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110 Business & Commercial Aviation n May 2006 www.AviationNow.com/BCA
By Fred George
General aviation aircraft manufac-turers set a billings record in 2005,topping $15 billion for the first time
and soaring more than 27 percent comparedto 2004, according to GAMA. Unitdeliveries jumped more than 20 percent in2005 vs. the previous year, reaching 3,580aircraft. In a prime sign of the industry’shealth and strength, 2005 piston-engineaircraft shipments were up by one-fifth over2004. Cessna single-engine airplane salessurged in large part because of marketenthusiasm for aircraft equipped withGarmin G1000 glass cockpit avionics.Cirrus and Columbia (nee Lancair) salesjumped, as well, with Piper, Raytheon andMooney also showing impressive gains.Virtually all of the hot sellers are equippedwith large-format LCD glass cockpits. It’stough to find new general aviation aircraftfrom major manufacturers that still havesteam gauges.
Mooney, not content to rest on last year’ssuccess, introduced the M20TN Acclaim atSun ‘n Fun this year. The Acclaim willreplace the 16-year-old TLS Bravo in theproduct lineup. Fitted with a 280-hp, twinturbo-normalized Continental TSIO-550-G, the Acclaim should be able to cruise at230 KTAS at FL 250 and reclaim the title offastest production single-engine aircraft,according to the Kerrville, Texas, firm. TheExtra 400, one of the Acclaim’s prime
competitors, has dropped out of this year’sHandbook as the German firm focuses ondeveloping the Extra 500 turboprop.
Moving up into cabin-class twins, manyfolks are still waiting for Adam to completepost-certification work and clean up IOUsfor the turbocharged, pressurized push/pullAdam 500. Nearly a year after basic certifi-cation, buyers still are waiting for full oper-ational approval, including pressurization,full IFR authorization and flight into knownicing. However, FAA certification authoritiessay that Adam is making headway on manyfronts, so 2006 could be the year that full-scale production deliveries begin.
In the single-engine turboprop sector,EADS Socata is making news with its TBM850, a TBM 700 with an 850-shp Pratt &Whitney Canada engine that boosts itsmaximum cruise speed by more than 20knots. The TBM 850 is limited to 700 hp forlanding and takeoff, but once the gear andflaps are retracted, operators can push up thepower lever to take advantage of the addi-tional 150 hp. Pilatus also has a new offering,the PC-12/47, signifying its 4,740 kilogramor 10,450 pound MTOW. The boost inweight enables typically equipped aircraft tocarry six passengers with full fuel. Butaircraft registered in EASA countries arerestricted to a 9,920-pound MTOW, so thatcosts operators three passengers with fulltanks.
Ibis has elected to pull its Ae270 from theHandbook’s listing pending the developmentof a new wing for the aircraft. This will
enable the aircraft to carry more fuel andra i se i t s MTOW, making i t morecompetitive with the PC-12. The modifiedAe270 should reappear in the 2007Handbook. We’re still listing the Extra 500in the single-engine turboprop section;however, the bargain leader in pressurizedsingle-engine turboprops has yet to earnEASA or FAA type certification.
Evolutionary progress continues in thetwin-turboprop class. Raytheon’s King AirC90GT, powered by twin PT6A-135engines, is making its debut in this year’sHandbook. It replaces the C90B. Taking alesson from Waco, Texas-based BlackhawkModifications, Raytheon fitted twin PT6A-135 engines to the C90 and boosted itsmaximum cruise speed by more than 40KTAS. The engines weigh virtually thesame as the -21 turboprops they replace, sothere’s very little downside to the upgrade,o ther than s l ight ly increased fue lconsumption in cruise. But the C90GTclimbs so much faster than the C90B its fueleconomy actually is better on typical 300-and 600-nm trips. And it’s capable ofslashing a half hour off 1,000-nm trips inexchange for an extra 5 percent fuel burn.
Piaggio’s Avanti II should be certifiedby the end of this year or the beginningof 2007. The lates t i terat ion has aRockwell Collins Pro Line 21 glasscockpit that both increases capabilitiesand reduces empty weight. The additionof -66B engines will boost high-altitudecruise speed, but precise data won’t be
Revenues and deliveries soared last year; more new models introduced.
Business Airplanes
B&
CA
available until all flight tests are complete.Glance please at the VLJ section.
Production deliveries of both the Eclipse 500and Cessna Citation Mustang will begin laterthis year. The Adam 700 becomes the thirdVLJ to appear in the Handbook. FAA insiderssay that Adam is making great strides towardrestoring its credibility with the folks in theaircraft certification office, so Adam 700development is getting back on track. Lookfor initial FAA type certification in the late2007 to early 2008 time frame.
The VLJ section of the Handbook willcontinue to grow in coming years asEmbraer along with upstarts such as CirrusDesign and Diamond Aircraft debut theirown VLJs.
Conventional business jets continue tooccupy the largest section of the Handbook.In 2004, deliveries increased by more thanone-quarter. Manufacturers are investingheavily in product development becauseprofit margins are strong, but competition isfierce. Raytheon, for instance, is developingthe Premier IA, an updated version of theoriginal design with improved brakes,better systems and upgraded avionics. Itwas designed to compete head-on withCessna’s CJ2, but Cessna then upped theante with the CJ2+. It’s fitted with highlyflat-rated 2,490-pound-thrust WilliamsFJ44-3-24 turbofans that improveperformance, and it’s also equipped withmuch more capable Pro Line 21 avionics, asreported in B&CA’s April 2006 issue (page34). The Premier IA retains a significantspeed advantage over the CJ2+, but theCessna has considerably better runwayperformance. The CJ2+’s spectacular climbperformance enables it to arrive within oneto six minutes of the Premier IA on typicalB&CA fixed distance missions.
Sino Swearingen now has earned basictype certification for the SJ30-2, but it’s stillworking on post-certification IOUs priorto full-scale production deliveries. Flightinto known icing approval is complete, so
the remaining items should not pose majorobstacles to deliveries.
Cessna’s Encore+ is new to this year’sHandbook. The newest iteration of theCitation V is fitted with a fully integratedCollins Pro Line 21 avionics package thatboth offers more capabilities and reducesBOW by 100 pounds.
This year’s Handbook welcomes aboardthe Grob G180 SPn Utilijet that made asurprise debut at the 2005 Paris Air Show.The G180 is designed to compete head-onwith turboprops that operate from unim-proved runways. It offers impressive short-and soft-field takeoff performance withrange and speed competitive with the CJ3.It can carry seven people with full fuel andit has the largest cabin in the light jet classby a wide margin.
Bombardier continues to refine itsLearjet 45 series aircraft. The basic modelshave been dropped in favor of the 40XRand 45XR, both of which are fitted withHoneywell TFE731-20BR engines, whichhave robust hot-and-high performance.However, the engines still are limited to3,500 pounds of thrust for takeoff, so sea-level runway performance is far from class
leading. But when departing hot-and-highairports, these aircraft are considerablymore sprightly than any direct competitors.Bombardier’s Learjet 60XR, fitted with ProLine 21 avionics, is appearing for the firsttime in this year’s Handbook. The cockpitimprovements add new capabilities, but theLearjet 60 needs airframe improvements ifit is to remain competitive in the future.
Gulfstream’s G150, in contrast, hasbecome considerably more competitive asfinal flight test data have been analyzed. Itsrunway per formance now i s verycompetitive with most other midsize jetsand it can carry four passengers 2,950 miles.That provides coast-to-coast range undermost probable wind conditions and one-stop range on transatlantic routes. It’s pricedbetween the Learjet 60XR and Raytheon’snew Hawker 850XP, which now sportswinglets. The aero improvements boost theHawker 850XP’s range by 100 nm, but its t i l l can ’t match the G150 ’s rangeperformance.
The Hawker 850XP remains Raytheon’stop offering as Hawker 4000 type certifi-cation and production deliveries remainstalled pending systems development andcompletion of final function and reliabilitytesting. Although the Hawker 4000 has hada provis ional type cert i f icate s inceDecember 2004, Raytheon officials arereluctant to predict when full FAA typecertification will be earned.
The Falcon 50EX is making its finalappearance in the Purchase PlanningHandbook. Dassault is concentrating ondeveloping its widebody aircraft, such as theFalcon 2000DX, which is making its firstappearance in this year’s Handbook. Similarto the Falcon 900DX, the 2000DX is aversion of an existing aircraft that has alower price tag and less fuel capacity. The2000DX, which replaces the Falcon 2000,offers better runway performance, morerange and better climb performance, plus
Business & Commercial Aviation n May 2006 111www.AviationNow.com/BCA
BCA • ISSUE: May 2006PAGE: 111 / Version: #1
Adam 700
Embraer Legacy
Embr
aer
Ada
m A
ircr
aft
112 Business & Commercial Aviation n May 2006
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BCA • ISSUE: May 2006PAGE: 112 / Version: #1
it’s fitted with the Primus Epic EASycockpit.
Bombardier’s Challenger 605, announcedat the 2005 NBAA Convention, joins theHandbook this year, replacing the Challenger604. While its performance is virtuallyidentical to the older model, the Challenger605 offers plenty of improvements forpassengers, including larger windows, aslightly wider cabin and better furnishings.It’s also 200 pounds lighter, so typicallyequipped aircraft will be able to carry fiveto six passengers with full fuel.
Airbus’ A318 Elite becomes a new heavy-weight in the business aircraft tables. Withup to 4,000-nm range with an optionalauxiliary center tank, the A318 is intendedto compete against veteran, purpose-builtheavy iron jets from Bombardier, Dassaultand Gulfstream. With 23,300 pounds ofthrust on each side, the A318 Elite will offerexcellent runway performance, comparingmost favorably with purpose-built businessjets. Lufthansa Technik is handlingcompletions, so buyers can be confidentthey’ll be built precisely and finished on
time. So where are the performancenumbers? Airbus has undertaken athorough aerodynamic clean-up of itssingle-aisle aircraft and the first beneficiaryis the A318 Elite. With modified winglets,fuselage-to-wing fairings and inlet ductchanges, the A318 Elite will be noticeablymore fuel efficient than legacy A318 aircraft.
The 71-ton A318, though, is no match forthe largest aircraft in this year’s Handbook,the BBJ3. Based on the next-generationBoeing 737-900ER airliner, the 94-ton BBJ3will sport Aviation Partners-Boeing winglets
and have a range of more than 4,700 nmwith typical 19- to 24-passenger loads.Offering 28 feet more cabin length than theoriginal BBJ, it’s designed for folks whoneed one-third more cabin volume than theoriginal aircraft and 11 percent more thanthat offered by the BBJ2.
For now, the surge in business aircraftsales seems secure. Market predictions fromHoneywell, Rolls-Royce and other firmsindicate strong growth through the decade.But storm clouds in the form of ever-tightening fuel supplies imperil futureunrestricted growth. As we mentioned inthe 2005 Handbook, “. . . fuel price increasesthreaten to create an economic microburstin the path of general aviation . . .” Folksflying these aircraft may be able to pay$5.00 or more per gallon for fuel, but theircustomers on the ground already arefeeling the pinch at the pump at $3.00 pergallon. Consumer confidence ultimatelywill determine if the current growth trendin business aircraft will continue or if it will once again suffer through turbulenttimes. B&CA
Manufacturer, ModelIn some cases, the airplane manufac-turer’s name is abbreviated, but thecompany’s full name and address canbe found in the “Air frame SuppliersDirector y” on page 168. The modelname also is included in this group.
B&CA Equipped PricePrice estimates are first quarter, cur-rent year dollars for the next availabledelivery. Some aircraft have long leadtimes, thus the actual price will behigher than our published price. Notewell, manufacturers may adjust priceswithout notification.
Piston-powered airplanes — Computed
retail price with at least the level ofequipment specified in the B&CARequired Equipment List on page 117.
Turbine-powered airplanes — Averageprice of 10 of the last 12 commercialdeliveries, if available. The aircraft seri-al numbers aren’t necessarily consecu-tive because of variations in completiontime and because some aircraft may beconfigured for non-commercial, specialmissions.
CharacteristicsSeating Capacity — Crew + TypicalExecutive Seating/Maximum Seating.
For example, 2+8/19 indicates thatthe aircraft requires two pilots, there
are eight seats in the typical execu-tive configuration and the aircraft iscer tificated for up to 19 passengerseats.
A four-place single-engine aircraft isshown as 1+3/3, indicating that onepilot is required and there are threeother seats available for passengers.We require two pilots for all turbofanairplanes, except the CJ1+, CJ2+,Mustang, Premier I, SJ30-2 and Eclipse500 which have, or will have, a largepercentage of single-pilot operators.
Four crewmembers are specified forultra-long-range aircraft — three pilotsand one flight attendant.
Each occupant of a turbine-poweredairplane is assumed to weigh 200pounds, thus allowing for stowed lug-gage and carryon items. In the case ofpiston-engine airplanes, we assumeeach occupant weighs 170 pounds.There is no luggage allowance for pis-ton-engine airplanes.
Wing Loading — MTOW divided by totalwing area.
Power Loading — MTOW divided bytotal rated horsepower or total ratedthrust.
FAR Part 36 Certificated Noise Levels — Fly-over noise in A-weighted decibels (dBA)for small and turboprop aircraft. For tur-bofan-powered aircraft, we provideEPNdB (effective perceived noise levels)for takeoff, sideline and approach.
How to Use the Airplane Charts
Lavatory
Aft Baggage Compartment
Passenger CabinGalley
Cabin Length
Cockpit
Cabin Length
Baggage
Lavatory
Aft Baggage Compartment
Passenger CabinGalley
Cabin Length
Cockpit
Cabin Length
Baggage
Cabin Length
Cessna MustangC
essn
a A
ircr
aft
DimensionsExternal Length, Height and Span dimen-sions are provided for use in determin-ing hangar and/or tiedown spacerequirements.
Internal Length, Height and Width arebased on a completed interior, includ-ing insulation, upholstery, carpet, car-pet padding and fixtures.
As shown in the Cabin Length illustra-tion, for airplanes other than “cabin-class” models, the length is measuredfrom the forward bulkhead ahead of therudder pedals to the back of the rear-most passenger seat in its normal,upright position.
For “cabin-class” aircraft, we showthe overall length of the passengercabin, measured from the aft side ofthe forward cabin divider to the aft-most bulkhead of the cabin. The aft-most point is defined by the rear side ofa baggage compartment that is acces-sible to passengers in flight or by theaft pressure bulkhead.
The overall length is reduced by thelength of any permanent mounted sys-tem or structure that is installed in thefuselage ahead of the aft bulkhead. Forexample, some aircraft have full fuse-lage cross-section fuel tanks mountedahead of the aft pressure bulkhead.
The second length number is the netlength of the cabin that may be occu-pied by passengers. It’s measuredfrom the aft side of the forward cabindivider to an aft point defined by therear of the cabin floor capable of sup-porting passenger seats, the rear wallof an aft galley or lavatory, an auxil-iar y pressure bulkhead or the frontwall of the pressurized baggage com-par tment. Some aircraft have thesame net and overall interior lengthbecause the manufacturer of fers atleast one interior configuration withthe aft-most passenger seat locatednext to the front wall of the aft lug-gage compartment.
