071 - Operational Procedures

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OPERATIONAL PROCEDURESsubj Domanda RispostaA RispostaB RispostaC RispostaD Check

071 A warning device alerts the crew in case of an excessive cabin altitude. This

warning must be triggered on reaching the following altitude:

10000 ft (approx. 3000 m 1!000 ft (approx. !"00 m #000 ft (approx. "!00 m 1"000 ft (approx. 3$00 m

071 An operator shall not operate an aeroplane first issued with an individual

%ertificate of Airworthiness on or after 1 April 1&' which has a maximumcertificated tae)off mass over *700 g' unless it is e+uipped with a cocpitvoice recorder which shall be capable of retaining information recorded during

at least the last:

" hours of its operation. 30 minutes of its operation. "0 hours of its operation. "* hours of its operation.

071The r is of d,namic h,droplaning depends primaril, on the: depth of the standing water on therunwa,.

aircraft-s weight. strength of the headwind. amount of the lift off speed.

071 roducts or materials are considered to be dangerous goods if the products or

materials in +uestion are defined as such b,:

The /%A document entitled

Technical /nstructions for the safetransport of dangerous goods b, air.

The 2 document entitled

4angerous 5oods 6egulations.

The directives of the %ommunit, 2nion. The /ATA document entitled

6egulations governing thetransportation of dangerous goods b,air.

071 /f a pilot has connected the automatic pilot to the g,ro compass (which is

assumed to be operating correctl, and the latter is fitted with a rate correctiondevice which is properl, corrected b, astronomical precession' the coursefollowed b, the aircraft (in still air conditions is a:

great circle. rhumb line. curve of some t,pe or other. spherical flight segment.

071 An aircraft leaves point ($0 0308 on a true heading e+ual to 0&0 whilethe g,ro compass' which is assumed to be operating perfectl, and without an

hourl, rate corrector unit' indicates 000. The aircraft arrives at point 9 ($"0108 on a true heading e+ual to 0&*. n the ourne, from to 9 the g,rocompass remains in free g,ro mode. /f the flight lasted 1 hour 30 minutes' the

g,ro heading at 9 will be:

3"#. 3!*. 003. 33!.

071 A pilot is using a polar stereographic chart whose grid is parallel to the ;eromeridian' with 5rid orth in the direction of the orth geographic pole. /n

polar regions' the pilot stops navigation in free)g,ro mode after leaving the $

microteslas ;one' and the grid heading c ontrolled b, information from theinertial navigation s,stem (/


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071 /n < airspace' the speed reference for turbo)et aircraft is the: ach number. ground speed. true airspeed. indicated airspeed.

071 (?or this +uestion use annex 071)"0#3A To compl, with the approved airlineperations anual in a twin)engine aircraft (1hour !* minutes flight on 1engine at an air speed of !"0 t to reach the alternate aerodromes in still air

conditions' a pilot has to choose an AT% route' in inimum avigationerformance 13. >73.*. )3".*.

071 n a polar stereographic chart where the earth convergence between " points

located on the parallel $0 is "0' the great circle maximum cross)tracdifference with the straight line oining the " points is:

30 . !.0 . &." . !.0 .

071 /n a polar Antarctic regions' the pilot uses a


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071 ?or an operation in < airspace along notified special routes unless

otherwise specified' an aircraft must be e+uipped with at least:

ne Gong 6ange avigation


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071 An aeroplane is operated over water at a distance of 3!0 awa, from an

aerodrome where an emergenc, landing could be performed. ormal cruisingspeed is 1#0 t. ne engine out airspeed is 1** t' and it is capable to oin thediversion aerodrome.

Gife acets must be available for all

occupants.

The regulation does not re+uire life

acets or rafts to be taen on board inthis particular case.

Gife acets and rafts must be available

for all occupants.

Gife rafts must be available for all

occupants.

071 The wae turbulence is the most severe when the aircraft is: 1. slow ". heav,3. in a clean configuration !. fl,ing with a high thrust The combination of

correct statement is:

1' "' 3 1' ! 1' "' 3' ! "' 3' !

071 The < (inimum avigation erformance


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is to be carried out at ?G "&0' this demonstration must be completed before:

071 8hat is the transponder code to be used b, the commander of an aircraft that issubect to unlawful interference (hiaced J:

A 7*00 A 7$00 A 7700 A 7#00

071 The validit, period of a nigh)time organised trac s,stem in < (inimumavigation erformance


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071 A categor, /// A precision approach (%AT /// A is an approach which ma, be

carried out with a runwa, visual range of at least:

"00 m 100 m "*0 m *0 m

071 A categor, /// C precision approach (%AT /// C is an approach which ma, be

carried out with a runwa, visual range of at least:

7* m 1*0 m "*0 m "00 m

071 8ith the %ontrol 4ispla, 2nit (%42 of an /nertial avigation


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flight using the T< (rganised Trac


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071 8hen establishing an instrument approach procedure' * aircraft categories

according to their speed at the threshold (Hat are established. This speed ise+ual to the stalling speed in the landing configuration at the maximumcertified landing mass multiplied b, a factor of:

1.3 1.!* 1.* 1.1*

071 /n the absence of wind and without the astronomic precession effect' anaircraft would' at a constant g,ro heading' follow a:

great circle line rhumb line spherical flight segment straight map line

071 osit: g' the longitude difference Gm' the average latitude Go' the latitude ofthe tangent The transport precession is e+ual to:

g.sin Gm 1*Ih.sin Gm g.(sin Gm)sin Go gI".sin Gm

071 osit: g' the longitude difference Gm' the average latitude Go' the latitude ofthe tangent The correct formula of the conversion angle applied' during atransoceanic and polar navigation' is e+ual to:

gI".sin Gm 1*Ih.sin Gm g.sin Gm g.(sin Gm)sin Go

071 4uring a transoceanic and polar flight' the transport precession is the rotationin degrees of the g,ro orth with respect to the:

true orth grid orth magnetic orth compass orth

071 4uring a transoceanic and polar flight' the chart precession is a rotation indegrees' for a moving aircraft' of the g,ro orth with respect to the:

grid orth for a given chart grid orth for an, chart true orth for a given chart true orth for an, chart

071 Astronomic precession is: existing whether the aircraft is on theground or fl,ing

inde pe nde nt of the latitude depending on the chart used ;ero when the aircraft is on the ground

071 osit: g' the longitude difference Gm' the average latitude Go' the latitude ofthe tangent The correct formula expressing the travel precession applied duringa transoceanic and polar navigation' is e+ual to:

1*Ih.sin Gm g.sin Gm g.(sin Gm)sin Go gI".sin Gm

071 Astronomic precession: causes an apparent spin of headingg,ro to the left in the southernhemisphere

causes an apparent spin of heading g,roto the right in the southern hemisphere

is ;ero at the orth pole is ;ero at the


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071ne of the ma in c ha ra cteri st ic s of windshea r i s tha t i t: c an oc cur a t a n, a lti tude in both the

vertical and hori;ontal planes

occurs onl, at a low altitude ( "000 ft

and never in the vertical plane

occurs onl, at a low altitude ( "000 ft

and never in the hori;ontal plane

can occur at an, altitude and onl, in

the hori;ontal plane

071 A polar trac is a trac part of which is included in an area where the

hori;ontal component of the earth magnetic field is less than:

$ micro)tesla 17 micro)tesla 3# micro tesla 10 micro)tesla

071 8hich parameter will change first' when penetrating an hori;ontal windshear J /ndicated airspeed. itch angle. Hertical speed. 5roundspeed.

