION DISTANCE CONSUMPTION(litres)2 3 4 D R A124°/1123 3 6 J G T123°/1319 6 8 N E L U BFIGURE 033-70FIGURE 033-71

033 PICTURE SUPPLEMENTS159© 2008AVIATIONEXAM.comEndurance / Fuel Calculation

Fuel (kg) Time (hh:mm)Trip Fuel 5.800 02:32Contingency FuelAlternate Fuel 1.800 00:42Final Reserve Fuel 1.325Minimum T/O FuelExtra FuelActual T/O FuelTaxi Fuel 200Ramp Fuel 10.000CH 000 045 090 135 ...Dev -2 -4 -3 -1Flight Level 40 80 120 160 200

TAS (knots) 190 198 204 212 220Hourly fuel flow (l/hrs) 210 202 182 170 156FIGURE 033-72FIGURE 033-73FIGURE 033-74

033 PICTURE SUPPLEMENTS160© 2008AVIATIONEXAM.comFIGURE 033-75


161© 2008AVIATIONEXAM.comFIGURE 033-76









033 PICTURE SUPPLEMENTS168© 2008AVIATIONEXAM.comSimpli ed Flight Planning Trip Distances 0 NM to 1,000 NMTRIP TIME hr

120320 10 0 -10ISA DEV °CREF LINEREF LINE0 200 400 600 800 1000TRIP DISTANCE NM100100HEAD

TAILWINDkt505002345



678FUEL REQUIRED 1000 kg30 40 50 60LANDING WEIGHT1000 kg1BASED ON:280 / 0.74 CLIMB0.74 / 250 DESCENTPRESSURE ALTITUDE 1000 ftPRESSURE ALTITUDE 1000 ftPRESSUREALTITUDE1000 ft12242081618810121416248

24REF LINE300 kt IAS CRUISEFIGURE 033-83

033 PICTURE SUPPLEMENTS169© 2008AVIATIONEXAM.comCritical Fuel Reserve One Engine Inoperative034

56789FUEL REQUIRED 1000 kg121011121514

131000100HEADTAILWINDkt5050



200 400 600 800 1000 0 1200 1400DISTANCE TO DIVERSION AIRPORT FROM CRITICAL POINT NMREF LINEEmergency descent to 10,000 ftLevel cruise at 10,000 ft250 KIAS descent to 1,500 ft15 minutes hold at 1,500 ftOne missed approach; approach & land5% allowance for wind errorsIncludes APU fuel burn70656055504540ONE ENGINE INOPERATIVEWEIGHT AT CRITICAL POINT 1000 kgINCREASE FUEL REQUIRED BY 0.5% FOR EACH 10°C HOTTER THAN ISA CONDITIONS.IF ICING CONDITIONS EXIST, INCREASE FUEL REQUIRED BY 20% TO ACCOUNT FORENGINE & WING A.I. ON & ICE ACCUMULATION ON UNHEATED SURFACES.ALLOWANCE FOR PERFORMANCE DETERIORATION NOT INCLUDED.COMPARE THE FUEL REQUIRED FROM THIS CHART WITH CRITICAL FUEL RESERVESFOR TWO ENGINES OPERATIVE. USE THE HIGHER OF THE TWO.FIGURE 033-84


AVIATIONEXAM.comCritical Fuel Reserve All Engines Operating03456789FUEL REQUIRED 1000 kg12

1011121514131000100HEADTAILWINDkt

5050200 400 600 800 1000 0 1200 1400DISTANCE TO DIVERSION AIRPORT FROM CRITICAL POINT NMREF LINEEmergency descent to 10,000 ftLevel cruise at 10,000 ft250 KIAS descent to 1,500 ft15 minutes hold at 1,500 ftOne missed approach; approach & land



5% allowance for wind errors70656055504540ALL ENGINES OPERATIVEWEIGHT AT CRITICAL POINT 1000 kgINCREASE FUEL REQUIRED BY 0.5% FOR EACH 10°C HOTTER THAN ISA CONDITIONS.IF ICING CONDITIONS EXIST, INCREASE FUEL REQUIRED BY 18% TO ACCOUNT FORENGINE & WING A.I. ON & ICE ACCUMULATION ON UNHEATED SURFACES.ALLOWANCE FOR PERFORMANCE DETERIORATION NOT INCLUDED.COMPARE THE FUEL REQUIRED FROM THIS CHART WITH CRITICAL FUEL RESERVESFOR ONE ENGINE INOPERATIVE. USE THE HIGHER OF THE TWO.FIGURE 033-85

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