Interior height is measured at the cen-ter of the cross section. It may be basedon an aisle that is dropped several inchesbelow the main cabin floor that supportsthe passenger seats. Some aircraft havedropped aisles of varying depths, result-ing in less available interior height in cer-tain sections of the cabin.
Two width dimensions are shown formultiengine turbine airplanes — one atthe widest par t of the cabin and theother at floor level. The dimensions,however, are not completely indicativeof the usable space in a specific air-craft because of individual variances ininterior furnishings.
PowerNumber of engines, if greater thanone, and the abbreviated name of themanufacturer:
CFE — ASE/GE joint ventureRR — Rolls-RoyceCFMI — CFM InternationalCont — Teledyne ContinentalHon — HoneywellIAE — International Aero EnginesLyc — Textron LycomingP&WC — Pratt & Whitney CanadaWms/RR — Williams/Rolls-Royce
Output — Takeoff rated horsepowerfor propeller-driven aircraft or poundsthrust for turbofan aircraft. If an engineis flat rated, enabling it to producetakeoff rated output at a higher thanISA (standard day) ambient tempera-ture, the flat rating limit is shown asISA+XX°C. Highly flat-rated engines,i.e., engines that can produce takeoffrated thrust at a much higher thanstandard ambient temperature, typical-ly provide substantially improved high-density altitude and high-altitude cruiseperformance.
Inspection Interval is the longest,scheduled hourly major maintenanceinterval for the engine, either “t” forTBO or “c” for compressor zone inspec-tion. OC is shown only for engines thathave “on condition” repair or replaceparts maintenance.
Weights (lb)Weight categories are listed as appro-priate to each class of aircraft.
Max Ramp — Maximum ramp weightfor taxi.
Max Takeoff — Max takeoff weight asdetermined by structural limits.
Max Landing — Max landing weight asdetermined by structural limits.
Zero Fuel — Maximum zero fuel
weight, shown by “c” indicating thecer tificated MZFW or “b,” a B&CA-computed weight based on MTOWminus the weight of fuel required to fly1.5 hours at high-speed cruise.
Max ramp, max takeof f and maxlanding weights may be the same forlight aircraft that may only have a cer-tificated max takeoff weight.
EOW/BOW — Empty operating weightis shown for piston-powered airplanes.Basic operating weight, which essen-tially is EOW plus required flightcrew, isshown for turbine-powered airplanes.EOW is based on the factory standardweight, plus items specified in theB&CA Required Equipment List, lessfuel and oil. BOW, in contrast, is basedon the average EOW weight of the last10 commercial deliveries, plus 200pounds for each required crewmember.We require four crewmembers — threeflight crew and one cabin attendant —for ultra-long-range aircraft.
There is no requirement to add in theweight of cabin stores, but some manu-facturers choose to include galleystores and passenger supplies as partof the BOW buildup. Life vests, life raftsand appropriate deep-water survivalequipment are included in the weightbuildup of the 80,000-pound-plus, ultra-long-range aircraft.
Max Payload — Zero fuel weight minusEOW or BOW, as appropriate. For pis-ton-engine airplanes, max payload fre-quently is a computed value because itis based on the B&CA (“b”) computedmaximum ZFW.
Executive Payload — Based on 170pounds per occupant for multienginepiston-engine airplanes and 200pounds per occupant for turbine-engine airplanes, as shown in the exec-utive seating section of the “Char-acteristics” section. Pilots and passen-
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BCA • ISSUE: May 2006PAGE: 113 / Version: #1
Gulfstream 450
Gul
fstr
eam
Aer
ospa
ce
gers, however, are counted as oc-cupants in piston-engine airplanes. Onlypassengers are counted as occupants inturbine-powered airplanes because therequired crew is included in the BOW. Ifthe executive payload exceeds the max-imum payload, we use maximum pay-load. Executive payload is not comput-ed for single-engine piston airplanes.
Max Fuel — Usable fuel weight basedon 6.0 pounds per U.S. gallon for avgasor 6.7 pounds per U.S. gallon for jetfuel. Fuel capacity includes optional,auxiliary and long-range tanks, unlessotherwise noted.
Available Payload With Max Fuel — Maxramp weight minus the tanks-fullweight, not to exceed zero fuel weightminus EOW or BOW.
Available Fuel With Max Payload — Maxramp weight minus zero fuel weight,not to exceed maximum fuel capacity.
Available Fuel With Executive Payload —Available fuel weight based on maxramp weight minus BOW plus exec-utive payload, up to the actual fuelcapacity.
LimitsB&CA lists V speeds and other limits asappropriate to the class of airplane.These are the abbreviations used onthe charts:
VNE — Never exceed speed (red linefor piston-engine airplanes).
VNO — Normal operating speed (top ofgreen arc for piston-engine airplanes).
VMO — Maximum operating speed(red line for turbine-powered airplanes).
MMO — Maximum operating Mach
number (red line for turbofan-pow-ered airplanes and a few turbopropairplanes).
FL/VMO — Transition altitude at whichVMO equals MMO (large turboprop andturbofan aircraft).
VA — Maneuvering speed (except forcertain large turboprop and all turbofanaircraft).
VDEC — Accelerate/stop decisionspeed (multiengine piston and lightmultiengine turboprop airplanes).
VMCA — Minimum control airspeed,airborne (multiengine piston and lightmultiengine turboprop airplanes).
VSO — Maximum stalling speed, land-ing configuration (single-engine air-planes) in KCAS.
VX — Best angle-of-climb speed (sin-gle-engine airplanes).
VXSE — Best angle-of-climb speed,one-engine inoperative (multiengine pis-ton and multiengine turboprop airplanesunder 12,500 pounds).
VY — Best rate-of-climb speed (single-engine airplanes).
VYSE — Best rate-of-climb speed, one-engine inoperative (multiengine pistonand multiengine turboprop airplanesunder 12,500 pounds).
V2 — Takeoff safety speed (large tur-boprops and turbofan airplanes).
VREF — Reference landing approachspeed (large turboprops and turbofanairplanes, four passengers, NBAA IFRreserves; eight passengers for ultra-long-range aircraft).
PSI — Cabin pressure differential (allpressurized airplanes).
Airport PerformanceApproved Flight Manual takeoff runwayper formance is shown for sea-level,standard day and for 5,000 feet eleva-tion/25°C day, density altitude. All-engine takeoff distance (TO) is shown forsingle-engine and multiengine piston,and turboprop airplanes with an MTOWof less than 12,500 pounds.
Accelerate/Stop distance (A/S) is shownfor small multiengine piston and smallturboprop airplanes. Takeoff field length(TOFL), the greater of the one-engineinoperative (OEI) takeoff distance orthe accelerate/stop distance, is shownfor FAR Part 23 Commuter Categoryand Part 25 airplanes. If the acceler-ate/stop and OEI accelerate/go dis-tances are equal, the TOFL is the bal-anced field length.
Landing distance (LD) is shown for Part23 Commuter Category and Par t 25Transport Category airplanes. The land-ing weight is BOW plus four passengersand NBAA IFR fuel reser ves. Weassume that 80,000-pound-plus ultra-long-range aircraft will have eight pas-sengers on board.
The V2 and VREF speeds are useful forreference when comparing the TOFLand LD numbers because they pro-vide an indication of potential mini-mum-length runway performance whenlow RCR or runway gradient is a factor.
B&CA lists two additional numbersfor large turboprop- and turbofan-pow-ered airplanes. First, we publish theMission Weight, which is the lower of:
(1) The actual takeoff weight withfour passengers (eight passengersfor ULR aircraft) and full fuel when de-parting from a 5,000-foot/25°C airport.
(2) The maximum allowable takeoffweight based when departing with thesame passenger load and at the samedensity altitude.
For two-engine aircraft, the missionweight, when departing from a 5,000-foot, ISA+20°C airpor t, may be lessthan the MTOW because of Par t 25second-segment, OEI, climb per form-ance requirements. Aircraft with highlyflat-rated engines are less likely to havea mission weight that is performancelimited when departing from hot-and-high airports.
For three- or four-engine aircraft, themission weight usually is based onfull tanks and the actual number of pas-sengers, rather than being performancelimited.
Second, we publish the NBAA IFR Rangefor the hot-and-high departure missionweight, assuming a transition into stan-dard day, ISA flight conditions after take-
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114 Business & Commercial Aviation n May 2006
NBAA IFR RANGE PROFILE
Climb to 5,000 ft and Hold Five Minutes for Clearance to Alternate
Standard Instrument Approach (Fuel = 5 Minute Hold @ 5,000 ft)
Conditions: Origin, destination and alternate airports are sea level elevation, ISA, zero wind, maximum of three cruise levels, �
30-minute VFR fuel reserve at alternate.
Step
Clim
b
Intermediate Cruise
Taxi
:1
0
Take
off
:01
3,0
00-fp
m D
esce
nt
to Ini
tial
App
roac
h Fi
x
3,0
00-fp
m D
esce
nt t
o
VFR
Lan
ding
at
Alt
erna
te
Long-Range Cruise for 200 nm AlternateInitial Cruise
Final Cruise
Step
Clim
b
Clim
b to
200 n
m
Alt
erna
te C
ruis
e
Alt
itud
e
NBAA IFR Range Profile
off. For purposes of computing NBAAIFR range, the aircraft is flown at thelong-range cruise speed shown in the“Cruise” block or at the same speed asshown in the “Range” block.
ClimbThe all-engine time to climb provides anindication of overall climb performance,especially if the aircraft has an all-engine service ceiling well above oursample top-of-climb altitudes.
We provide the all-engine time toclimb to one of three specific altitudes,based on type of aircraft departing atMTOW from a sea-level, standard-dayairport:
(1) FL 100 (10,000 feet) for normallyaspirated single-engine and multienginepiston aircraft, plus pressurized single-engine piston aircraft and un-pres-surized turboprop aircraft.
(2) FL 250 for pressurized single-engine and multiengine turboprops.
(3) FL 370 for turbofan-powered air-craft. The data are published as timeto climb in minutes/climb altitude.For example, if a non-pressurizedtwin-engine piston aircraft can departfrom a sea-level airport at MTOW andclimb to 10,000 feet in eight minutes,the time to climb is expressed as8/FL 100.
We also publish the initial all-engineclimb feet-per-nautical-mile gradient,plus initial engine-out climb rate andgradient, for single-engine and multi-engine pistons and turboprops withMTOWs of 12,500 pounds or less.
The OEI climb rate for multiengine air-craft at MTOW is derived from theAirplane Flight Manual. OEI climb rateand gradient is based on landing gearretracted and wing flaps in the takeoffconfiguration used to compute the pub-lished takeoff distance.
The climb gradient for such airplanesis obtained by dividing the product ofthe climb rate (fpm) in the AirplaneFlight Manual times 60 by the VY orVYSE climb speed, as appropriate.
The OEI climb gradients we show forPart 23 Commuter Category and Part25 Transport Category aircraft are thesecond-segment net climb performancenumbers published in the AFMs. Pleasenote:
The AFM net second-segment climbper formance numbers are adjusteddownward by 0.8 percent to compen-sate for variations in pilot techniqueand ambient conditions.
The OEI climb gradient is computedat the same flap configuration used tocalculate the takeoff field length.
Ceilings (ft)Maximum Certificated Altitude — Maximumallowable operating altitude determinedby airworthiness authorities.
All-Engine Service Ceiling — Maximumaltitude at which at least a 100-fpmrate of climb can be attained, assumingthe aircraft departed a sea-level, stan-dard-day airport at MTOW and climbeddirectly to altitude.
OEI (engine-out) Service Ceiling —Maximum altitude at which a 50-fpmrate of climb can be attained, assumingthe aircraft departed a sea-level, stan-dard-day airport at MTOW and climbeddirectly to altitude.
Sea-Level Cabin — Maximum cruisealtitude at which a 14.7-psia, sea-levelcabin altitude can be maintained in apressurized airplane.
CruiseCruise performance is computed usingEOW with four occupants or BOW withfour passengers and one-half fuel load.Ultra-long-range aircraft carr y eightpassengers for purposes of computingcruise per formance. Assume 170pounds for each occupant of a piston-engine airplane and 200 pounds foreach occupant of a turbine-poweredaircraft.
Long Range — TAS, Fuel Flow inpounds/hour, flight level (FL) cruiseAltitude and Specific Range for long-rangecruise by the manufacturer.
Recommended (piston-engine air-planes) — TAS, Fuel Flow in pounds/hour,flight level (FL) cruise Altitude andSpecific Range for normal cruise perfor-mance specified by the manufacturer.
High Speed — TAS, Fuel Flow in pounds/hour, flight level (FL) cruise Altitude andSpecific Range for shor t-range, high-speed per formance specified by themanufacturer.
Speed, fuel flow, specific range andaltitude in each category are basedon one mid-weight cruise point. Theyare not an average for the overallmission.
B&CA imposes a 12,000-foot maxi-mum cabin altitude requirement onCAR3/ FAR Part 23 normally aspiratedaircraft. Turbocharged airplanes arelimited to FL 250, providing they are fit-ted with supplemental oxygen systemshaving sufficient capacity for all occu-pants for the duration of the mission.
Pressurized CAR 3/FAR Par t 23 aircraft are limited to a maximum cabinaltitude of 10,000 feet. For Par t 23Commuter Category and Part 25 air-craft, the maximum cabin altitude for computing cruise per formance is8,000 feet.
To conserve space, we use flight lev-els (FL) for all cruise altitudes, whichis appropriate considering that weassume standard day ambient tem-perature and pressure conditions.Cruise per formance is subject toB&CA’s verification.
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During recent years, the U.S. Federal Trade Commissionhas conducted investigations into the practice of cer-tain industries in fixing and advertising list prices. It isthe position of the FTC that it is deceptive to the publicand against the law for list prices of any product to bespecified or advertised in a trade area if the majority ofsales are made at less than those prices.
B&CA is not in a position to know the prices for mostof the sales in each trading area in the United Statesfor each of the products in this issue. Therefore, theprices shown in the tables and text in the PurchasePlanning Handbook are based on suggested list pricesfurnished to us by the manufacturers or distributors, oron prices estimated by the editors. It may be possibleto purchase some items in your trading area at pricesless than those reported in this issue of B&CA. Also, al-most all manufacturers and distributors caution thatprices are subject to change without notice.
NOTICE TO READERS
Bombardier Learjet 45XR
Bom
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ier
116 Business & Commercial Aviation n May 2006
RangesB&CA shows various paper missions foreach aircraft that illustrate range versuspayload tradeoffs, runway and cruiseper formance, plus fuel ef ficiency.Similar to the cruise profile calcula-tions, B&CA limits the maximum alti-tude to 12,000 feet for normally aspirat-ed, non-pressurized CAR 3/FAR Part 23aircraft, 25,000 feet for turbochargedairplanes with supplemental oxygen,10,000 feet cabin altitude for pressur-ized CAR 3/FAR Part 23 airplanes and8,000 feet cabin altitude for Part 23Commuter Category or Part 25 aircraft.
Seats-Full Range (single-engine pistonairplanes) — Based on typical execu-tive configuration with all seats filledwith 170-pound occupants, with maxi-mum available fuel less 45-minute IFRfuel reser ves. We use the lower ofseats full or maximum payload.
Tanks-Full Range (single-engine pistonairplanes) — Based on one 170-poundpilot, full fuel less 45-minute IFR fuelreserves.