071 8ae turbulence ris is highest: when a heav, aircraft has ustperformed a tae)off at a closel,situated parallel runwa, with a light

crosswind.

if' ust before landing a much lighteraircraft has landed at the same runwa,with heav, c rosswind.

following a preceding aircraft at highspeed.

when a preceding aircraft has briefl,applied tae)off thrust ust prior to taeoff.

071 The accumulation of frost' snow or ice on an aeroplane in flight induces an

increase in the:

stalling speed value of the stall angle of attac tuc under roll rate

071 The regulations for transportation of dangerous goods are contained in: /%A Annex 1# /%A Appendix # the 8ashington %onvention /%A Annex 17

071 /%A (/nternational %ivil Aviation rgani;ation Appendix 1# is a documentdealing with:

the safet, of the air transport ofdangerous goods

the air transport of live animals the noise pollution of aircraft the technical operational use of a ircraf t

071 Arriving at the point of entr, into < (inimum avigation erformance


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071 According to the FA6 < 1' when a commercial transport passenger aircraft

is e+uipped with a door in the flight crew compartment area' this door mustinclude:

a locing s,stem to prevent an,

unauthori;ed access.

a device preventing the flight crew

from being loced in the cocpit.

distinctive red or ,ellow coloured

marings indicating the access area (incase of a bloced door.

a sealing s,stem which' in case of

depressurisation in the compartmentarea allows the maintenance of the

pressure in the cocpit for as long aspossible.

071 8hen a commander of an aircraft notices' after tae)off' a floc of birds

presenting a bird strie ha;ard' heIshe shall:

immediatel, inform the local ground

stationIAT< unit.

inform the other aircraft b, radio. inform the appropriate ground station

within a reasonable period of time.

submit a written ha;ard bird strie

report upon arrival and within at most!# hours.

071 Bour flight manual does not include specific supplementar, information on

landing distances on wet runwa,s and the service bulletins or weather reportsindicate that the runwa, ma, be wet at the estimated time of arrival. The

re+uired landing distance on a dr, runwa, must be increased b,:

1* K 1# K "0 K 17'$ K

071 /n the FA6


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071 8hile approaching a mountainous airfield' the captain of a transport aircraft

notices a fast and high increase in the indicated airspeed without an, change inthe pre)selected engine and attitude parameters. The preceding crews hadreported the occurrence of windshears in final phase. ,ou must:

maintain the aircraft on the glide path'

accept a positive speed deviation'monitor the speed evolution.

reduce rapidl, the selected thrust'

maintain on the glide path.

tae a level flight attitude to reduce

speed' then come bac to glide path fromabove.

reduce rapidl, the selected thrust in

order to reach 1." Hs and tr, aprecision landing.

071 The highest ris of bird stries occurs: under *00 m above 1 000 m between *00 and 1 000 m between *00 and 1 *00 m

071 8hile approaching the outer)marer' the tower informs ,ou about the presenceof a microburst. Bou will expect to encounter:

windshears (vertical and hori;ontal. wae turbulence . supercooled water. convection motion of air mass.

071/f obliged to ettison part of the fuel in flight' it would be better to do so: in a straight line and at a relativel,

high flight level.

in a holding stac' after control

clearance.

under f light level *0 (?G*0. during f inal phase of approach.

071 /f ,ou encounter a microburst ust after taing)off' at the beginning ,ou will

have: 1 ) a head wind " ) a strong rear wind 3 ) better climb performances ! ) adiminution of climb gradient * ) an important thrust drop The combination

regrouping all the correct statements is:

1'3 "'! 1'! !'*

071 8hen taing)off' in winter conditions' the wing contamination b, ice or frostwill cause the following effects: 1 ) an increase in the tae)off distance " ) adecrease of the tae)off run 3 ) an increase in the stalling speed ! ) a decreaseof the stalling speed * ) a decrease of the climb gradient The combination


1' 3' * "' !' * 1' "' 3 "' 3' *

071 The application of a t,pe // anti)icing fluid on an aircraft on ground willprovide a:

l imi te d holdove r t ime . protec tion time up to "! hours . l imi te d t ime of protec tion inde pe nde nt ofthe outside temperature.

protection against icing for theduration of the flight.

071 An operator shall not operate an aeroplane first issued with an individual

%ertificate of Airworthiness on or after 1 April 1&' which has a maximumcertificated tae)off mass over *700 g' unless it is e+uipped with a cocpitvoice recorder which records: 1 ) Hoice communications transmitted from orreceived on the flight dec b, radio " ) The aural environment of the flight

dec 3 ) The cabin attendants communications in the cabin using theaeroplane-s interphone s,stem ! ) Hoice communications of flight crewmembers on the flight dec using the aeroplane-s interphone s,stem * ) Hoice

or audio signals identif,ing navigation or approach aids introduced into aheadset or speaer $ ) Hoice communications of flight crew members on theflight dec using the public address s,stem' if installed The combinationregrouping all the correct statements is:

1' "' !' *' $ 1' "' 3' *' $ "' 3' !' $ "' !' *' $

071 An operator shall not operate an aeroplane unless it is e+uipped with a cocpitvoice recorder which starts to record automaticall,:

prior to the aeroplane moving under itsown power until the termination of theflight when the aeroplane is no longer

capable of moving under its ownpower.

when the paring brae is released untilthe termination of flight when the

paring brae is set.

when full thrust is applied until thetermination of the flight when theaeroplane is no longer capable of moving

under its own power.

prior to the aeroplane moving under itsown power until the termination offlight when the paring brae is set.