Executive Payload (multiengine pistonairplanes and single-engine turboprops)— Based on typical executive configu-ration with all seats filled with 170-pound occupants, maximum availablefuel less 45-minute IFR fuel reserves.
We use the lower of seats full or maxi-mum payload.
Max Fuel With Available Payload (single-engine turboprops) — Based on BOW,plus full fuel and the maximum avail-able payload up to maximum rampweight. Range is based on arriving atdestination with NBAA IFR fuelreserves, but only a 100-mile alternateis required.
Ferry (multiengine piston airplanesand single-engine turboprops) — Basedon one 170-pound pilot, maximum fuelless 45-minute IFR fuel reserves.
Please note: None of the missions forpiston-engine aircraft include fuel fordiverting to an alternate. However, sin-gle-engine turboprops are required tohave NBAA IFR fuel reserves, but only a100-mile alternate is required.
NBAA IFR range format cruise pro-files, having a 200-mile alternate, areused for Part 25 Transport Category tur-bine-powered aircraft. In the case ofPart 23 turboprops, including those cer-tificated in the Commuter Category, andPart 23 turbofan aircraft, only a 100-mile alternate is needed. The differencein alternate requirements should bekept in mind when comparing range per-formance of various classes of aircraft.
Max Payload With Available Fuel (multi-engine turbine airplanes) — Based onaircraft loaded to maximum zero fuelweight with maximum available fuel upto maximum ramp weight, less NBAAIFR fuel reserves at destination.
Max Fuel With Available Payload (multi-engine turbine airplanes) — Based onBOW plus full fuel and maximum avail-able payload up to maximum rampweight. Range based on NBAA IFRreserves at destination.
Full/Max Fuel With Four Passengers (multi-engine turbine airplanes) — Based onBOW plus four 200-pound passengers
and the lesser of full fuel or maximumavailable fuel up to maximum rampweight. Ultra-long-range aircraft musthave eight passengers on board.
Ferry (multiengine turbine airplanes) —Based on BOW, required crew and fullfuel, arriving at destination with NBAAIFR fuel reserves.
We allow 2,000-foot increment stepclimbs above the initial cruise altitudeto improve specific range per form-ance. The altitude shown in the rangesection is the highest cruise altitudefor the trip — not the initial cruise ormid-mission altitude.
The range profiles are in NauticalMiles, and the Average Speed is comput-ed by dividing that distance by thetotal flight time or weight-off-wheelstime en route. The Fuel Used or Trip Fuelincludes the fuel consumed for start,taxi, takeoff, cruise, descent and land-ing approach, but not after-landing taxior reserves.
The Specific Range is obtained by divid-ing the distance flown by the total fuelburn. The altitude is the highest cruisealtitude achieved on the specific mis-sion profile shown.
MissionsVarious paper missions are computedto illustrate the runway requirements,speeds, fuel burns and specific range,plus cruise altitudes. The missionranges are chosen to be representativefor the airplane category.
All fixed-distance missions are flownwith four passengers on board, exceptfor ultra-long-range airplanes, whichhave eight passengers on board. Thepilot is counted as a passenger onboard piston-engine airplanes. If an air-plane cannot complete a specific fixeddistance mission with the appropriatepayload, B&CA shows a reduction ofpayload in the remarks section ormarks the fields NP (Not Possible) atour option.
Runway per formance is obtainedfrom the Approved Airplane Flight
B u s i n e s s A i r p l a n e s
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BCA • ISSUE: May 2006PAGE: 116 / Version: #1
Liftoff35'
Gear Up
Flaps Up (If Applicable)Flaps Up (If Applicable)
Obstacle
Accelerate-Go Takeoff Field Length
Initial OEI Climb (Gear Down) Ob
stac
le H
eigh
t Abo
ve
Refe
renc
e Ze
ro
First
Segment
Crucial Second Segment
Third or Transition Segment
Fourth or Final Segment
OEI En Route Climb Performance
Takeoff Flight Path/OEI Climb Gradient (Gear Up)
Brake BrakeReleaseRelease
Reference ReferenceZeroZero Actual Climb Gradient Required Actual Climb Gradient Required
to Clear Close-in Obstructionto Clear Close-in Obstruction
Accelerate-Stop Accelerate-StopDistanceDistance
Distance From Reference Zero Distance From Reference ZeroDistance From Reference Zero
Brake Release
Reference Zero Actual Climb Gradient Required
to Clear Close-in Obstruction
Accelerate-Stop Distance
Flaps Up (If Applicable)
FAR Part 25 and Part 23 Commuter Category OEI Climb Performance
B&
CA
Dassault 2000EX M28 Skytruck
Das
saul
t
PZ
L
Business & Commercial Aviation n May 2006 117www.AviationNow.com/BCA
BCA • ISSUE: May 2006PAGE: 117 / Version: #1
Manual. Takeof f distance is listedfor single-engine airplanes; acceler-ate/stop distance is listed for piston-twins and light turboprops; and take-of f field length, which often corre-sponds to balanced field length, isused for Part 23 Commuter Categoryand Part 25 large Transport Categoryairplanes.
Flight Time (takeoff to touchdown, orweight-off-wheels, time) is shown forturbine airplanes. Some piston-enginemanufacturers also include taxi time,resulting in a chock-to-chock, blocktime measurement. Fuel Used, though, isthe actual block fuel burn for each typeof aircraft, but it does not include fuelreserves. The cruise Altitude shown isthat which is specified by the manufac-turer for fixed-distance missions.
200 nm — Piston-engine airplanes.500 nm — Piston-engine airplanes.300 nm — Turbine-engine airplanes,
except ultra-long-range.600 nm — Turbine-engine airplanes,
except ultra-long-range.1,000 nm — All turbine-engine
airplanes.3,000 nm — Ultra-long-range, turbine-
engine airplanes.6,000 nm — Ultra-long-range, turbine-
engine airplanes.
RemarksIn this section, B&CA generallyincludes the base price, if it is availableor applicable; the certification basisand year; and any notes about estima-tions, limitations or qualificationsregarding specifications, performanceor price.
All prices are in 2006 dollars, FOB ata U.S. delivery point, unless otherwisenoted. The certification basis includesthe regulation under which the airplaneoriginally was type cer tificated, theyear in which it originally was certificat-ed and, if applicable, subsequent yearsduring which the airplane wasre-certificated.
“All data preliminary” indicates thatactual aircraft weight, dimension andper formance numbers may vary con-siderably after the model is cer tifi-cated and deliver y of completedaircraft begins. These aircraft are listedin italics.
GeneralThe following abbreviations are usedthroughout the tables: “NA” means notavailable; “—” indicates the informa-tion is not applicable; and “NP” signi-fies that specific per formance is notpossible. B&CA
Jets ≥20,000 lb
Jets <20,000 lb
Turboprops >12,500 lb
Turboprops ≤12,500 lb
Single-Engine Turboprops
Multiengine Pistons, Turbocharged
Multiengine Pistons
Single-Engine Pistons, Pressurized
Single-Engine Pistons, Turbocharged
Single-Engine Pistons
l Required l Dual required
B&CA Required Equipment List
POWERPLANT SYSTEMSBatt temp indicator (nicad only, for each battery) l l l l lEngine synchronization l lFire detection, each engine l l l l lFire extinguishing, each engine l l lPropeller, reversible pitch l l lPropellers, synchronized l lThrust reversers/attenuators l l
AVIONICSADF l l l l lAir data computer l l l lAltitude alerter l l l l lAltitude encoder l l l l l l l l l lAntennas, headsets, microphones l l l l l l l l l lAudio control panel l l l l l l l l l lAutomatic flight guidance, 2-axis, alt hold l l lAutomatic flight guidance, 3-axis, alt hold l l l l l l lDME l l l l lEFIS l l l lELT l l l l l l l l l lFlight director l l l lFMS, TSO C115 or GPS, TSO C129 IFR approach l l l l l l l l l lGlideslope receiver l l l l l l l l l lHSI, slaved (or equivalent EFIS function) l l l l l l l l l lMarker beacon receiver l l l l l l l l l lRadio altimeter l l l l lRadiotelephone l l lRMI (or equivalent function on EFIS display) l l l l lRVSM certification l lTAWS l lTCAS I/II (FAR Part 25 airplanes only) l lTransponder l l l l l l l l l lVHF comm, 25-kHz spacing l l l l l l l l l lVHF comm, 8.33-kHz spacing l lVHF nav, 360-channel l l l l l l l l l lWeather radar l l l l l
GENERALAir conditioning, vapor cycle (not required with APU) l l l l l lAnti-skid brakes l l lAPU (required for air-start engines, ACM air conditioning) lCabin/cockpit dividers l l lCorrosion-proofing, internal l l l l l l l l l lExterior paint, tinted windows l l l l l l l l l lFire extinguisher, cabin l l l l lFire extinguisher, cockpit l l l l l l l l l lFuel tanks, long-range l l l l l l l lGround power jack l l l l l l l l l lHeadrests, air vents, all seats l l l l l l l l l lLavatory l l lLights, strobe/anti-collision beacon, navigation, landing/taxi l l l l l l l l l lLights, internally lighted instrument, cockpit flood, courtesy l l l l l l l l l lOxygen, supplemental, all seats l l l l l l lRefreshment center l l l lSeats, crew, articulating l l l l l l l l l lSeats, passenger, reclining l l l l l l l l l lShoulder harness, all seats and crew with inertia reel l l l l l l l l l lTables, cabin work l l l l l
ICE AND RAIN PROTECTIONAlternate static pressure source (not required with 2 DADC) l l l l l l lApproval, flight into known icing l l l l l l l lIce protection plates l lPitot heat l l l l l l l l l lStatic wicks l l l l l l l l l lWindshield rain removal, mechanical or repellent coating l l l l
INSTRUMENTATIONAngle-of-attack stall margin indicator l lEGT l l l l lIVSI (or equivalent EFIS, DADC function) l l l lOutside air temperature gauge l l l l l l l l l lPrimary flight instruments l l l l l l l l l l
118 Business & Commercial Aviation n May 2006
B u s i n e s s A i r p l a n e s
www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engine
Output (hp)Inspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelEOW
Max PayloadUseful Load
Max BaggageMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Limits VNE
VNO
VA
Airport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
VSO
VX
VY
Climb Time to Climb (min.)/AltitudeInitial Gradient (ft/nm)
Ceiling (ft) ServiceCruise Long TAS
Range Fuel FlowAltitude
Specific RangeRec’d TAS
Fuel FlowAltitude
Specific RangeHigh TASSpeed Fuel Flow
AltitudeSpecific Range
Ranges Seats Nautical MilesFull Average Speed
Fuel UsedSpecific Range/AltitudeTanks Nautical MilesFull Average Speed
Fuel UsedSpecific Range/Altitude
Missions 200 nm Runway(4 occupants) Block Time
Fuel UsedSpecific Range/Altitude500 nm Runway
Block TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
Cirrus DesignSR20-G2
SR20$249,750
1+3/322.215.0083.426.08.635.58.04.14.1
ContIO-360-ES
200 hp2,000t3,0003,0002,9002,900c2,070830930130336594100200165131
2,0643,486
568196
16/FL 100581
17,50014050
FL 0802.80015263
FL 0802.41315970
FL 0802.271584140210
2.781/FL 080764140275
2.778/FL 0801,4461 + 18100
2.000/FL 0801,4463 + 17226
2.212/FL 080$236,700
FAR 23, 1999
CessnaSkylaneCE-182T
$326,150 1+3/317.813.4877.729.09.336.07.24.03.5Lyc
IO-540-AB1A5230 hp2,000t3,1103,1002,9502,985b1,9441,0411,166200522644126175140110
1,3502,708
506582
15/FL 100694
18,10012360
FL 1002.05013568
FL 1001.98514077
FL 0601.818735120435
1.690/FL 060980123471
2.081/FL 1001,5141 + 29128
1.563/FL 0601,5143 + 37274
1.825/FL 060$258,500
FAR 23, 1996/01Includes G1000with TIS, XM wxand Stormscope.
Cirrus DesignSR22-G2
SR22$349,750
1+3/323.510.9783.726.08.838.38.04.14.1
ContIO-550-N310 hp1,700t3,4003,4003,4003,250b2,2501,0001,150130486664150201178133
1,5752,717
5978101
10/FL 100864
17,50016279
FL 0802.05117291
FL 0801.890181100
FL 0801.810841162411
2.046/FL 080873162427
2.044/FL 0801,0201 + 06122
1.639/FL 0801,3412 + 45308
1.623/FL 080$334,700
FAR 23, 2000
New PiperArrow
PA-28R-200$360,650
1+3/316.213.7575.524.77.935.47.34.13.5Lyc
IO-360-C1C6200 hp2,000t2,7582,7502,7502,645b1,787858971200432539113186148120
1,6003,200
557290
17/FL 100584
16,20011748
FL 0802.43813155
FL 0802.38214270
FL 0802.029327136159
2.057/FL 080907135396
2.290/FL 0801,3501 + 28107
1.869/FL 0801,4803 + 41230
2.174/FL 080$292,400
CAR 3, 1960/78
LancairColumbia 350LC42-550FG$378,900
1+3/324.110.9784.025.29.036.17.94.24.2
ContIO-550-N310 hp2,000t3,4003,4003,2303,228c2,400828
1,000120588412172235179148
1,2501,800
5780106
11/FL 100947
18,00015464
FL 0802.40618397
FL 0801.887191104
FL 0801.837580153320
1.813/FL 0801,242153515
2.412/FL 0801,2501 + 10109
1.835/FL 0801,2502 + 48246
2.033/FL 120$378,900 FAR 23
Includes AvidyneEntegra.
SINGLE-ENGINE PISTONS NORMALLY ASPIRATED
Business & Commercial Aviation n May 2006 119www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engine
Output (hp)Inspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelEOW
Max PayloadUseful Load
Max BaggageMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Limits VNE
VNO
VA
Airport TO (SL elev./ISA temp)Performance TO (5,000’ elev. @25
0C)
VSO
VX
VY
Climb Time to Climb (min.)/AltitudeInitial Gradient (ft/nm)
Ceiling (ft) ServiceCruise Long TAS
Range Fuel FlowAltitude
Specific RangeRec’d TAS
Fuel FlowAltitude
Specific RangeHigh TASSpeed Fuel Flow
AltitudeSpecific Range
Ranges Seats Nautical MilesFull Average Speed
Fuel UsedSpecific Range/AltitudeTanks Nautical MilesFull Average Speed
Fuel UsedSpecific Range/Altitude
Missions 200 nm Runway(4 occupants) Block Time
Fuel UsedSpecific Range/Altitude500 nm Runway
Block TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
SocataTrinidad GTTB-20 GT$381,500
1+3/424.112.3474.025.39.432.18.33.94.2Lyc
IO-540-C4D5D250 hp2,000t3,0973,0863,0862,959b1,8151,1441,282143517765139189151130
2,0833,400
588195
12/FL 100783
20,00013964
FL 1002.17215173
FL 1002.06816585
FL 1001.941715150355
2.014/FL 100935149469
1.994/FL 1001,5601 + 12104
1.923/FL 1001,6503 + 11248
2.016/FL 100$381,500
FAR 23, 1981/84Includes KFC225,
KMD 550, WX 500; Garmin430/530 opt’l.