071 The operations re+uirements in regard to the suppl, of ox,gen' for apressuri;ed aeroplane intended to be operated at ?G "$0' 1*0 passengers onboard are . As concerns the regulator, re+uirements about ox,gen: 1. each

crew member will have available a +uic donning t,pe of mas. ". the aircraft

will be e+uipped with a warning s,stem indicating that the cabin altitude ishigher than 13 000ft. 3 . the +uantit, of ox,gen on board shall be sufficient forthe suppl, of 100 K of the occupants during the whole flight time at cabin

pressure altitude above 1* 000 ft (not less than 10 minutes. !. the first aid+uantit, of ox,gen shall be sufficient for the suppl, of two passengers duringthe whole flight time when the cabin altitude is greater than # 000 feet. The

combination regrouping all the correct statements is:

1'3 1'"'3'! "' 3 3'!

071 /n accordance with FA6)< 1.!30 (Aerodrome perating inima' thelowest minima to be used b, an operator in a categor, C aeroplane for circling

are:

4E@*00 ft and visibilit,@1$00 m 4E@!00 ft and visibilit,@1*00 m 4E@$00 ft and visibilit,@"!00 m 4E@700 ft and visibilit,@"$00 m

071 FA6 < 1.!$* (H?6 perating minima' establishes that' the operator shall

ensure about H?6 flights' that:

special H?6 flights are not

commenced when visibilit, is lessthan 3 m

for conducted H?6 flights in airspace

C' hori;ontal distance from clouds is 1000 m at least

for conducted H?6 flights in airspace ?'

vertical distance from clouds is "*0 m atleast

for conducted H?6 flights in airspace

=' flight visibilit, at and above 3 0*0m. (10 000 ft is * m at least (clear ofcloud


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071 /n accordance with FA6 < 1(Aerodrome perating inima' the %ategor,

/// A approach and landing' the 6H6 shall not be less than:

"00 m "*0 m "30 m 300 m

071 According with the noise abatement tae)off and climb procedure C' as

established in /%A A< < #1$# ) ps Holume 1' part H' aircraft mustclimb at H" > 10 to "0 t' until reaching:

1 000 ft *00 ft 1 *00 ft 3 000 ft

071 /n accordance with FA6)< 1.!30 (Aerodrome perational inima' an

operator must ensure that s,stem minima for non)precision approachprocedures' which are based upon the use of /G< without glidepath (GGMonl,' H6 4C'


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071 A runwa, covered with ! mm thic water' is said to be: contaminated. wet. flooded. damp.

071 The minimum number of hand fire)extinguishers to be located in the passengercompartment of an aircraft with a maximum approved passenger seatingconfiguration of 31 is:

" 1 3 0

071 The number of crash axes or crowbars on board an aeroplane' whosemaximum approved configuration of passenger seats is "01' is:

" 1 3 !

071 The wae turbulence caused b, an aircraft is mainl, the result of: 1. Anaerod,namic effect (wing tip vortices. ". The engines action (propellers

rotation or engine gas exhausts. 3. The importance of the drag devices (si;e ofthe landing gear' of the flaps' etc.. The combination regrouping all the correct

statements is:

1. 3. " and 3. 1' " and 3.

071 An aircraft having undergone an anti)icing procedure must be anti)icing fluid

free at the latest when:

it is rotating (before taing)off. releasing the braes in order to tae)

off.

it is implementing its own anti)icing

devices.

leaving the icing ;one.

071 An aeroplane having undergone an anti)icing procedure and having exceededthe holdover time of the anti)icing fluid:

must undergo a de)icing procedurebefore a new application of anti)icingfluid for tae)off.

must onl, undergo a new anti)icingprocedure for tae)off.

need not undergo a new anti)icingprocedure for tae)off.

must onl, undergo a de)icingprocedure for tae)off.

071 The time of useful consciousness in case of an explosive decompression at analtitude of !0 000 ft is:

1" seconds. 30 seconds. 1 minute. * minutes.

071 /n case of landing on a flooded runwa, and in heav, rain: 1. ,ou increase ,ourapproach speed' ". ,ou land firml, in order to obtain a firm contact of thewheels with the runwa, and immediatel, land ,our nose gear' 3. ,ou decrease

,our approach speed' !. ,ou use s,stematicall, all the lift dumper devices' *.,ou land as smoothl, as possible' $. ,ou brae energicall,. The combinationregrouping all the correct statements is:

1' "' ! 3' * "' 3' ! 1' !' *' $

071 /n case of a serious threat based on the presence of a bomb on board a

pressuri;ed aircraft and disregarding an, fuel considerations:

,ou descend to the flight level

corresponding to the indicated cabinaltitude or the safet, altitude if higherand tae preventive steps b, putting

,ourself in a landing approachconfiguration.

,ou carr, out an emergenc, descent to

reach the safet, altitude.

,ou climb to the maximum flight level

which does not need the use ofpressuri;ation.

,ou go down to the level

corresponding to the indicated cabinaltitude and eep the aircraft in a cleanconfiguration until the final approach.

071 ist in the cabin' pressure and temperature drop characterise: a rapid depressuri;ation. a slow depressuri;ation. an electrical fire. a plastic fire.

071 /n a ditching situation' except for infants' the passengers shall be instructed toinflate their life acets:

whe n e xi ting the ai rc ra ft . imme diatel, on the ope ning of theexits.

immedia te l, on ditching. as soon as ditching is prepared.

071 /n case of a ditching' the cabin attendants should: 1. evacuate women andchildren first. ". have the passengers embar directl, in the life rafts. 3. prevent

passenger movements which ma, impede the aircraft-s flotation abilit,. !.ensure the complete evacuation of the aircraft. The combination regrouping allthe correct statements is:

"' 3' ! "' 3 1' "' 3' ! 1' !

071 The purpose of the first aid ox,gen is to: provide undiluted ox,gen topassengers for ph,siological reasons

following a cabin depressurisation.

provide the cabin attendants withrespirator, protection.

suppl, all the passengers in case ofdepressuri;ation.

provide the flight crew withrespirator, assistance after

depressuri;ation.071 4uring a de)icingIanti)icing procedure carried out in two stages' the holdover

time starts:at the beginning of the second stage(anti)icing stage.

at the beginning of the first stage (de)icing stage.

at the end of the second stage (anti)icingstage.

a the end of the first stage (de)icingstage.

071 A 1"11 halon fire)extinguisher can be used for: 1. a paper fire ". a fabric fire 3.an electric fire !. a wood fire *. a h,drocarbon fire The combinationregrouping all the correct statements is:

1' "' 3' !' * 1' 3' * "' 3' ! "' !' *

071 A %" fire extinguisher can be used for: 1. a paper fire ". a h,drocarbon fire 3.a fabric fire !. an electrical fire *. a wood fire The combination regrouping all

the correct statements is:

1' "' 3' !' * 1' 3' * "' 3' ! "' !' *

071?or a p re ssur ised a irc ra ft' the supp le me ntal ox,gen is : the ox,ge n suppl ie d to the ae roplaneoccupants in case of cabin

pressurisation failure.

the ox,gen supplied to a passenger whoneeds ox,gen for ph,siological

reasons.

the ox,gen used for protection againstsmoe and carbon dioxide.

a therapeutic ox,gen specificall,carried for certain passengers.