MooneyOvation2 GX
M-20R$442,000
1+3/419.312.0372.626.98.336.18.13.73.6
ContIO-550-G280 hp2,000t3,3743,3683,2003,226b2,260966
1,114120612502149195174123
1,6201,980
5980105
11/FL 100714
20,00016350
FL 1203.26018684
FL 1202.21419095
FL 0802.0001,075161438
2.454/FL 1201,465173558
2.625/FL 1201,2301 + 13115
1.739/FL 0501,2902 + 58221
2.262/FL 100$442,000
CAR 3, 1955/94Includes Garmin
G1000.
CessnaStationairCE-206H$448,160
1+5/520.712.0084.528.39.336.09.34.13.7Lyc
IO-540-AC1A5300 hp2,000t3,6143,6003,6003,448b2,2021,2461,412200522890166182149125
1,8603,375
577086
15/FL 100691
15,70012778
FL 1201.62813588
FL 0801.534142100
FL 0601.420326123326
1.000/FL 060595127456
1.305/FL 1201,8601 + 33166
1.205/FL 0601,8603 + 36377
1.326/FL 060$448,160
FAR 23, 1998Includes G1000with TIS, XM wxand Stormscope.
New PiperPiper 6X
PA-32-201FT$453,000
1+4/520.212.0083.927.98.536.29.73.54.1Lyc
IO-540-K1G5300 hp2,000t3,6153,6003,6003,434b2,2141,2201,401200612789182189150132
2,0283,763
598090
15/FL 100967
17,20013687
FL 1201.56314499
FL 1001.455149111
FL 0701.342403128386
1.044/FL 080800132547
1.463/FL 1001,5001 + 25159
1.258/FL 1001,7203 + 50359
1.393/FL 100$382,900
CAR 3, 1965/96Includes Avidyne
Entegra.
BeechcraftBonanza
G36$691,390
1+4/520.212.1776.727.58.633.512.64.23.5
ContIO-550-B300 hp1,700t3,6633,6503,6503,509b2,530979
1,133670444689154203165139
1,9134,145
5984100
14/FL 100730
18,50013756
FL 1202.44616380
FL 1002.03817494
FL 0801.851527130240
2.196/FL 040930140403
2.308/FL 0801,7501 + 11130
1.538/FL 0601,8502 + 54304
1.645/FL 060$667,000
CAR 3,1956/69/83/05Includes Garmin
G1000.
SINGLE-ENGINE PISTONS NORMALLY ASPIRATED
120 Business & Commercial Aviation n May 2006
B u s i n e s s A i r p l a n e s
www.AviationNow.com/BCA
SINGLE-ENGINE PISTONS TURBOCHARGED
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engine
Output (hp)Inspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelEOW
Max PayloadUseful Load
Max BaggageMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Limits VNE
VNO
VA
Airport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
VSO
VX
VY
Climb Time to Climb/AltitudeInitial Gradient (ft/nm)
Ceilings (ft) CertificatedService
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
Rec’d TASFuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
Ranges Seats Nautical MilesFull Average Speed
Fuel UsedSpecific Range/AltitudeTanks Nautical MilesFull Average Speed
Fuel UsedSpecific Range/Altitude
Missions 200 nm Runway(4 occupants) Block Time
Fuel UsedSpecific Range/Altitude500 nm Runway
Block TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
CessnaTurbo Skylane
CE-T182T$355,050
1+3/317.813.1975.429.09.436.07.24.03.5Lyc
TIO-540-AK1A235 hp2,000t3,1123,1002,9502,971b2,042929
1,070200522548141175140110
1,3501,928
506484
10/FL 100743
20,00020,000
13262
FL 2002.12914772
FL 2002.04215886
FL 2001.837542121334
1.623/FL 060814132468
1.739/FL 2001,8601 + 28143
1.399/FL 0601,8603 + 05300
1.667/FL 200$355,050
FAR 23, 2001Includes Garmin
G1000.
SocataTrinidad GT T/C
TB-21 GT$431,670
1+3/424.112.3476.025.39.432.18.33.94.2Lyc
TIO-540-AB1AD250 hp2,000t3,0863,0863,0862,939b1,990949
1,096143517579147189151130
1,9222,411
598195
10/FL 100711
25,00025,000
14067
FL 1002.09015474
FL 1002.08116698
FL 1501.694484154246
1.967/FL 150917153461
1.989/FL 1001,5601 + 12111
1.802/FL 1001,6503 + 11244
2.049/FL 100$431,670
FAR 23, 1986Includes KFC225.
LancairColumbia 400LC41-550-FG
$479,900 1+3/425.511.6179.025.29.036.17.94.24.2
ContTSIO-550-C
310 hp2,000t3,6003,6003,4203,390b2,500890
1,100120588512210230181158
1,3001,730
5982110
7/FL 100993
25,00025,000
20878
FL 2502.667227120
FL 2501.892235140
FL 2501.679831203325
2.557/FL 1001,279203493
2.594/FL 2501,3001 + 03155
1.290/FL 2501,3002 + 24322
1.553/FL 250$479,900 FAR 23
Includes AvidyneEntegra.
CessnaTurbo Stationair
CE-T206H$482,160
1+5/520.711.6175.828.39.336.09.34.13.7Lyc
TIO-540-AJ1A310 hp2,000t3,6173,6003,6003,429b2,3191,1101,298200522776190182149125
1,7402,498
576989
11/FL 100724
25,00027,000
13785
FL 2401.61215498
FL 2401.571164114
FL 2001.439202126204
0.990/FL 060547136448
1.221/FL 2001,7401 + 25188
1.064/FL 0601,7403 + 13416
1.202/FL 200$482,160
FAR 23, 1998Includes Garmin
G1000.
New PiperPiper 6XT
PA-32-301XTC$490,315
1+4/520.212.0077.627.98.536.29.73.54.1Lyc
TIO-540-AH1A300 hp2,000t3,6153,6003,6003,420b2,2741,1461,341200612729195189150132
1,8882,742
598090
14/FL 100680
20,00020,000
13975
FL 1201.853156102
FL 1201.529164120
FL 1201.367361132319
1.132/FL 100945137547
1.728/FL 1001,5001 + 25159
1.258/FL 0801,7003 + 19356
1.404/FL 140$401,600
CAR 3 56/97Includes Avidyne
FlightMaxEntegra.
MooneyAcclaimMO-20TN$495,000
1+3/519.312.03TBD26.98.336.48.13.73.6
ContTSIO-550-G
280 hp2,000t3,3743,3683,2003,152b2,353799
1,021120612409222195174127
1,6201,980
6080105
7/FL 1001,12525,00025,000
20081
FL 2502.469230144
FL 2501.597230144
FL 2501.597520195274
1.898/FL 2001,200198551
2.178/FL 2501,3401 + 02135
1.481/FL 1201,6202 + 30270
1.852/FL 250$495,000
CAR 3,1955/89/pend.Includes GarminG1000 . All data
preliminary.
Business & Commercial Aviation n May 2006 121www.AviationNow.com/BCA
SINGLE-ENGINE PISTONS PRESSURIZED
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engine
Output (hp)Inspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelEOW
Max PayloadUseful Load
Max BaggageMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Limits VNE
VNO
VA
PSIAirport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
VSO
VX
VY
Climb Time to Climb (min.)/AltitudeInitial Gradient (ft/nm)
Ceilings (ft) CertificatedService
Sea-level CabinCruise Long TAS
Range Fuel FlowAltitude
Specific RangeRec’d TAS
Fuel FlowAltitude
Specific RangeHigh TASSpeed Fuel Flow
AltitudeSpecific Range
Ranges Seats Nautical MilesFull Average Speed
Fuel UsedSpecific Range/AltitudeTanks Nautical MilesFull Average Speed
Fuel UsedSpecific Range/Altitude
Missions 200 nm Runway(4 occupants) Block Time
Fuel UsedSpecific Range/Altitude500 nm Runway
Block TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
New PiperMalibu MiragePA-46-350P$970,000
1+4/524.812.4074.528.911.343.012.43.94.2Lyc
TIO-540-AE2A350 hp2,000t4,3584,3404,1234,123c3,1001,0231,2582007205382351981681335.5
2,0902,977
5881110
8/FL 100703
25,00025,00012,300
15666
FL 2502.364203108
FL 2501.880212120
FL 2501.767212129149
1.423/FL 0701,370158670
2.045/FL 2502,0901 + 06170
1.176/FL 1702,0902 + 30352
1.420/FL 250$970,000
FAR 23, 1983/88
SINGLE-ENGINE PISTONS TURBOCHARGED
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engine
Output (hp)Inspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelEOW
Max PayloadUseful Load
Max BaggageMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Limits VNE
VNO
VA
Airport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
VSO
VX
VY
Climb Time to Climb/AltitudeInitial Gradient (ft/nm)
Ceilings (ft) CertificatedService
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
Rec’d TASFuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
Ranges Seats Nautical MilesFull Average Speed
Fuel UsedSpecific Range/AltitudeTanks Nautical MilesFull Average Speed
Fuel UsedSpecific Range/Altitude
Missions 200 nm Runway(4 occupants) Block Time
Fuel UsedSpecific Range/Altitude500 nm Runway
Block TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
New PiperSaratoga II TCPA-32R-301T
$581,600 1+4/520.212.0076.627.98.536.29.73.54.1Lyc
TIO-540-AH1A300 hp2,000t3,6153,6003,6003,420b2,486934
1,129200612517195197154134
1,8102,680
638595
9/FL 100753
20,00020,000
16675
FL 2002.21318499
FL 2001.859194138
FL 2001.406354142204
1.735/FL 0801,058161540
1.959/FL 1801,6701 + 07177
1.130/FL 2001,7802 + 57333
1.502/FL 150$548,700
CAR 3, 56/97Seats-full range
based onfive occupants.
122 Business & Commercial Aviation n May 2006
B u s i n e s s A i r p l a n e s
www.AviationNow.com/BCA
MULTIENGINE PISTONS TURBOCHARGED
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engines
Output (hp ea.)Inspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelEOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Payload – Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits VNE
VNO
VA
PSIAirport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
A/S (SL elev./ISA)A/S (5,000’ elev. @ 25
0C)
VMCA
VDEC
VXSE
VYSE
Climb Time to Climb (min.)/AltitudeInitial Engine-Out Rate (fpm)
Initial All-Engine Gradient (ft/nm)Initial Engine-out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
Rec’d TASFuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
Ranges Exec. Nautical MilesPayload Average Speed
Trip FuelSpecific Range/Altitude
Ferry Nautical MilesAverage Speed
Trip FuelSpecific Range/Altitude
Missions 200 nm Runway(4 occupants) Block Time
Fuel UsedSpecific Range/Altitude
500 nm RunwayBlock Time
Fuel UsedSpecific Range/Altitude
Remarks Suggested Base PriceCertification Basis
Vulcanair SpAP 68C-TCP 68C-TC$639,000
1+5/520.710.9474.731.3311.239.410.63.93.8
2 LycTIO-360-C1A6D
210 hp ea.2,000t4,6304,5944,3654,167c2,9761,1911,6541,0201,146508463634193153126—
1,2602,2002,3003,000
63NANANA
10/FL 100240
1,400NA
20,00020,00011,500
—144100
FL 0801.440155125
FL 0801.240162150
FL 0801.0801,050145942
1.115/FL 0801,100145950
1.158/FL 080NA
1 + 28260
0.769/FL 080NA
3 + 25485
1.031/FL 080$539,000
FAR 23, 1982Data B&CA est.
Sagem glass c’pit.
PiperSeneca V
PA-34-220T$797,330
1+4/522.810.8075.628.69.938.910.43.64.8
2 ContTSIO-360-RB220 hp ea.
1,800t4,7734,7504,5134,479c3,3911,0881,382850732650294532205166140—
1,7072,4352,5103,117
66738388
11/FL 100253996173
25,00025,00016,500
—170108
FL 2301.574200144
FL 2501.389204156
FL 2501.308504156408
1.235/FL 130865159651
1.329/FL 1401,9401 + 11225
0.889/FL 1502,0402 + 44484
1.033/FL 210$669,200 FAR 23,
1971/80/97
MULTIENGINE PISTONS NORMALLY ASPIRATEDManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engines
Output (hp ea.)Inspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelEOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Payload – Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits VNE
VNO
VA
Airport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
A/S (SL elev./ISA)A/S (5,000’ elev. @ 25
0C)
VMCA
VDEC
VXSE
VYSE
Climb Time to Climb (min.)/AltitudeInitial Engine-Out Rate (fpm)
Initial All-Engine Gradient (ft/nm)Initial Engine-out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceCruise Long TAS
Range Fuel FlowAltitude
Specific RangeRec’d TAS
Fuel FlowAltitude
Specific RangeHigh TASSpeed Fuel Flow
AltitudeSpecific Range
Ranges Exec. Nautical MilesPayload Average Speed
Trip FuelSpecific Range/Altitude
Ferry Nautical MilesAverage Speed
Trip FuelSpecific Range/Altitude
Missions 200 nm Runway(4 occupants) Block Time
Fuel UsedSpecific Range/Altitude
500 nm RunwayBlock Time
Fuel UsedSpecific Range/Altitude
Remarks Suggested Base PriceCertification Basis
Vulcanair SpAP 68CP 68C
$599,000 1+5/620.711.4974.730.911.239.413.33.93.8
2 LycIO-360-A1B6200 hp ea.
2,000t46304,5944,3654,167c29101,2571,7201,0201,063657463700194154132
1,2604,0002,3004,025
60708288
12/FL 100217920147—
15,0003,80014494
FL 801.532155108
FL 801.435162116
FL 801.397575145395
1.456/FL 80855145561
1.524/FL 801,4501 + 28140
1.429/FL 801,5003 + 25375
1.333/FL 80$599,000
FAR 23, 1976/80Sagem glass
cockpit standard.
BeechcraftBaronG58
$1,222,035 1+4/527.69.1777.629.89.837.812.64.23.5
2 ContIO-550-C
300 hp ea.1,700t5,5245,5005,4005,215p3,8801,3351,644850
1,164480309794223195165
2,3004,0003,0004,330
8485100101
10/FL 100390988232—
20,6887,284163106
FL 1201.538193150
FL 1001.287200190
FL 801.053993154711
1.397/FL 401,563164
1,0811.446/FL 120
2,8501 + 02226
0.885/FL 602,9002 + 31531
0.942/FL 60$1,186,000
CAR 3,1957/69/83/05Inlcudes Garmin
G1000.
Business & Commercial Aviation n May 2006 123www.AviationNow.com/BCA
MULTIENGINE PISTONS PRESSURIZED
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engines
Output (hp ea.)Inspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelEOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Payload – Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits VNE
VNO
VA
PSIAirport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
A/S (SL elev./ISA)A/S (5,000’ elev. @ 25
0C)
VMCA
VDEC
VXSE
VYSE
Climb Time to Climb (min.)/AltitudeInitial Engine-Out Rate (fpm)
Initial All-Engine Gradient (ft/nm)Initial Engine-out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
Rec’d TASFuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
Ranges Exec. Nautical MilesPayload Average Speed
Trip FuelSpecific Range/Altitude
Ferry Nautical MilesAverage Speed
Trip FuelSpecific Range/Altitude
Missions 200 nm Runway(4 occupants) Block Time
Fuel UsedSpecific Range/Altitude
500 nm RunwayBlock Time
Fuel UsedSpecific Range/Altitude
Remarks Suggested Base PriceCertification Basis
Adam AircraftA500A500
$1,150,000 1+5/541.210.0088.036.79.544.013.64.34.5
2 ContTSIO-550-E3B/E4B
350 hp ea.1,600t7,0507,0006,7506,500c4,2502,2502,8001,0201,3201,480550
1,7802281661615.5
2,471NANANANA8190105
10/FL 100227912151
25,00025,00016,00012,400
200153
FL 2501.307230209
FL 2501.100230209
FL 2501.100449923408
1.100/FL 2501,541200
1,2231.260/FL 250
NA1 + 02210
0.952/FL 180NA
2 + 24483
1.035/FL 250NA
FAR 23 A 55All data preliminary.
SINGLE-ENGINE TURBOPROPSManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engine
Output (shp)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits VMO
VAPSI
Airport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
VSOVXVY
Climb Time to Climb (min.)/AltitudeInitial Gradient (ft/nm)
Ceilings (ft) CertificatedService
Sea-level CabinCruise Long TAS
Range Fuel FlowAltitude
Specific RangeHigh TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Exec. Nautical MilesRanges Payload Average Speed(100 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeMissions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayFlight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
Vulcanair SpA MissionVF-600w
$1,300,0001+9/932.211.0776.843.014.050.116.63.74.1
WalterM601F
777/ISA+8°C3,000t8,6538,5988,2017,937c5,1812,7563,4721,8002,2041,268716
1,672190143NA
2,020NA6195125
NA/FL 100NANANA—NANANANANANANANANANANA
NA/NANANANA
NA/NANANANA
NA/NANANANA
NA/NANANANA
NA/NANANANA
NA/NA$1,300,000
FAR/EASA 23pending
Extra AircraftEA 500
$1,345,000 1+5/530.510.4479.033.211.138.313.64.14.6RR
250-B17F/2450/ISA+10°C
3,500t4,6964,6964,4094,319c3,1861,1331,5101,0001,0324783775102191585.5
1,4001,900
6190100
15/FL 250982
25,00025,00012,300
210107
FL 2501.963230225
FL 1401.022985200593
1.661/FL 2501,600205905
1.768/FL 2501,625207905
1.796/FL 2501,2001 + 30205
1.463/FL 2501,2502 + 56400
1.500/FL 2501,3004 + 46650
1.538/FL 250$1,345,000FAR 23 A 55
pending
124 Business & Commercial Aviation n May 2006
B u s i n e s s A i r p l a n e s
www.AviationNow.com/BCA
SINGLE-ENGINE TURBOPROPSManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length
HeightWidth
Power Engine
Output (shp)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits VMO
VAPSI
Airport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
VSOVXVY
Climb Time to Climb (min.)/AltitudeInitial Gradient (ft/nm)
Ceilings (ft) CertificatedService
Sea-level CabinCruise Long TAS
Range Fuel FlowAltitude
Specific RangeHigh TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Exec. Nautical MilesRanges Payload Average Speed(100 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeMissions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayFlight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
CessnaCaravan
CE-208-675$1,693,400
1+9/928.611.8579.037.614.852.112.74.55.3
P&WCPT6A-114A
675/ISA+27°C3,600t8,0358,0007,8007,467b4,8522,6153,1831,8002,224959569
1,383175150—
2,0532,950
6190107
9/FL 100625
25,00025,000
—154276
FL 1000.558186379
FL 1000.491584181
1,2380.472/FL 100
866183
1,8120.478/FL 100
1,131157
2,0140.562/FL 120
1,1951 + 41651
0.461/FL 1001,4683 + 181,265
0.474/FL 100NPNPNPNP
$1,440,000 FAR 23, 1984/98Utility category.
CessnaGrand Caravan
CE-208B$1,744,125
1+9/931.312.9682.741.615.552.116.74.55.3
P&WCPT6A-114A
675/ISA+27°C3,600t8,7858,7508,5008,217b5,2582,9593,5271,8002,2241,303569
1,727175148—
2,4203,604
6172104
12/FL 100465
25,00023,700
—154291
FL 1000.529182379
FL 1000.480678178
1,5450.439/FL 100
834179
1,7880.466/FL 100
1,070158
2,0060.533/FL 120
1,2251 + 43667
0.450/FL 1001,4983 + 221,295
0.463/FL 100NPNPNPNP
$1,474,000 FAR 23, 1986
Utility category.
New Piper AircraftMeridian
PA-46-500T$1,924,730
1+4/527.810.1876.829.511.343.012.33.94.1
P&WCPT6A-42A
500/ISA+55°C3,600t5,1345,0924,8504,850c3,4041,4461,730800
1,1395912849301871265.5
2,4383,691
6195125
19/FL 250753
30,00030,00012,400
178135
FL 2801.319257242
FL 2801.062470170480
0.979/FL 280960245965
0.995/FL 2801,100175965
1.140/FL 2802,2001 + 20379
0.792/FL 2802,4002 + 40662
0.906/FL 2802,438*4 + 041,028
0.973/FL 280$1,895,000 FAR 23 A 52
*1,000 nm missionflown with three
passengers.
SocataTBM 850
TBM 700 N$2,799,850
1+5/639.210.5676.234.914.341.615.04.14.0
P&WCPT6A-66D
700*/ISA+49°C3,000t7,4307,3947,0246,761b4,8851,8762,5451,0001,690855669
1,5452701606.2
2,8404,282
65100124
18/FL 250750
31,00031,00014,390
255260
FL 3100.981320446
FL 2600.7171,106300
1,1960.925/FL 310
1,396255
1,6770.832/FL 310
1,396255
1,6770.832/FL 310
1,8801 + 10434
0.691/FL 2602,1002 + 011,125
0.533/FL 2602,4503 + 151,641
0.609/FL 260$2,576,930
FAR 23, 1990/03/06*850 shp max
continuous with flapsretracted; RVSM.
PilatusPC-12 Series 10
PC-12/47$3,350,000
1+7/1037.68.7174.347.314.053.316.94.85.0
P&WCPT6A-67B
1,200/ISA+36°C3,500t10,49510,4509,9219,039c6,5652,4743,9301,4002,7041,2261,4562,5302401615.8
2,6504,346
67110120
26/FL 250660
30,00030,00013,200
202230
FL 3000.878270453
FL 2200.5961,450253
2,2340.649/FL 260
1,449253
2,2330.649/FL 260
1,487258
2,2440.663/FL 260
1,6001 + 14540
0.556/FL 2601,8002 + 23974
0.616/FL 2602,0503 + 561,556
0.643/FL 260$2,792,000
FAR 23, 1996/05EASA limits
Max ramp weight9,965 lb.
MTOW 9,920 lb.
126 Business & Commercial Aviation n May 2006 www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length (OA/Net)
HeightWidth (max)/Width (floor)
Power Engines
Output (shp ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits VMO
VAPSI
Airport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25
0C)
A/S (SL elev./ISA temp.)A/S (5,000’ elev. @ 25
0C)
VMCAVDECVXSEVYSE
Climb Time to Climb (min.)/AltitudeInitial Engine-Out Rate (fpm)
Initial All-Engine Gradient (ft/nm)Initial Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(100 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFull Fuel Nautical Miles(w/4 pax) Average Speed
Trip FuelSpecific Range/Altitude
Ferry Nautical MilesAverage Speed
Trip FuelSpecific Range/Altitude
Missions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayBlock Time
Fuel UsedSpecific Range/Altitude
1,000 nm RunwayFlight TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
Vulcanair SpAViator
AP68TP 600$1,400,000
1+8/933.010.0871.737.011.939.4
17.2/11.94.1
3.7/3.72 RR
250 B17C328/ISA+25°C
3,500t6,6696,6136,2835,621c3,7041,9172,9651,6001,5011,4641,0481,365200141—
2,0342,9502,8873,740
798590105
7/FL 100NA700NA
25,00025,0009,000
—169261
FL 1000.648214375
FL 1000.571324170
1,0480.309/FL 100
590170
1,1000.536/FL 100
620170
1,1000.564/FL 100
585170
1,1000.532/FL 100
NA1 + 45563
0.533/FL 100NA
3 + 351,100
0.545/FL 100NPNPNP
NP/NP$1,300,000
FAR 23, 1986B&CA estimated
performance data.
BeechcraftKing Air C90GT
C90GT$2,952,010
1+5/1234.49.1876.035.514.350.3
12.4/12.44.8
4.5/4.12 P&WC
PT6A-135A550/ISA+30°C
3,600t10,16010,1009,6009,212b7,1502,0623,0101,0002,573437948
2,0102261695.0
2,3923,3723,3824,411
8097100108
17/FL 250474
1,953259
30,00030,00019,17011,065
208332
FL 2600.627270612
FL 2000.441178218462
0.385/FL 2601,026255
2,0740.495/FL 260
831252
1,7070.487/FL 260
1,036257
2,0780.499/FL 260
3,0541 + 14745
0.403/FL 2103,2512 + 221,347
0.445/FL 2303,368
3 + 54*2,075
0.482/FL 250$2,950,000
CAR 3, 1959/81/91*Two passengers.
Reims CessnaCaravan II
RA406$3,200,000
1+8/1338.99.3669.939.113.249.5
14.2/12.84.3
4.7/4.72 P&WC
PT6A-112500/ISA+22°C
3,500t9,4359,3609,3608,500c5,7322,7683,7031,6003,183520935
2,103229162—
2,9644,8564,3636,000
9098105111
6/FL 100320913173
30,00030,00014,800
—180416
FL 1000.433231617
FL 1000.374427179
1,0090.423/FL 100
1,188180
2,7670.429/FL 100
1,201180
2,7700.434/FL 100
1,228176
2,7870.441/FL 100
3,8151 + 21807
0.372/FL 1004,0752 + 391,609
0.373/FL 100NPNPNP
NP/NPNA
FAR 23, 1986
BeechcraftKing Air B200
B200$5,088,610
1+7/1541.37.3581.143.814.854.5
16.7/16.74.8
4.5/4.12 P&WCPT6A-42
850/ISA+26°C3,600t12,59012,50012,50011,000c8,6552,3453,9351,4003,645290
1,5902,5352601826.5
2,5793,8003,4114,600
8694115121
16/FL 250740
1,076364
35,00035,00021,90015,293
228378
FL 2900.603289700
FL 2200.413406249923
0.440/FL 3301,644267
3,0240.544/FL 330
1,331265
2,4840.536/FL 330
1,671270
3,0270.552/FL 330
3,1961 + 07793
0.378/FL 2503,2642 + 131,327
0.452/FL 2903,3643 + 392,105
0.475/FL 290$5,073,000
FAR 23, 1973/80Pro Line 21
RVSM approved.
Piaggio Aero IndustriesAvanti II
P180$6,195,000
1+7/967.07.1276.047.313.046.0
14.1/14.15.8
6.1/4.32 P&WC
PT6A-66B850/ISA+45°C
3,600*t12,15012,10011,5009,800c7,8002,0004,3501,4002,8021,5482,3502,8022601999.0
3,2624,1704,2505,700
99106132140
9/FL 250756
1,106324
41,00041,00024,70024,000
311387
FL 3900.804392781
FL 2800.502960309
1,4700.653/FL 390
1,575309
2,1700.726/FL 410
1,600301
2,1700.737/FL 410
1,686306
2,1700.777/FL 410
2,3000 + 53658
0.456/FL 3102,4101 + 441,092
0.549/FL 3502,5403 + 011,526
0.655/FL 390$6,195,000
FAR 23, 1990Includes Pro Line 21
avionics. All datapreliminary.
MULTIENGINE TURBOPROPS 12,500 LB MTOW OR LESS
128 Business & Commercial Aviation n May 2006 www.AviationNow.com/BCA
B u s i n e s s A i r p l a n e s
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (dBA)Dimensions External Length(ft) Height
SpanInternal Length (OA/Net)
HeightWidth (max)/Width (floor)
Power Engines
Output (shp ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FLVMO
VAPSI
Airport TO (SL elev., ISA temp.)Performance TO (5,000’ elev. @25
0C)
Hot/High WAT LimitNBAA IFR Range
V2VREF
Landing DistanceClimb Time to Climb (min.)/Altitude
*FAR 25 Initial Engine-Out Rate (fpm)FAR 25 Initial Engine-Out Gradient (ft/nm)Ceilings (ft) Certificated
All-Engine ServiceEngine-Out Service
Sea-Level CabinCruise Long TAS
Range Fuel FlowAltitude
Specific RangeHigh TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(100 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFull Fuel Nautical Miles(w/4 pax) Average Speed
Trip FuelSpecific Range/Altitude
Ferry Nautical MilesAverage Speed
Trip FuelSpecific Range/Altitude
Missions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayFlight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Suggested Base Price
Certification Basis
Polski Zaklady LotniczeM28 SkytruckPZL M28 05$4,750,000 2+19/21
38.77.5281.143.216.172.3
19.3/17.35.7
5.7/NA2 P&WC
PT6A-65B1,100/ISA+23°C
5,400t16,58416,53416,53415,212c9,6955,5176,8893,8003,9702,9191,3723,089
——
1921326.6
1,0664,60016,5341,050
9273682
7/FL 10650395
25,00030,00016,050
—152550
FL 100.276176720
FL 100.244205145650
0.315/FL 101,050145
3,2500.323/FL 10
1,150145
3,2750.351/FL 10
1,195145
3,2750.365/FL 10
8251 + 531,400
0.214/FL 10875
3 + 452,750
0.218/FL 101,0006 + 273,000
0.333/FL 10$4,750,000
FAR 25 pendingChelton EFIS
BeechcraftKing Air 350
350$5,970,580 1+9/15*
48.47.1472.146.714.357.9
19.5/19.54.8
4.5/4.12 P&WC
PT6A-60A1,050/ISA+10°C
3,600t15,10015,00015,00012,500c9,8502,6505,2501,8003,6111,6392,6003,450
——
2601826.6
3,3005,37614,1961,556109100
2,39015/FL 250
552304
35,00035,00021,50015,293
235362
FL 3300.649312773
FL 2400.404899274
1,8970.474/FL 350
1,489280
2,9510.505/FL 350
1,540285
2,9580.521/FL 350
1,567290
2,9640.529/FL 350
2,5641 + 02880
0.341/FL 2502,6792 + 011,467
0.409/FL 2902,8043 + 262,098
0.477/FL 330$5,954,000
FAR 23, 1989Commuter cat.
*max pax requirestwo pilots. Pro Line21 RVSM approved.
*FAR 23 for some Commuter Category aircraft.