071 An aircraft whose maximum approved seating configuration is 10 seats mustbe e+uipped with:

one hand fire)extinguisher in thecocpitIflight dec and one hand fire)

one hand fire)extinguisher in thecocpitIflight dec and two hand fire)

three hand fire)extinguishers in thepassengers compartment.

two hand fire)extinguishers in thecocpitIflight dec and two hand fire)


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extinguisher in the passengers

compartment.

extinguishers in the passengers

compartment.

extinguishers in the passengers

compartment.

071 A water fire extinguisher can be used without restriction for: 1. a paper fire ". a

h,drocarbon fire 3. a fabric fire !. an electrical fire *. a wood fire Thecombination regrouping all the correct statements is:

1' 3' * 1' "' 3' !' * "' 3' ! "' !' *

071 An aeroplane whose maximum approved configuration is "00 passenger seats

must be e+uipped with:

3 hand fire extinguishers in the

compartment.

* hand fire extinguishers in the

passenger compartment.

7 hand fire extinguishers in the passenger

compartment.

! hand fire extinguishers in the

passenger compartment.

071 The information concerning dangerous goods that passengers ma, carr,' a relisted in the:

/%A document titled Technicalsafet, instructions for the airtransportation of dangerous products

a ir cr aft -s fl ight ma nual . /ATA doc ume nt 4ange rous p roduc tstransportation.

FA6)< documentation.

071 The protection time of an anti)icing fluid depends on: 1. the t,pe and intensit,of the showers ". the ambient temperature 3. the relative humidit, !. thedirection and speed of the wind *. the temperature of the airplane sin $. thet,pe of fluid' its concentration and te mperature The combination regrouping all

the correct statements is:

1' "' 3' !' *' $ 1' 3' *' $ "' 3' !' * 1' "' !' $

071 The anti)icing fluid protecting film can wear off and reduce considerabl, theholdover time:

during strong winds or as a result ofthe other aircraft engines et blast.

when the outside temperature is closeto 0 %.

when the temperature of the aeroplanesin is close to 0 %.

when the aeroplane is pared facinginto wind.

071 4ue to ris of t,res explosion' after landing' when the braes are at a ver, hightemperature' one should approach the landing gear:

either from aft or fore. sidewards. from an, direction. from the inboard side.

071 /n case of a fire due to the heating of the braes' ,ou fight the fire using: 1. a

dr, powder fire extinguisher ". a water spra, atomi;er 3. a water fire)extinguisher !. a %" fire)extinguisher to the maximum The combinationregrouping all the correct statements is:

1' " "' 3' ! 3' ! 1' !

071 /n case of an engine no;;le fire while on ground ,ou: carr, out a dr, craning. carr, out a damp craning. pull the fire shut off handle and triggerthe engines fire)extinguishers.

fight the no;;le fire with a water fire)extinguisher.

071 8hen taing)off behind a wide)bod, aircraft' with wind coming from the rightside' ,ou adopt a path' whenever possible:

distinct from the preceding airplane'b, remaining on the right of and aboveits path.

distinct from the preceding airplane' b,remaining on the left of and under its

path.

identical to the one of the precedingairplane.

different from the preceding airplane'b, remaining behind it and under itspath.

071 8hen taing)off behind a wide)bod, aircraft' with wind coming from the leftside' ,ou adopt a path' whenever possible:

distinct from the preceding airplane'b, remaining at the left of and aboveits path.

distinct from the preceding airplane' b,remaining at the right of and under its

path.

identical to the one of the precedingairplane.

distinct form the preceding airplane'b, remaining behind it and under itspath.

071 The time needed for the dissipation of a turbulent wae created b, a wide)bod,

aircraft during tae)off is about:

3 minutes. 30 seconds. 1 minute. 10 minutes.

071 To extinguish a fire in the cocpit' ,ou use: 1. a water fire)extinguisher ". apowder or chemical fire)extinguisher 3. a halon fire)extinguisher !. a %" fire)extinguisher The combination regrouping all the correct statements is:

3' ! 1' "' 3' ! 1' " "' 3' !

071 A passenger is allowed to carr, match)boxes: 1. on himselfIherself ". in hisIher

hand luggage 3. in hisIher checed luggage The combination regrouping all thecorrect statements is:

1 1' "' 3 1' " "' 3

071 /n icing conditions and after the application of an anti)icing fluid on ,our

aeroplane' ,ou should: 1. avoid positioning ,ourself in the engine et blast of

the preceding aircraft ". avoid positioning ,ourself in the turbo)props wash ofthe preceding aircraft 3. position ,ourself in the engine et blast of the

preceding aircraft !. position ,ourself in the turbo)props wash of the preceding

aircraft The combination regrouping all the correct statements is:

1' " 3' ! "' 3 1' !

071 8 ithout wind' the tip vortice s crea te d b, an airpla ne at tae)off: separate on each side of the runwa,. stagnate on the runwa ,. separate to the right side . separate to the left side .

071 2nder icing conditions' if ,ou exceeded the holdover time' the correctprocedure is:

de)ice again the aeroplane' then appl,anti)icing fluid.

appl, directl, anti)icing fluid withoutprevious de)icing.

operate the aeroplane de)icingIanti)icings,stems.

de)ice the aeroplane.

071 The wae turbulence: starts at rotation and stops as soon asthe aeroplane-s wheels touch theground.

starts as soon as the aeroplanecommences rolling and stops as soon asit has come to a stop at landing.

starts when the aeroplane reaches aheight of 3* ft above the ground andstops when it crosses this height before

landing.

starts when pulling out the dragdevices and stops when retracting thedrag devices.

071/n a microburst combined with a violent storm the winds at: low alti tude diverge from the centre ofthe phenomenon and the atmospheric

low altitude diverge from the centre ofthe phenomenon and the atmospheric

high altitude converge on the centre ofthe phenomenon and the atmospheric

low altitude converge on the centre ofthe phenomenon and the atmospheric


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pressure increases b, a few

hectopascals.

pressure decreases b, a few

hectopascals.

pressure increases b, a few hectopascals. pressure decreases b, a few

hectopascals.

071 Bou will use a %" fire)extinguisher for: 1. a paper fire ". a plastic fire 3. a

h,drocarbon fire !. an electrical fire The combination regrouping all thecorrect statements is:

1'"'3'! 3'! 1'"'3 "'3

071 Bou will use a powder fire)extinguisher for: 1. a paper fire ". a plastic fire 3. a

h,drocarbon fire !. an electrical fire The combination regrouping all thecorrect statements is:

1' "' 3' ! 1' "' 3 "' 3 1' !