MULTIENGINE TURBOPROPS >12,500 LB MTOW
Business & Commercial Aviation n May 2006 129www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length: OA/Net
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb. ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TOFL (SL elev., ISA temp.)Performance TOFL (5,000’ @ 25
0C)
Hot/High Weight LimitNBAA IFR RANGE
V2 @SL ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeNBAA IFR 300 nm RunwayMissions Flight Time(4 pax) Fuel Used
Specific Range/Altitude600 nm Runway
Flight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
Eclipse AviationEA 500
$1,486,000 1+4/539.03.13
NA/NA/NA33.111.037.4
7.5/5.24.2
4.7/3.026/260NA/NA2 P&WCPW610F
900/ISA+10°C3,500t5,6805,6405,3604,640c3,5901,0502,090800
1,540550
1,0401,2900.640
FL 200/2858.3
2,1553,6985,6409349483
2,04023/FL 370
506323
41,00041,00025,00021,500
331284
FL 4101.165375472
FL 3100.794637306700
0.910/FL 4101,280316
1,2401.032/FL 410
934316950
0.983/FL 4101,315316
1,2401.060/FL 410
1,9700 + 54622
0.482/FL 1802,1251 + 43899
0.667/FL 2902,1552 + 551,144
0.874/FL 370FAR 23 pending;FAR 23 runwayperformance;
1,000-nm missionflown w/3 pax. Alldata preliminary.
Adam AircraftA700
$2,400,000 1+5/744.63.17
NA/NA/NA40.99.644.0
11.9/9.04.2
4.5/NANA/NA30/NA
2 Wms IntlFJ33-4A
1,200/ISA+7°C3,500t7,6507,6007,4007,000c4,8602,1402,7901,0002,345445650
1,7900.700
FL 280/2608.5
3,4005,4887,6001,25510296
2,31625/FL 370
850500
41,00041,00029,00021,500
357615
FL 4100.580387851
FL 3500.455912344
1,9240.474/FL 410
1,333359
2,6150.510/FL 410
1,231353
2,4650.499/FL 410
1,373365
2,6410.520/FL 410
NA1 + 00623
0.482/FL 350NA
1 + 54965
0.622/FL 390NA
3 + 061,441
0.694/FL 410FAR 23 pending
All datapreliminary.
CessnaCitation Mustang
CE-510$2,538,000
1+5/5NANA
NA/NA/NA40.613.443.2
9.8/9.84.5
4.6/NA6/98
57/6202 P&WCPW615F
1,350/ISA+10°C3,500t
NANANANAcNANANA
1,000NA600NANA
0.630FL 271/250
8.33,120
NANANANANANA
23/FL 370NANA
41,000NANA
22,027298424
FL 4100.703340633
FL 3500.537726300
1,3500.538/FL 410
1,158309
2,0030.578/FL 410
1,002307
1,7680.567/FL 410
1,201316
2,0280.592/FL 410
NA0 + 58709
0.423/FL 350NA
1 + 551,173
0.512/FL 390NA
3 + 161,765
0.567/FL 410FAR 23 pending
All datapreliminary.
JETS LESS THAN 10,000 LB MTOW
130 Business & Commercial Aviation n May 2006 www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length: OA/Net
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb. ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TOFL (SL elev., ISA temp.)Performance TOFL (5,000’ @ 25
0C)
Hot/High Weight LimitNBAA IFR RANGE
V2 @SL ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeNBAA IFR 300 nm RunwayMissions Flight Time(4 pax) Fuel Used
Specific Range/Altitude600 nm Runway
Flight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
CessnaCJ1+
CE-525$4,241,000
1+7/744.62.72
73.5/85.2/88.542.613.846.9
11.0/11.04.8
4.8/3.10/0
45/7252 Wms IntlFJ44-1AP
1,965/ISA+7°C3,500t10,80010,7009,9008,400c6,9651,4353,8351,4003,220615
2,4002,4350.710
FL 305/2638.5
3,2505,89010,7001,195111101
2,34721/FL 370
596322
41,00041,00021,20022,027
323532
FL 4100.607384858
FL 3500.448779344
1,6750.465/FL 410
1,300353
2,5690.506/FL 410
1,173352
2,3510.499/FL 410
1,346359
2,6040.517/FL 410
2,5940 + 53847
0.354/FL 3502,6701 + 411,371
0.438/FL 3903,0502 + 512,035
0.491/FL 410FAR 23, 1992/00/05
CessnaCJ2+
CE-525A$5,745,000
1+8/947.42.51
75.5/86.1/89.747.714.049.8
13.6/13.64.8
4.8/3.10/0
65/1,0002 Wms IntlFJ44-3A-24
2,490/ISA+7°C4,000t12,62512,50011,5259,700c7,9251,7754,7001,6003,930770
2,9253,1000.737
FL 291/2788.9
3,3605,18012,5001,597116101
2,64015/FL 370
611316
45,00045,00023,80023,586
356585
FL 4500.609413
1,096FL 3500.377995368
2,0750.480/FL 450
1,613379
3,1570.511/FL 450
1,574378
3,0890.510/FL 450
1,655386
3,1870.519/FL 450
2,4460 + 49897
0.334/FL 3702,6741 + 351,458
0.412/FL 4102,9482 + 362,158
0.463/FL 430FAR 23, 2000/05
BeechcraftPremier IAModel 390$6,057,240
1+6/750.62.72
78.3/87.9/92.046.015.344.5
13.5/11.25.4
5.5/3.723/21054/550
2 Wms IntlFJ44-2A
2,300/ISA+13°C3,500t12,59012,50011,60010,000c8,5501,4504,0401,2003,670370
2,5902,8400.800
FL 280/3208.4
3,7926,88812,5001,178118112
2,99717/FL 370
586298
41,00041,00028,00021,400
369662
FL 4100.557451
1,203FL 3300.375787390
1,8240.431/FL 410
1,360408
2,9340.464/FL 410
1,131402
2,4930.454/FL 410
1,347410
2,8930.466/FL 410
2,9370 + 48898
0.334/FL 3703,2021 + 331,432
0.419/FL 4103,6422 + 302,229
0.449/FL 410FAR 23 A 52, 2001
BOW includes 110-lboptions.
CessnaCitation Bravo
CE-550$6,145,000
2+7/845.82.56
73.7/85.2/91.247.315.051.7
15.8/15.84.8
4.8/3.228/30045/8502 P&WCPW530A
2,887/ISA+8°C4,000t15,00014,80013,50011,300c9,5001,8005,5001,4004,824676
3,7004,1000.700
FL 279/2758.9
3,6005,52014,8001,508121102
2,51719/FL 370
845419
45,00043,00027,75023,586
342607
FL 4500.563399
1,135FL 3500.352907336
2,3380.388/FL 450
1,614345
3,6030.448/FL 450
1,495344
3,3930.441/FL 450
1,698347
3,6330.467/FL 450
2,8580 + 531,086
0.276/FL 3703,0361 + 421,713
0.350/FL 4103,2782 + 492,495
0.401/FL 430FAR 25, 1978/97
Sino SwearingenSJ30-2SJ30-2
$6,195,000 1+5/673.23.03
78.5/86.2/91.846.814.242.3
12.5/12.54.4
4.8/2.86/10053/500
2 Wms IntlFJ44-2A
2,300/ISA+7°C3,500t14,05013,95012,72510,500c8,6501,8505,4001,0004,850550
3,5504,4000.830
FL 295/32012.03,9398,78413,1251,915110100
2,55516/FL 370
312170
49,00044,00025,80041,000
436684
FL 4500.637475
1,188FL 3600.4001,445428
2,7150.532/FL 450
2,503415
4,1330.606/FL 450
2,220422
3,8550.576/FL 450
2,550425
4,1950.608/FL 470
2,9500 + 46745
0.403/FL 4102,9501 + 281,205
0.498/FL 4502,9402 + 221,865
0.536/FL 450FAR 23 Commuter
categoryAll data preliminary.
JETS LESS THAN 20,000 LB MTOW
B u s i n e s s A i r p l a n e s
Business & Commercial Aviation n May 2006 131www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length: OA/Net
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb. ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TOFL (SL elev., ISA temp.)Performance TOFL (5,000’ @ 25
0C)
Hot/High Weight LimitNBAA IFR RANGE
V2 @SL ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeNBAA IFR 300 nm RunwayMissions Flight Time(4 pax) Fuel Used
Specific Range/Altitude600 nm Runway
Flight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
CessnaCJ3
CE-525B$6,652,000
2+6/847.22.46
74.0/88.8/88.650.215.253.3
15.7/15.74.8
4.8/3.14/100
65/1,0002 Wms Intl
FJ44-3A2,820/ISA+7°C
4,000t14,07013,87012,75010,510c8,7001,8105,3701,2004,710660
3,5604,1700.737
FL 293/2788.9
3,1804,75013,8701,76111498
2,41115/FL 370
800425
45,00045,00026,25023,586
351618
FL 4500.568415
1,198FL 3500.3461,174369
2,5760.456/FL 450
1,875378
3,8800.483/FL 450
1,740377
3,6300.479/FL 450
1,916381
3,9000.491/FL 450
2,6060 + 49968
0.310/FL 3702,6121 + 341,569
0.382/FL 4102,7542 + 372,313
0.432/FL 430FAR 23, 2004
Commuter category
GrobSPn Utilijet
G180$6,960,000
1+8/951.62.46
NA/NA/NA48.616.848.9
16.7/16.75.4
5.0/4.15/10037/331
2 Wms IntlFJ44-3A
2,820/ISA+11°C4,000t14,00013,88913,44810,430c7,9392,4916,0611,6004,5751,4863,5704,4610.700
FL 284/2728.3
3,0004,42413,3141,96710087
2,56013/FL 370
750450
41,00041,00028,30021,300
364671
FL 4100.542407
1,029FL 3300.3961,333352
2,8490.468/FL 410
1,897355
3,8720.490/FL 410
1,946351
3,8880.501/FL 410
2,028343
3,9030.520/FL 410
2,1920 + 49784
0.383/FL 4102,2651 + 341,386
0.433/FL 4102,4512 + 342,192
0.456/FL 410FAR 23 Commutercategory pending
All data preliminary.
Raytheon AircraftHawker 400XP
Model 400A$7,145,000
2+7/967.62.75
89.0/93.7/91.748.413.943.5
15.5/15.54.8
4.9/3.727/41026/4502 P&WCJT15D-5
2,965/ISA+12°C3,600t16,50016,30015,70013,000c10,9502,0505,5501,4004,912638
3,5004,1500.780
FL 260/3209.1
3,9066,311
15,830p1,197116105
2,96018/FL 370
305158
45,00043,45020,60024,000
414938
FL 4300.441450
1,255FL 3900.359750378
2,1330.352/FL 430
1,433394
3,7500.382/FL 430
1,351393
3,4570.391/FL 430
1,561394
3,7860.412/FL 450
2,9040 + 461,098
0.273/FL 3703,1541 + 271,859
0.323/FL 4103,5702 + 242,767
0.361/FL 430FAR 25, 1981/85
CessnaCitation Encore+
CE-560$8,068,000
2+7/1152.22.48
70.0/89.8/90.548.915.254.8
17.3/17.34.8
4.8/3.228/65543/8102 P&WCPW535B
3,400/ISA+12°C5,000t17,03016,83015,20012,600c10,5002,1006,5301,4005,4001,1304,4305,1300.755
FL 289/2928.9
3,5905,94016,8301,69411699
2,42613/FL 370
858444
45,00045,000
NA23,586
376804
FL 4500.468426
1,335FL 3700.3191,152372
3,0390.379/FL 450
1,652381
4,1380.399/FL 450
1,672384
4,1500.403/FL 450
1,727393
4,1900.412/FL 450
2,8900 + 491,076
0.279/FL 3902,9561 + 311,830
0.328/FL 4103,0472 + 312,715
0.368/FL 430FAR 25, 1988/94/00
pendingAll data preliminary.
JETS LESS THAN 20,000 LB MTOW
132 Business & Commercial Aviation n May 2006 www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length (OA/Net)
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TOFL (SL elev., ISA temp.)Performance TOFL (5,000’ @25
0C)
Hot/High Weight LimitNBAA IFR Range
V2 @ SL ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeMissions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayFlight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
BombardierLearjet 40XR
Model 45$8,750,000
2+6/767.43.00
75.5/85.1/93.455.614.147.8
17.7/17.74.9
5.1/3.115/17050/5002 HON
TFE731-20BR3,500/ISA+25°C
5,000c21,25021,00019,20016,000c13,7152,2857,5351,2005,3752,1605,2505,3750.810
FL 270/3309.4
4,6805,09019,7601,617123112
2,33415/FL 370
389190
51,00045,20028,40025,700
433950
FL 4700.456453
1,079FL 4700.4201,367421
3,7540.364/FL 470
1,484422
4,0140.370/FL 470
1,617422
4,0870.396/FL 470
1,710424
4,1340.414/FL 490
3,3820 + 441,201
0.250/FL 3903,5371 + 231,966
0.305/FL 4303,7222 + 153,101
0.322/FL 430FAR 25 A 77JAR 25 A 13,
1997/03incorporatesSB 40-11-1
CessnaCitation XLSCE-560-XL
$10,716,800 2+9/12
54.62.53
72.7/86.3/92.851.817.256.3
18.5/18.55.7
5.5/3.910/10080/7002 P&WCPW545B
3,991/ISA+13°C5,000t20,40020,20018,70015,100c12,8002,3007,6001,8006,740860
5,3005,8000.750
FL 265/3059.3
3,5605,49020,2001,742118106
2,73915/FL 370
765389
45,00045,00028,60025,230
354862
FL 4500.411431
1,235FL 4100.3491,130387
3,6070.313/FL 450
1,724396
5,1800.333/FL 450
1,722396
5,1750.333/FL 450
1,769402
5,2190.339/FL 450
2,7750 + 461,245
0.241/FL 3902,7841 + 292,094
0.287/FL 4103,0212 + 263,210
0.312/FL 430FAR 25, 1998/04
RE100 APUstandard.
BombardierLearjet 45XR
Model 45$11,149,000
2+8/969.03.07
75.5/85.1/93.457.614.147.8
19.8/19.84.9
5.1/3.115/17050/5002 HON
TFE731-20BR3,500/ISA+25°C
5,000c21,75021,50019,20016,000c13,8902,1107,8601,6006,0621,7985,7506,0620.810
FL 270/3309.4
5,0405,65020,6621,869130113
2,34915/FL 370
585270
51,00044,70027,90025,700
436982
FL 4700.444450
1,074FL 4700.4191,557423
4,2540.366/FL 450
1,764424
4,7120.374/FL 470
1,869423
4,7640.392/FL 470
1,971426
4,8110.410/FL 490
3,4050 + 441,206
0.249/FL 3903,5681 + 231,977
0.303/FL 4303,7392 + 153,123
0.320/FL 430FAR 25 A 77JAR 25 A 13
BombardierLearjet 60XR
Model 60$12,900,000
2+7/988.82.55
70.8/83.2/87.758.714.643.8
17.7/15.85.7
5.9/3.924/35024/3002 P&WCPW305A
4,600/ISA+17°C6,000t23,75023,50019,50017,000c14,9852,0158,7651,4007,910855
6,7507,3650.810
FL 270/3309.4
5,4508,520
23,371p2,228147131
3,06113/FL 370
715292
51,00042,40024,50025,700
4231,134FL 4300.373446
1,297FL 4300.3441,742413
5,2610.331/FL 410
2,289415
6,5960.347/FL 410
2,269415
6,5480.347/FL 410
2,389413
6,6420.360/FL 410
3,3600 + 441,194
0.251/FL 3903,5901 + 251,940
0.309/FL 4303,9852 + 193,083
0.324/FL 430FAR 25, 1981/92FAR 25 pending
Pro Line 21std.