071 /n case of an unexpected encounter with windshear' ,ou will: 1. set themaximum tae)off thrust ". increase the pitch)up attitude up to the limitactuating the stic shaer 3. pull in the drag devices (gear and flaps !. eep

the airplane-s current configuration *. tr, to reach the maximum lift)to)dragratio The combination regrouping all the correct statements is:

1' "' ! 1' 3' * "' 3 3' *

071 A fast decompression is recogni;able b, the following elements: 1. mist in the

cabin ". blast towards the exterior of the aircraft 3. expansion of bod, gases !.blast of air released violentl, from the lungs The combination regrouping allthe correct statements is:

1' "' 3' ! "' 3' ! 1' "' 3 1' !

071 A slow decompression ma, be caused b,: 1. a lea in a doorseal during normalpressurised flight ". loss of a cabin window 3. malfunction of all pressurised

s,stems !. loss of a door The combination regrouping all the correct statementsis:

1' 3 1' "' 3' ! "' ! 1' "' 3

071 The flight data recorder must start automaticall, to record the data: prior to the airplane being able to

move b, its own power.

when taing)off. when the landing gear is retracted. when lining up.

071 The flight data recorder must stop automaticall, to record the data: after the aeroplane is unable to moveb, its own power.

when the main gear shoc strutcompresses when touching the runwa,.

when the landing gear is extended andloced.

when the aeroplane clears the runwa,.

071 FA6)< 1 applies to: the operation b, a FAA state member

of an, civil c ommercial transportaeroplane.

aircraft proceeding from =uropean

states or fl,ing over them.

aircraft used b, police' customs and

defence departments.

the operation b, a FAA state member

of an, civil aircraft.

071 The dangerous goods regulations /%A annex 1# and FA6 < re+uire that'when delivering cargo for transport' the responsibilit, for compliance with theregulations are to:

sender. commander. station manager. aerodrome manager.

071 An operator must ensure that for the duration of each flight' be ept on theground' if re+uired:

mass and balance documentation. a cop, of the calculated tae)offperformances.

the calculation of the airborne fuel+uantit,.

meteorological information.

071 After an accident' the operator of an aircraft e+uipped with a flight recordermust eep the original recordings for a minimum period of:

$0 da,s. 30 da,s. &0 da,s. !* da,s.

071 The commander is re+uired b, the authorit, to present the aircraft documents.

Ee

shall do so' within a reasonable period

of time.

ca n re +ue st a dela, of !# hours . c an r efuse to pre se nt the m. sha ll do so i f a uthori se d b, the

operator.

071 An aeroplane whose maximum approved passenger seating configuration is 7to 30 seats must be e+uipped with at least:

1 hand fire)extinguisher convenientl,located in the passenger compartment.

" hand fire)extinguishers convenientl,located in the passenger compartment.

3 hand fire)extinguishers convenientl,located in the passenger compartment.

! hand fire)extinguishers convenientl,located in the passenger compartment.

071 An aeroplane whose maximum approved passenger seating configuration is 31

to $0 seats must be e+uipped with at least:

" hand fire)extinguishers convenientl,

located in the passenger compartment.

3 hand fire)extinguishers convenientl,


! hand fire)extinguishers convenientl,


* hand fire)extinguishers convenientl,


071 An aeroplane whose maximum approved passenger seating configuration is $1to "00 seats must be e+uipped with at least:


" hand fire)extinguishers convenientl,located in the passenger compartment.


* hand fire)extinguishers convenientl,located in the passenger compartment.

071 An aeroplane whose maximum approved passenger seating configuration is"01 to 300 seats must be e+uipped with at least:




$ hand fire)extinguishers convenientl,located in the passenger compartment.

071 An aeroplane whose maximum approved passenger seating configuration is

301 to !00 seats must be e+uipped with at least:



! hand fire)extinguishers convenientl,


$ hand fire)extinguishers convenientl,




071 An aeroplane whose maximum approved passenger seating configuration is!01 to *00 seats must be e+uipped with at least:




# hand fire)extinguishers convenientl,located in the passenger compartment.

071 An aeroplane whose maximum approved passenger seating configuration is

*01 to $00 seats must be e+uipped with at least:



# hand fire)extinguishers convenientl,


$ hand fire)extinguishers convenientl,




071 An aeroplane whose maximum approved passenger seating configuration isgreater than $00 seats must be e+uipped with at least:

# hand fire)extinguishers convenientl,located in the passenger compartment.

& hand fire)extinguishers convenientl,located in the passenger compartment.



071 An aeroplane whose maximum approved passenger seating configuration is 3 EAG 1"11 fire)extinguishers or " EAG 1"11 fire)extinguishers or ! EAG 1"11 fire)extinguishers or 1 EAG 1"11 fire)extinguisher or


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greater than $0 seats must be e+uipped (including flight dec with at least: e+uivalent. e+uivalent. e+uivalent. e+uivalent.

071 /n accordance with FA6)< 1' an airplane whose maximum tae)off massexceeds * 700 g or whose maximum approved passenger seating

configuration is greater than & seats and less than "00 seats must be e+uippedwith a:

crash axe or a crow)bar in the flightdec.

crash axe and a crow)bar in thepassenger compartment.

crash axe in the flight dec and a crow)bar in the passenger compartment.

crow)bar in the flight dec and a crashaxe in the passenger compartment.

071 /n accordance with FA6)


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071 The holdover time of an a nti)icing procedure will var, considerabl, depending

on the ambient temperature and the weather conditions. ?or a given ambienttemperature' the longest protection will be in weather conditions of:

frost free;ing fog rain on a cold soaed wing stead, snow

071 /f after anti)icing has been completed a pre)departure inspection revealspresence of frost' ice or snow' the correct action is to:

carr, out a further de)icingIanti)icingprocess

complete departure as soon as possibleto reduce the possibilit, of furtherfree;ing

switch on all the aeroplane anti)icing andde)icing s,stems and leave on until clearof icing conditions when airborne

complete departure provided that therecommended anti)icing holdover(protection time for the prevailing

conditions and t,pe of fluid used hasnot been exceeded

071 At a high ambient temperature (> 30 % and with a relative humidit, as low as

!0 K' in clear air' free of fog and precipitation' serious carburettor icing:

can occur' but onl, at a low power

setting

cannot occur can occur' but onl, at full power or cruise

settings

is possible at an, setting

071 8hich weather condition will give the shortest holdover time for a given

ambient temperature and t,pe of de)icing fluid J

Gight free;ing rain


18/24


071 ?or the purpose of wae turbulence separation' what is the /%A minimum

radar separation distance if a heav, aeroplane is following directl, behindanother heav, aeroplane on the approach to the same runwa, J