Gulfstream Aero.Gulfstream 150
G150$13,500,000
2+7/882.32.95
80.7/91.2/91.956.819.155.6
17.67/17.675.75
5.75/4.6725/TBD
55/1,1002 HON
TFE731-40AR-200G4,420/ISA+13°C
5,000c26,25026,10021,70017,500c15,1002,40011,1501,40010,300
8508,7509,7500.850
FL 293/3308.8
5,0128,12026,1002,977131115
2,42817/FL 370
606278
45,000TBDTBD
23,000430
1,187FL 4300.362470
1,735FL 3700.2712,276420
7,2940.312/FL 430
2,943422
8,9390.329/FL 450
2,950422
8,9420.330/FL 450
3,071422
8,9910.342/FL 450
3,5900 + 491,227
0.244/FL 4503,7571 + 301,977
0.303/FL 4503,9492 + 273,014
0.332/FL 450FAR 25 A108,
2005
Raytheon AircraftHawker 850XPHawker 850XP$13,786,100
2+8/1574.93.00
79.3/87.1/93.351.118.154.3
21.3/21.35.7
6.0/4.450/395—/—2 HON
TFE731-5BR4,660/ISA+10°C
4,200c28,12028,00023,35018,450c16,3302,12011,7901,60010,0001,7909,67010,0000.800
FL 290/3108.6
5,0327,95227,0492,676140113
2,24519/FL 370
354152
41,00039,00018,80022,200
4021,168FL 3900.344448
1,826FL 3700.2452,394390
7,9590.301/FL 410
2,522391
8,3450.302/FL 410
2,642391
8,3950.315/FL 410
2,698393
8,4340.320/FL 390
3,7630 + 481,472
0.204/FL 3703,8521 + 282,720
0.221/FL 3703,9742 + 224,387
0.228/FL 370CAR 4b, 1963;FAR 25 Amend1984/95/06
Pro Line 21 std.36-150 APU.
JETS 20,000 LB MTOW OR GREATER
B u s i n e s s A i r p l a n e s
Business & Commercial Aviation n May 2006 133www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length (OA/Net)
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TOFL (SL elev., ISA temp.)Performance TOFL (5,000’ @25
0C)
Hot/High Weight LimitNBAA IFR Range
V2 @ SL ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeMissions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayFlight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
CessnaCitation Sovereign
CE-680$15,479,000
2+9/1258.22.63
71.5/87.6/91.363.520.363.3
25.3/25.35.7
5.5/3.935/415
100/1,0002 P&WCPW306C
5,770/ISA+18°C6,000t30,55030,30027,10020,450c18,1502,30012,4001,80011,2161,18410,10010,6000.800
FL 298/3059.3
3,6404,95030,0002,90311595
2,20214/FL 370
617322
47,00043,00027,56025,230
3871,133FL 4700.342446
1,738FL 3900.2572,405404
8,3270.289/FL 470
2,847406
9,5640.298/FL 470
2,881406
9,5760.301/FL 470
2,960407
9,6080.308/FL 470
3,0580 + 451,488
0.202/FL 3903,0681 + 272,399
0.250/FL 4303,0932 + 223,750
0.267/FL 430FAR 25, 2004;JAR 25, 2005
EmbraerLegacy Shuttle
EMB-135LR$17,800,000
2+16/3780.03.12
79.7/84.5/92.386.422.265.8
53.4/42.46.0
6.9/5.242/551
325/2,2052 RR
AE 3007 A1/37,057/ISA+30°C
OC44,31244,09240,78535,274c25,3539,92118,9593,20011,3217,6389,03811,3210.780
FL 276/3207.8
5,6007,02444,0922,049129106
2,05722/FL 370
301140
37,00037,00022,33119,493
4241,931FL 3700.220446
2,122FL 3700.2101,167393
6,6620.175/FL 370
1,658402
9,0390.183/FL 370
1,893407
9,4360.201/FL 370
1,918408
9,4690.203/FL 370
3,4580 + 531,916
0.157/FL 3703,4681 + 353,288
0.182/FL 3703,4972 + 325,147
0.194/FL 370RBHA/FAR/JAR
25, 1999Equipment levelexceeds B&CA
MEL.
BombardierChallenger 300BD-100-1A10$19,210,000
2+8/1374.42.85
75.3/87.6/89.668.620.063.8
28.6/16.56.1
7.2/5.1106/750
—/—2 HON
HTF 70006,826/ISA+15°C
OC39,00038,85033,75027,000c23,5003,50015,5001,60014,0451,45512,00013,9000.830
FL 290/3208.8
4,7206,86038,3453,276130113
2,29014/FL 370
473219
45,00044,00027,80023,500
4591,577FL 4500.291470
1,794FL 4300.2622,544446
9,9350.256/FL 450
3,291449
12,2200.269/FL 450
3,291449
12,2200.269/FL 450
3,335451
12,2310.273/FL 450
3,3700 + 471,570
0.191/FL 4503,3991 + 262,554
0.235/FL 4503,4722 + 183,889
0.257/FL 450FAR 25 A 98 and JAR 25 Chg 15
Raytheon AircraftHawker 4000Model 4000$19,557,000
2+8/1470.62.72
NA/NA/NA69.219.661.8
29.5/25.06.0
6.5/4.0115/NA—/—
2 P&WCPW308A
6,900/ISA+20°C6,000t37,70037,50033,50025,000c22,4752,52515,2251,60014,600
62512,70013,6250.840
FL 200/3509.6
4,5096,72037,5003,362134107
2,49013/FL 370
602270
45,00042,90028,00025,240
4301,453FL 4500.296470
1,790FL 4100.2632,775422
10,7270.259/FL 450
3,400422
12,6830.268/FL 450
3,341423
12,5030.267/FL 450
3,466423
12,7010.273/FL 450
2,6390 + 481,520
0.197/FL 4502,6951 + 262,542
0.236/FL 4502,8472 + 173,940
0.254/FL 450FAR/JAR 25
2005
CessnaCitation X
CE-750$20,062,000
2+8/1168.52.67
73.2/83.8/90.372.319.363.9
23.9/23.95.7
5.5/3.9variable/variable
82/7752 RR
AE3007C16,764/ISA+15°C
4,500*t36,40036,10031,80024,400c22,1002,30014,3001,60012,9311,36912,00012,7000.920
FL 307/3509.3
5,1407,350
34,980p2,980137112
2,73018/FL 370
486213
51,00043,00026,00025,230
4701,529FL 4700.307513
2,229FL 4100.2302,703462
9,9730.271/FL 470
3,070462
11,0550.278/FL 490
3,125463
11,0780.282/FL 490
3,221463
11,1180.290/FL 490
3,5360 + 411,837
0.163/FL 3703,5801 + 162,855
0.210/FL 4303,6722 + 034,469
0.224/FL 430FAR 25, 1996/02JAR 25, 1999/02*Engine flight hour
inspection.
DassaultFalcon 50EX
DA50$21,150,000
2+9/1979.83.58
83.8/95.2/93.160.822.961.8
28.0/23.55.9
6.1/5.2—/—
115/2,2003 HON
TFE731-403,700/ISA+17°C
6,000c39,90039,70035,71525,570c22,2503,32017,6501,80015,5202,13014,33015,5200.860
FL 240/3709.2
4,9357,24738,5703,382123106
2,15917/FL 370
671322
49,00041,90031,90023,000
4171,586FL 4300.263481
2,533FL 3900.1902,868410
12,3080.233/FL 450
3,249410
13,5900.239/FL 470
3,350411
13,5900.247/FL 470
3,428412
13,5900.252/FL 470
2,8530 + 471,607
0.187/FL 4502,9591 + 272,705
0.222/FL 4503,0052 + 214,232
0.236/FL 450FAR 25,
1977/79/96Optional
40,780-lb MTOW.
JETS 20,000 LB MTOW OR GREATER
136 Business & Commercial Aviation n May 2006 www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length (OA/Net)
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TOFL (SL elev., ISA temp.)Performance TOFL (5,000’ @25
0C)
Hot/High Weight LimitNBAA IFR Range
V2 @ SL ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeMissions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayFlight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
Gulfstream Aero.Gulfstream 200
G200$21,646,000
2+10/1896.12.93
81.7/85.8/92.762.321.458.1
24.4/24.46.3
7.2/5.725/367
125/1,9802 P&WCPW306A
6,040/ISA+17°C6,000c35,60035,45030,00024,000c20,2003,80015,4002,00015,000
40011,60013,4000.850
FL 245/3608.8
6,0838,804
33,255p2,845150121
2,59019/FL 370
395158
45,00039,61223,72023,000
4301,555FL 4100.277470
2,065FL 3700.2282,371421
9,8510.241/FL 410
3,444423
13,3880.257/FL 430
3,312423
12,9740.255/FL 410
3,493423
13,4010.261/FL 430
3,8500 + 481,361
0.220/FL 4303,9001 + 302,340
0.256/FL 4303,9652 + 263,695
0.271/FL 430FAR 25 A82, 1998
Optional35,600-lb MTOW.
EmbraerLegacy Executive
EMB-135BJ$23,600,000
2+13/1690.03.11
79.7/86.8/91.386.422.268.9
49.8/42.46.0
6.9/5.2240/1,000
—/—2 RR
AE 3007 A1E7,987/ISA+22°C
OC49,75849,60440,78535,274c30,1485,12619,6102,60018,1701,44014,48417,0100.800
FL 276/3208.4
5,4537,38549,1193,432139113
2,30621/FL 370
619267
41,00039,80023,54821,653
4241,874FL 4100.226447
2,240FL 3900.2002,450413
12,3000.199/FL 410
3,361419
16,1160.209/FL 410
3,403419
16,1380.211/FL 410
3,455419
16,1670.214/FL 410
3,4550 + 531,944
0.154/FL 4103,4971 + 353,225
0.186/FL 4103,5602 + 295,056
0.198/FL 410RBHA/FAR/JAR
25, 1999quipment levelexceeds B&CA
MEL.
BombardierChallenger 850 CS
CL-600-2B19$24,530,000
2+27/5094.63.04
78.6/82.4/92.187.820.469.6
48.4/43.36.1
8.2/7.2296/2,700
—/—2 GE
CF34-3B18,729/ISA+8°C
OC53,25053,00047,00044,000c32,25711,74320,9935,40014,3056,6889,25014,3050.850
FL 254/3358.3
6,3057,43347,1122,477146122
2,36626/FL 370
572235
41,00037,76019,37021,100
4261,826FL 4100.233460
2,170FL 3900.2121,116402
6,7590.165/FL 370
2,186413
11,9980.182/FL 390
2,477415
12,2130.203/FL 410
2,521415
12,2420.206/FL 410
3,0590 + 492,062
0.145/FL 4103,2851 + 303,386
0.177/FL 4103,5972 + 255,196
0.192/FL 410FAR/JAR 25, 1992Corporate shuttle;baggage volume is
flexible. Opt’lISA+15°C
engine flat rating.
DassaultFalcon 2000DX
DA2000EX$25,550,000
2+8/1978.32.93
79.5/91.7/91.066.323.263.4
31.2/26.36.2
7.7/6.3131/1,600
—/—2 P&WCPW308C
7,000/ISA+15°C7,000c41,20041,00039,30029,700c24,0005,70017,2001,60014,6002,60011,50014,6000.860
FL 250/3709.3
5,3007,53539,2833,458135113
2,64015/FL 370
643286
47,00043,000
NA25,300
4181,441FL 4300.290482
2,306FL 3900.2092,311416
9,5670.242/FL 450
3,270419
12,7500.256/FL 470
3,425419
12,7500.269/FL 470
3,508418
12,7500.275/FL 470
3,2000 + 481,527
0.196/FL 4503,2231 + 272,498
0.240/FL 4503,3672 + 213,836
0.261/FL 450FAR/EASA 25
pendingAll data
preliminary.
BombardierChallenger 605
$26,714,000 2+9/19
97.92.76
81.2/86.2/90.368.420.764.3
28.4/25.56.1
8.2/7.2115/900
—/—2 GE
CF34-3B8,729/ISA+15°C
OC48,30048,20038,00032,000c26,9855,01521,3151,80019,8501,46516,30019,5150.850
FL 222/3489.2
5,6849,12347,5354,035147117
2,36421/FL 370
680278
41,00038,25020,00023,200
4371,891FL 4100.231470
2,437FL 3700.1933,010416
14,2550.211/FL 410
3,975419
17,9380.222/FL 410
4,035419
17,9620.225/FL 410
4,109419
17,9920.228/FL 410
3,3840 + 471,589
0.189/FL 4103,4121 + 272,823
0.213/FL 4103,4682 + 194,510
0.222/FL 410FAR 25,
1980/83/87/95pending
DassaultFalcon 2000EX
DA2000EX$27,200,000
2+8/1978.33.01
80.7/91.7/91.066.323.263.4
31.2/26.36.2
7.7/6.3131/1,600
—/—2 P&WCPW308C
7,000/ISA+15°C7,000c42,40042,20039,30029,700c24,0005,70018,4001,60016,6601,74012,70016,6600.860
FL 250/3709.3
5,5858,12041,3433,944136113
2,64016/FL 370
643286
47,00043,000
NA25,300
4221,496FL 4300.282482
2,351FL 3900.2052,579418
10,7670.240/FL 450
3,823419
14,8100.258/FL 470
3,912419
14,8100.264/FL 470
4,000419
14,8100.270/FL 470
3,2000 + 481,527
0.196/FL 4503,2231 + 272,498
0.240/FL 4503,3672 + 213,836
0.261/FL 450FAR 25, 2003
JETS 20,000 LB MTOW OR GREATER
B u s i n e s s A i r p l a n e s
Business & Commercial Aviation n May 2006 137www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length (OA/Net)
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TOFL (SL elev., ISA temp.)Performance TOFL (5,000’ @25
0C)
Hot/High Weight LimitNBAA IFR Range
V2 @ SL ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeMissions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayFlight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
BombardierChallenger 850 ER
CL-600-2B19$28,950,000
2+15/1994.63.04
78.6/82.2/92.187.820.469.6
48.4/40.26.1
8.2/7.2202/900
—/—2 GE
CF34-3B18,729/ISA+8°C
OC53,25053,00047,00044,000c34,1679,83319,0833,00018,305
7789,25016,0830.850
FL 254/3358.3
6,30511,34453,000p3,091146125
2,45829/FL 370
501206
41,00037,76019,37021,100
4261,968FL 4100.216459
2,187FL 4100.2101,116402
6,7590.165/FL 370
3,096416
16,1430.192/FL 390
3,091416
16,1200.192/FL 390
3,141417
16,1720.194/FL 390
3,4300 + 502,103
0.143/FL 4103,6431 + 313,480
0.172/FL 4103,9752 + 255,389
0.186/FL 410FAR/JAR 25, 1992
Exec. config.;baggage volume isflexible. OptionalISA+15°C engine
flat rating.