7.! m (! &.3 m (* 11.1 m ($ 3.7 m ("

071 ?or purpose of wae turbulence separation' what is the /%A minimum radarseparation distance and minimum time if a medium aeroplane (less than13$000 g and more than 7000 g is following directl, behind a heav,

aeroplane on the approach to the same runwa, J

&.3 m (* and " minutes 11.1 m ($ and 3 minutes 7.! m (! and " minutes &.3 m (* and 3 minutes

071 ?or purpose of wae turbulence separation' what is the /%A minimumseparation time if a light aeroplane (7000 g or less is following a medium

aeroplane (less than 13$000 g but more than 7000 g on the approach tolanding J

3 minutes ! minutes * minutes " minutes

071 /n accordance with /%A and A< 6A% procedures' which letter should beentered into a flight plan to denote an aeroplane which has a weight of lessthan 13$000 g but greater than 7000 g:

E G 10 to "0 Dt

071 8hen a G/5ET aircraft is landing behind a =4/2 aircraft' the waeturbulence non)radar minimum time approach separation' according with 4%!!!! (/%A' shall be:

3 / 1 / " / ! /

071 According with 4% !!!! (/%A' a wae turbulence non)radar separationminima of 3 minutes shall be applied:

to G/5ET aircraft taing)off behind a=4/2 aircraft from anintermediate part of a parallel runwa,separated b, less than 7$0 m

to a departing =4/2 aircraftfollowing a E=AHB aircraft arrivalwhen operating on a runwa, with adisplaced landing threshold

to an arriving G/5ET aircraft following a=4/2 aircraft departure whenoperating on a runwa, with a displacedlanding threshold' if the proected flight

paths are expected to cross

Cetween a G/5ET aircraft and a=4/2 aircraft maing a missedapproach and the G/5ET aircraftutili;ing an opposite)direction runwa,

for tae)off

071 According to 4% !!!! (/%A' a wae turbulence non)radar separationminima of " minutes shall be applied to:

=4/2 aircraft landing behind aE=AHB aircraft

=4/2 aircraft taing)off behind aE=AHB aircraft from an intermediate

part of a parallel runwa, separated b,less than 7$0 m

G/5ET aircraft taing)off behind a=4/2 aircraft from an intermediate

part of the same runwa,

G/5ET aircraft landing behind a=4/2 aircraft

071 /n accordance with 4% !!!! (/%A when a =4/2 and a G/5ETaircraft are using the same runwa,' or parallel runwa,s separated b, less than7$0 m' (in approach or departure phases of flight' shall be applied a wae

turbulence radar separation minima of:

* ! 3 "

071 According with 4% !!!! (/%A' a wae turbulence non)radar separationminima of 3 minutes shall be applied to:

G/5ET aircraft landing behind a=4/2 aircraft

G/5ET aircraft taing)off behind a=4/2 aircraft from a parallelrunwa, separated b, less than 7$0 m.(using whole runwa,

G/5ET aircraft taing )off behind a=4/2 aircraft when aircraft are usingthe same runwa,

=4/2 aircraft landing behind aE=AHB aircraft


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071 According with 4% !!!! (/%A' a wae turbulence radar separation

minima of &'3 m (*'0 shall be applied when a:

G/5ET aircraft is crossing behind a

=4/2 aircraft' at the same altitudeor less than 300 m (1 000 ft

G/5ET aircraft is crossing behind a

E=AHB aircraft' at the same altitude orless than 300 m (1 000 ft

E=AHB aircraft is crossing behind a

E=AHB aircraft' at the same altitude orless than 300 m (1 000 ft

=4/2 aircraft is crossing behind a

=4/2 aircraft' at the same altitudeor less than 300 m (1 000 ft

071 /n accordance with < 1 !30 (Aerodrome perating inima ) 5eneral' it isestablished' among other considerations' that an perator must tae fullaccount of Aeroplane %ategories. The criteria taen into consideration for

classification of Aeroplanes b, %ategories is the indicated airspeed atthreshold (Hat' which is e+ual to the stalling speed at the maximum landingmass (Hso multiplied b, 1'3. %orresponding Aeroplane %ategor, when Hat isfrom 1!1 t to 1$* t is:

4 C % =

071 /n the Airspace where the < is applicable' the vertical separation that can

be applied between ?G "&0 and ?G!10 inclusive is:

1 000 ft *00 ft "000ft 1 *00 ft

071 An aircraft fl,ing at flight level 370 (?G 370 in < Airspace is unable tocontinue flight in accordance with its air traffic control clearance (d' but is able

to maintain its assigned level (?G 370' and due to a total loss ofcommunications capabilit,' cannot obtain a revised clearance from AT%. Theaircraft should leave its assigned route or trac b, turning &0 (&0 degrees tothe right or left whenever this is possible' and turn to ac+uire and maintain in

either direction a trac laterall, separated b, 30 from its assigned routeand:

climb or descend *00 ft climb or descent 1 000 ft climb or descent 1 000 ft or descend *00ft

climb *00 ft or descend 1 000 ft

071 An aircraft fl,ing above ?G !10 in orth Atlantic (AT Airspace is unable to

continue flight in accordance with its air traffic control clearance' but is able tomaintain its assigned level' and due to a total loss of communicationscapabilit,' cannot obtain a revised clearance from AT%. The aircraft shouldleave its assigned route or trac b, turning &0 (&0 degrees to the right of left

whenever this is possible' and turn to ac+uire and maintain in either directiontrac laterall, separated b, 30 from its assigned route and:

climb or descend 1 000 ft climb or descent *00 ft climb 1 000 ft or descent *00 ft climb *00 ft or descend 1 000 ft

071 An aircraft operating within < Airspace is unable to continue flight inaccordance with its air traffic control clearance' but is able to maintain itsassigned level' and due to a total loss of communications capabilit,' cannot

obtain a revised clearance from AT%. The aircraft should leave its assignedroute or trac b, turning &0 (&0 degrees to the right or left whenever this is

possible' and turn to ac+uire and maintain in either direction a trac laterall,

separated b, 30 from its assigned route and climb 1 000 ft or descend *00ft' if:

at ?G!10 above ?G !10 below ?G !10 at ?G !30

071 An aircraft operating within < Airspace is unable to continue flight in

accordance with its air traffic control clearance' but is able to maintain itsassigned level' and due to a total loss of communications capabilit,' cannotobtain a revised clearance from AT%. The aircraft should leave its assignedroute or trac b, turning &0 (&0 degrees to the right or left whenever this is

possible' and turn to ac+uire and maintain in either direction a trac laterall,separated b, 30 from its assigned route and climb or descend *00 ft' if:

below ?G !10 at ?G !10 above ?G !10 at ?G !30

071 4% !!!! (/%A establishes' that wae turbulence separation minima shallbe based on a grouping of aircraft t,pes into three categories according to themaximum certificated tae)off mass. Eeav, (E %ategor,' are all aircraft t,pes

of:

13$ 000 Dg or more 13* 000 Dg or more less than 13$ 000 Dg but more than 1"$000 Dg

1!$ 000 Dg or more

071 The field of application of the inimum =+uipment Gist (=G is defined b,a phase of flight operation. The commander must use the limitations provided

b, the =G:

At the paring area prior to the aircrafttaxiing.

r ior to the ai rc ra ft t ae )off . At an, time dur ing the flight . 2nti l the a ir cra ft ha s c ome to acomplete stop at the end of the flight.

071 4uring a special H?6 flight' the minimum visibilit, re+uired b, FA6 < is: 1.*00 meters or more 3.000 meters ".*00 meters *.000 meters

071 The operator must ensure that the mass and balance documentation of a flightis stored for a minimum period of:

3 months 1 month $ months 1 ,ear

071 The operator must ensure that the information contained in the aircrafttechnical log is stored for a minimum period of:

"! months 3 months 1* months 1" months

071 A public address s,stem is re+uired to operate an airplane whose maximum 1& 30 & $1


22/24


approved passenger seating configuration is greater than:

071The number of spare fuses available for use in f light must be: 10 K of the number of fuses of eachrating with a minimum of 3

* K of the number fuses of each ratingwith a minimum of 1

10 K of the number of fuses of eachrating with a minimum of 1

"0 K of the number of fuses of eachrating with a minimum of "

071 A windshield wiper or an e+uivalent device at each pilot position is re+uired tooperate an aircraft:

maximum certificated tae)off mass isgreater than *'700 g

maximum certificated tae)off mass isgreater than 1*'000 g

maximum approved passenger seatingconfiguration is greater than &

maximum approved passenger seatingconfiguration is greater than 30 afterFanuar, 1st' "000

071 A runwa, is considered to be contaminated when its surface is covered for

more than:

"* K with compacted snow 10 K with ice "* K with melted snow with a +uantit,

e+uivalent to more than * mm of water

*0 K with melted snow with a +uantit,

e+uivalent to more than 1 mm of water

071 A runwa, is considered to be contaminated when its surface is covered formore than:

"* K with loose snow with a +uantit,e+uivalent to more than 3 mm of water

*0 K with loose snow with a +uantit,e+uivalent to more than " mm of water

10 K with compacted snow 1* K with ice

071 The public address s,stem must be audible and intelligible at: 1 ) all passengerseats " ) toilets 3 ) cabin crew seats ! ) wor stations The combination


1)")3)! 1)" 1 1)")3

071 /n order to operate an airplane at night' the airplane must be e+uipped with anairborne weather radar when the airplane is: 1 ) pressurised " ) non)

pressurised' and maximum tae)off mass is more than *'700 g 3 ) non)pressurised' and maximum approved seating configuration is more than & seats! ) non)pressurised' operating for public transportation The combinationregrouping all the correct statements is:

1)")3 1)! 1)" !

071 /f the engine fails in the hover' at 3- sid height in still air' in a single engine

helicopter' the recommended action is:

counteract ,aw with pedals' maintain

position with c,clic' cushiontouchdown with collective

use rudder to prevent ,aw' hold c,clic

stead,' lower collective briefl, thenraise to cushion landing

counteract ,aw with pedals' use c,clic to

raise tail rotor' lower collective slightl,to maintain rotor 6

use rudder to prevent ,aw' push c,clic

forward for touchdown' use collectiveto cushion landing

071 unintentional over)pitching is liel, to occur: at low airspeed in a transition to or

from the hover

as a result of excessive c,clic

movement

after attaining effective translational lift when commencing a flare

071 /n the event of an engine failure in a single engine helicopter in the cruise' therecommended se+uence of immediate actions is:

lower collective' counteract ,aw withpedals' select attitude with c,clic'

select landing site' transmit ma,da,'position helicopter for an into wind

landing

correct ,aw with pedals' lowercollective' transmit ma,da,' select

landing site' use c,clic and collective toposition for landing

flare with c,clic' counteract ,aw withpedals' establish descent with collective'

select landing site' adust collective forrange' land into wind' transmit ma,da,

lower collective' adust ,aw pedals'select airspeed' transmit ma,da,'

autorotate to open ground' adust speedfor landing

071 / f the rotor is overpitche d' the correc tive action is to: reduce collective pitch and leaveengine power constant

reduce both engine power andcollective pitch

increase engine power and collectivepitch

reduce engine power and leavecollective pitch constant

071 /f ground resonance is encountered in a helicopter' the correct recover, action

is::

To tae)off if rotor 6 sufficient' to

shut down and appl, rotor brae ifrotor 6 insufficient

To shut down immediatel,' regardless

of rotor 6

To appl, pitch for tae)off immediatel,'

regardless of rotor 6

To increase rotor 6 to tae)off

power and get airborne

071 To minimise the dangers of blade sailing: the start)up and shut)down should becarried out with the helicopter facing

slightl, out of wind

the start)up and shut)down should becarried out facing directl, into wind

flapping restrictors' if fitted' should bewithdrawn before start)up or shut)down

ensure that rotor 6 during start)upor shut)down are increased or

decreased as slowl, as possible

071


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exceeding 13 000 ft

071 ?or a non pressurised aircraft' all re+uired cabin crew members shall besupplied with supplemental ox,gen during:

the entire flight time at pressurealtitudes above 13 000 ft and for an,

period exceeding 30 minutes atpressure altitudes above 10 000 ft butnot exceeding 13 000 ft

the entire flight time at pressurealtitudes above 10 000 ft

the entire flight time at pressure altitudesabove 13 000 ft

the entire flight time after 30 minutesat pressure altitudes greater than 10

000 ft but not exceeding 13 000 ft

071 ?or a non pressurised aircraft' 100K of passengers shall be supplied withsupplemental ox,gen during:



the entire flight time after 30 minutes atpressure altitudes greater than 10 000 ftbut not exceeding 13 000 ft

the entire flight time at pressurealtitudes above 13 000 ft and for an,

period exceeding 30 minutes at

pressure altitudes above 10 000 ft butnot exceeding 13 000 ft

071 ?or a pressurised aeroplane' all re+uired cabin crew members shall be suppliedwith supplemental ox,gen during: 1 O the entire flight time when cabin

pressure altitude exceeds 13 000 ft but not less than 30 minutes " O the entire

flight time at pressure altitudes above 13 000 ft and for an, period exceeding30 minutes at pressure altitudes above 10 000 ft but not exceeding 13 000 ft 3

O the flight time minus 30 minutes when cabin pressure altitude is greater than10 000 ft but not exceeding 13 000 ft ! O the flight time when cabin pressure

altitude is greater than 10 000 ft but not exceeding 13 000 ft after the first 30minutes at these altitudes The combination regrouping all c orrect statements is:

1' 3 "' 3 1' ! "' !

071 ?or a pressurised aeroplane' certificated to fl, above "* 000 ft' all occupants of

flight dec seats on flight dec dut, shall be supplied with supplementalox,gen during a period in an, case no less than:

" hours 30 minutes 1 hour 10 minutes

071 A helicopter commander shall ensure that the amount of usable fuel remainingin flight is not less than the fuel re+uired to proceed to a heliport where a safelanding can be made with:

f ina l re serve fue l r ema ining 1* minutes of re ma ining fue l fue l to hold 30 minutes at 1*00 ft abovethe heliport

fuel to fl, "0 minutes at best rangespeed

071 /f no meteorological information is available for the destination' thecommander of a helicopter must: select two destination alternatives tae extra fuel to fl, two hours atholding speed tae extra fuel to fl, one hour at holdingspeed' 1*00 ft above the alternateheliport

not tae)off until gettingmeteorological forecast

071 The amount of fuel to be carried b, a helicopter for /?6 flight' when noalternate is re+uired' should include a final reserve fuel of +uantit, to fl, :

30 minutes at holding speed at 1*00 ftabove the destination' in standard

conditions

"0 minutes at holding speed at 1*00 ftabove the destination' in standard

conditions

30 minutes at best range speed "0 minutes a t best range speed

071 The amount of fuel to be carried b, a helicopter on a H?6 flight navigating b,da, with reference to visual landmars should include a final reserve fuel of

+uantit, to fl, :

"0 minutes at best range speed 30 minutes at best range speed "0 minutes at holding speed at 1*00 ftabove the destination heliport

30 minutes at holding speed at 1*00 ftabove the destination heliport

071 The amount of fuel to be carried b, a helicopter on a H?6 flight in a non)hostile environment should include contingenc, fuel of:

*K of the planned t rip fuel 10K of the pla nne d t rip fue l +ua nt it, to fl, "0 minutes at be st ra ngespeed

+uantit, to fl, 30 minutes at best rangespeed

071 The pre)flight fuel calculation' for a helicopter on an /?6 flight should include

contingenc, fuel +uantit,:

of 10K of the planned tr ip fuel of *K of the planned trip fuel to f l, "0 minutes a t best range speed to f l, 30 minutes a t best range speed

071 A helicopter with a aximum tae)off mass exceeding * 700 g conducting

Eelicopter =mergenc, edical


24/24


e+uipment configuration compl,ing with FA6 < is:

071 /n accordance with FA6 < 3' a helicopter must be e+uipped with amegaphone when operated with an approved seating capacit, of more than:

1& 13 & 10

071 /n accordance with FA6 < 3 ' an operator shall ensure that a pilot does notoperate a helicopter unless he has carried out ( except when fl,ing under thesupervision of a nominated commander ' at least:

3 tae)offs' 3 circuits and 3 landingsas pilot fl,ing in a helicopter (or aflight simulator of the same t,pe to be

used' in the preceding &0 da,s

$ tae)offs' $ circuits and $ landings ina helicopter (or a flight simulator ofthe same t,pe to be used' in the

previous 3 calendar months

3 tae)offs' 3 circuits and 3 landings aspilot fl,ing in a helicopter (or a flightsimulator of the same t,pe to be used' in

the previous 3 calendar months

$ tae)offs' $ circuits and $ landings ascommander in a helicopter ( or a flightsimulator of the same t,pe to be used'

in the preceding &0 da,s

071 FA6 < 3 applies to an, operator' whose principal place of business is in aFAA state member' for the operation of:

an, civil helicopter for commercial airtransportation

helicopters proceeding from =uropeanstates or fl,ing over them

an, aircraft proceeding from =uropeanstates or fl,ing over them

an, civil aircraft for commercial airtransportation

071 According to /%A 4oc #1$#' a noise abatement departure procedure is T

to be initiated at less than:

#00 ft above aerodrome elevation 1 000 ft above aerodrome elevation 1 *00 ft above aerodrome elevation " 000 ft above aerodrome elevation

071 According to the recommended noise abatement tae)off and climb

procedure A4"' established in /%A 4oc #1$#' acceleration andflapsIslats retraction is initiated:

not below #00 ft not below 1 000 ft at 3 000 ft at 1 *00 ft

071 To operate a helicopter which maximum approved passenger configuration is

more than &' along a route where thunderstorms are expected' an airborneweather radar e+uipment is re+uired : 1 ) for a pressurised helicopter " ) atnight 3 ) for /?6 flights ! ) if T is more than 317* g The combinationregrouping all the correct statements is:

"' 3 1' "' 3' ! 3' ! 1' 3' !

071 ?or performance class " operations onshore' the commander must operate to

tae)off minima with an 6H6IH/< not lower than:

#00 m 1*00 m $00 m *00 m

071 =xcept if a different value is approved b, the authorit,' the contingenc, fuelfor an /?6 helicopter flight should be:

10K of the planne d t rip fue l *K of the planne d t rip fue l a n a mount of fuel suff ic ie nt for 1*minutes fl,ing at long range speed

an amount of fuel sufficient for 30minutes fl,ing at long range speed

071 =xcept if a different value is approved b, the authorit,' the contingenc, fuel

for a H?6 helicopter flight in a non hostile environment should be:

*K of the planned t rip fuel 10K of the p la nne d t rip fue l a n a mount of fuel suff ic ie nt for 1*

minutes fl,ing at long range speed

an amount of fuel sufficient for 1*

minutes fl,ing at holding speed

071 As a result of an in)flight fuel chec' the expected fuel remaining on arrival isless than the re+uired alternate fuel plus final reserve fuel. The commanderma, permit alternate fuel to be used before landing at the destination' provided

that' at on shore destination:

separate touchdown and lift)off areasare available and weather c onditionsare above the planning minima

latest forecast indicates that' at theexpected time of arrival' the weatherconditions are above the planning

minima

the appropriate weather reports orforecasts indicates that' during a periodcommencing 1 hour before and ending 1

hour after the estimated time of arrival'the weather conditions are above the

planning minima

two independent runwa,s are availableand expected weather conditions aresuch that ceiling is *00 ft above 4A

and above 1*00 ft above airportelevation

Documents

071 - Operational Procedures