Gulfstream Aero.Gulfstream 350
GIV-X$29,500,000
2+14/1974.62.56
74.1/89.7/92.389.325.277.8
45.1/37.06.2
7.3/5.5169/2,000
—/—2 RR
Tay Mk 611-8C13,850/ISA+15°C
12,000 or OCt71,30070,90066,00049,000c42,7006,30028,6002,80025,8072,79322,30025,8000.880
FL 280/3409.6
5,0507,21270,9003,890146122
2,64015/FL 370
790323
45,00043,20026,00026,700
4592,510FL 4500.183476
2,969FL 4100.1603,008450
19,0970.158/FL 450
3,726453
22,7630.164/FL 450
3,848453
22,8550.168/FL 450
3,898453
22,8910.170/FL 450
3,2070 + 462,595
0.116/FL 4503,2401 + 254,102
0.146/FL 4503,2872 + 186,158
0.162/FL 450FAR 25, 2004
BombardierChallenger 870 CS
CL-600-2C10$29,650,000
4+42/70101.52.96
82.7/89.4/92.6106.124.876.3
68.1/59.26.2
8.3/7.2439/4,305
—/—2 GE
CF34-8C512,670/ISA+15°C
OC75,25075,00067,00062,300c44,90717,39330,3438,40019,45010,89312,95019,4500.850
FL 254/3358.6
5,5626,26764,9072,502138125
4,46218/FL 370
425185
41,00038,10021,40021,100
4472,661FL 4100.168471
2,886FL 4100.1631,138418
9,2700.123/FL 390
2,157432
16,0170.135/FL 390
2,503435
16,3660.153/FL 410
2,528435
16,3920.154/FL 410
3,7040 + 482,683
0.112/FL 4103,7441 + 294,450
0.135/FL 4103,8002 + 236,836
0.146/FL 410FAR/JAR 25,1980/2002
Corporate shuttle;baggage volume is
flexible.
DassaultFalcon 900DX
DA900EX$32,750,000
2+12/1988.53.11
79.7/90.5/92.366.324.863.4
39.0/33.26.2
7.7/6.3127/2,866
—/—3 HON
TFE731-605,000/ISA+17°C
6,000c46,90046,70042,20030,865c25,8005,06521,1002,40018,8302,27016,03518,7000.870
FL 250/3709.3
4,8906,91045,4304,088131109
2,39717/FL 370
796365
51,00040,60031,60025,300
4351,738FL 4300.250474
2,198FL 3900.2163,405421
15,5300.219/FL 450
3,912421
16,8100.233/FL 470
4,057422
16,8100.241/FL 470
4,143422
16,8100.246/FL 470
2,7000 + 471,607
0.187/FL 4502,7821 + 272,675
0.224/FL 4502,7952 + 204,150
0.241/FL 450FAR 25,
1979/91/99
BombardierChallenger 890 CS
CL-600-2D24$33,950,000
4+52/90114.43.22
83.4/89.4/92.6118.924.881.6
80.9/71.86.2
8.3/7.2486/5,005
—/—2 GE
CF34-8C513,123/ISA+15°C
OC85,00084,50075,00070,600c48,26222,33836,73810,40019,45017,28814,40019,4500.850
FL 254/3358.6
6,8086,46568,2622,356150121
4,51126/FL 370
410164
41,00037,80018,10021,100
4472,819FL 4100.159471
3,152FL 4100.1491,118418
10,0890.111/FL 370
1,823428
15,3400.119/FL 390
2,356435
16,2000.145/FL 410
2,381435
16,2280.147/FL 410
4,1960 + 482,822
0.106/FL 4104,1961 + 294,668
0.129/FL 4104,1962 + 237,174
0.139/FL 410FAR/JAR 25,1980/2004
Optional 89,700-lbMTOW.
Optional BEVS.
Gulfstream Aero.Gulfstream 450
GIV-X$34,170,000
2+14/1977.82.67
75.8/89.5/92.589.325.277.8
45.1/37.06.2
7.3/5.5169/2,000
—/—2 RR
Tay Mk 611-8C13,850/ISA+15°C
12,000t or OC74,30073,90066,00049,000c43,0006,00031,3002,80029,2812,01925,30028,5000.880
FL 280/3409.6
5,4507,88673,9004,385149122
2,65016/FL 370
712285
45,00042,40025,00026,700
4592,585FL 4500.178476
3,055FL 4100.1563,463452
22,0970.157/FL 450
4,281453
26,2590.163/FL 450
4,363453
26,3150.166/FL 450
4,419453
26,3510.168/FL 450
3,2140 + 462,603
0.115/FL 4503,2481 + 254,116
0.146/FL 4503,2942 + 186,180
0.162/FL 450FAR 25, 2004
JETS 20,000 LB MTOW OR GREATER
138 Business & Commercial Aviation n May 2006 www.AviationNow.com/BCA
B u s i n e s s A i r p l a n e s
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length (OA/Net)
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TOFL (SL elev., ISA temp.)Performance TOFL (5,000’ @25
0C)
Hot/High Weight LimitNBAA IFR Range
V2 @ SL ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeMissions 300 nm Runway(4 pax) Flight Time
Fuel UsedSpecific Range/Altitude
600 nm RunwayFlight TimeFuel Used
Specific Range/Altitude1,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
DassaultFalcon 900EX
DA900EX$36,150,000
2+12/1991.63.22
79.8/90.5/92.366.324.863.4
39.0/33.26.2
7.7/6.3127/2,866
—/—3 HON
TFE731-605,000/ISA+17°C
6,000c48,50048,30042,00030,865c26,0294,83622,4712,40021,0001,47117,63520,0710.870
FL 250/3709.3
5,2137,21447,8294,501133110
2,41118/FL 370
755340
51,00040,10031,40025,300
4361,809FL 4300.241474
2,268FL 3900.2093,405421
15,5300.219/FL 450
4,404422
18,9800.232/FL 470
4,469422
18,9800.235/FL 470
4,562422
18,9800.240/FL 470
2,7000 + 471,614
0.186/FL 4502,7841 + 272,688
0.223/FL 4502,7962 + 204,173
0.240/FL 450FAR 25
1979/91/96Optional 49,000-lb
MTOW. Priceincludes EASy
cockpit.
BombardierGlobal 5000BD-700-1A11$36,750,000
3+8/1785.82.97
79.9/89.1/89.796.825.594.0
42.5/37.36.3
8.2/6.9195/1,000
—/—2 RR
BR700-710A2-2014,750/ISA+20°C
OC87,95087,70078,60056,000c50,8305,17037,1201,60035,7331,38731,95035,5200.890
FL 303/34010.35,0006,65087,7004,800130107
2,18018/FL 370
651300
51,00044,60020,60026,500
4702,836FL 4500.166499
3,664FL 4300.1364,150477
28,6180.145/FL 470
4,858479
32,5260.149/FL 470
4,876479
32,5350.150/FL 470
4,921479
32,5600.151/FL 470
2,4950 + 462,755
0.109/FL 4902,5841 + 234,441
0.135/FL 4902,7062 + 136,746
0.148/FL 490FAR 25, 1998/04EASA 25, 2004
Optional 89,700-lbMTOW. Optional
BEVS.
Gulfstream Aero.Gulfstream 500
GV-SP$38,760,000
2+16/1974.92.77
77.6/90.5/90.896.425.893.5
50.1/42.66.2
7.3/5.5226/2,500
—/—2 RR
BR700-710C4-1115,385/ISA+15°C
OC85,50085,10075,30054,500c48,0006,50037,5003,20034,9392,56131,00034,3000.885
FL 270/34010.25,1507,68085,1005,969141111
2,22016/FL 370
707301
51,00044,00027,70029,200
4592,425FL 4500.189488
3,021FL 4300.1624,893451
28,0930.174/FL 490
5,788453
32,1420.180/FL 490
5,941453
32,1930.185/FL 490
6,009453
32,2160.187/FL 490
3,3660 + 472,380
0.126/FL 4503,3881 + 273,700
0.162/FL 5103,4132 + 205,511
0.181/FL 510FAR 25, 2002
DassaultFalcon 7X
DA7X$39,200,000
2+12/1983.73.48
TBD/TBD/TBD76.125.682.6
46.0/39.16.2
7.7/6.3140/NA—/—
3 P&WCPW307A
6,100/ISA+17°C7,200c63,90063,70060,50039,100c33,1006,00030,8002,40028,9001,90024,80028,4000.900
NA/37010.25,200
NANA
5,700134104
2,300NANANA
51,000NANA
29,200NANANANANANANANANANANANANANANANA
5,820460
26,4910.220/FL 490
NANANANA
2,7600 + 461,902
0.158/FL 4102,7541 + 262,912
0.206/CL 4902,7502 + 194,374
0.229/FL 490FAR/EASA 25
pendingAll data
preliminary.
AirbusElite
A318-112$45,000,000
4+18/18107.73.05
83.0/91.9/93.9103.242.1111.8
NA/70.27.4
12.2/11.6NA/NANA/NA2 CFMI
CFM56-5B9/P23,300/ISA+15°C
OC143,080142,197126,765120,151c93,70026,45149,3803,60045,7613,61922,92945,7610.820
FL 250/3508.2
5,1506,370
142,2003,800129NANANANANA
39,800NANANA447NANANA469NANANANANANANANANANANANANANANANANANANANANANANANANANANANA
2 + 32NANA
FAR 25 2003*Also avail. withPW6124 enginesand opt’l. 3,540-lb
capacity ACT.
BoeingBBJ3
737-900ER$77,500,000 4+19/215
139.93.44
NA/NA/NA138.241.2117.4
107.2/107.27.1
11.6/10.7NA/NA
1,250/NA2 CFMI
CFM56-7B2727,300/ISA+15°C
OC188,200187,700157,300149,300c110,50038,80077,7003,80063,00714,69338,90063,0070.820
FL 260/3409.0
7,00012,840174,8574,761
NA121
2,47526/FL 370
NANA
41,00035,000
NA18,500
4555,278FL 3700.086470
6,103FL 3700.0772,190436
31,9200.069/FL 350
4,324445
56,8000.076/FL 390
4,736446
57,4400.082/FL 410
4,789446
57,4900.083/FL 410
NA0 + 493,700
0.081/FL 410NA
1 + 297,300
0.082/FL 4104,0652 + 2512,020
0.083/FL 410FAR 25 A 77
pending2008 dollars. Alldata preliminary.300 & 600 nm
missions B&CA est.
JETS 20,000 LB MTOW OR GREATER
140 Business & Commercial Aviation n May 2006 www.AviationNow.com/BCA
ManufacturerModel
B&CA Equipped PriceCharacteristics Seating
Wing LoadingPower Loading
Noise (EPNdB): TO/Sideline/APRDimensions External Length(ft) Height
SpanInternal Length: OA/Net
HeightWidth: Max/Floor
Baggage Internal Cu. ft/lbExternal Cu. ft/lb
Power Engines
Output (lb ea.)/Flat RatingInspection Interval
Weights (lb) Max RampMax TakeoffMax Landing
Zero FuelBOW
Max PayloadUseful Load
Executive PayloadMax Fuel
Available Payload w/Max FuelAvailable Fuel w/Max Payload
Available Fuel w/Exec. PayloadLimits MMO
Trans. Alt. FL/VMOPSI
Airport TO (SL elev.; ISA)Performance TO (5,000’ elev. @ 25
0C)
Hot/High Weight LimitNBAA IFR Range
V2 @ SL, ISA, MTOWVREF w/4 Pax, NBAA IFR Res.
Landing Distance w/4 Pax, NBAA IFR Res.Climb Time to Climb/Altitude
FAR 25 Engine-Out Rate (fpm)FAR 25 Engine-Out Gradient (ft/nm)
Ceilings (ft) CertificatedAll-Engine Service
Engine-Out ServiceSea-Level Cabin
Cruise Long TASRange Fuel Flow
AltitudeSpecific Range
High TASSpeed Fuel Flow
AltitudeSpecific Range
NBAA IFR Max Nautical MilesRanges Payload Average Speed(200-nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude
Max Fuel Nautical Miles(w/avail. Average Speedpayload) Trip Fuel
Specific Range/AltitudeEight Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel
Specific Range/AltitudeFerry Nautical Miles
Average SpeedTrip Fuel
Specific Range/AltitudeNBAA IFR 1,000 nm RunwayMissions Flight Time(8 Pax) Fuel Used
Specific Range/Altitude3,000 nm Runway
Flight TimeFuel Used
Specific Range/Altitude6,000 nm Runway
Flight TimeFuel Used
Specific Range/AltitudeRemarks Certification Basis
Gulfstream Aero.Gulfstream 550
GV-SP$46,665,000
4+16/1980.12.96
79.3/90.2/90.896.425.893.5
50.1/42.66.2
7.3/5.5226/2,500
—/—2 RR
BR700-710C4-1115,385/ISA+15°C
OC91,40091,00075,30054,500c48,7005,80042,7003,20040,9941,70636,90039,5000.885
FL 270/34010.25,9109,07091,0006,738147112
2,24018/FL 370
594242
51,00042,70025,82029,200
4592,563FL 4500.179488
3,021FL 4300.1625,767452
33,9930.170/FL 490
6,698454
38,2020.175/FL 490
6,708453
38,2050.176/FL 490
6,862451
38,1100.180/FL 510
3,4362 + 205,599
0.179/FL 4903,5996 + 4215,474
0.194/FL 4905,277
13 + 1533,428
0.179/FL 490FAR 25, 1997/03/02
BombardierGlobal Express XRS
BD-700-1A10$47,750,000
4+8/1795.93.32
83.4/88.4/89.899.425.594.0
48.4/43.26.3
8.2/6.9195/1,000
—/—2 RR
BR700-710A2-2014,750/ISA+20°C
OC98,25098,00078,60056,000c51,2004,80047,0501,60044,6422,40842,25044,6420.890
FL 303/34010.36,1907,880
94,513p5,924136108
2,19620/FL 370
473209
51,00042,40018,00030,125
4702,947FL 4300.159499
3,652FL 4100.1375,575478
38,9550.143/FL 470
6,020479
41,4200.145/FL 490
6,075479
41,4450.147/FL 490
6,185480
41,4930.149/FL 490
2,7562 + 136,676
0.150/FL 4903,6696 + 2018,988
0.158/FL 4906,006
12 + 3140,851
0.147/FL 490FAR 25, 1998/03
JAR 25BEVS standard.
AirbusCorporate Jetliner
A319-133$55,000,000 4+48/134
126.33.14
85.9/91.5/94.3111.038.6111.8
78.0/78.07.4
12.2/11.6NA/NA
NA/4,6872 IAE
V2527M-A5*26,500/ISA+30°C
OC167,380166,447137,787128,969c97,65331,31669,7279,60061,0178,71038,41160,1270.820
FL 250/3508.3
5,9058,900
166,4504,650152111
2,97025/FL 370
770NA
41,00037,20022,00022,000
4474,565FL 3700.098469
5,800FL 3900.0812,625436
33,1610.079/FL 410
5,085435
55,8170.091/FL 410
5,200439
55,8320.093/FL 410
5,250434
55,8670.094/FL 410
3,3002 + 259,975
0.100/FL 4103,9006 + 5428,600
0.105/FL 410NPNPNPNP
FAR 25, 1999*Also available withCFM56-5B7 engines
with 27,000 lbf.
BoeingBBJ1
737-700IGW$57,500,000 4+19/149
127.53.13
85.6/95.2/95.9110.341.2117.4
79.2/79.27.1
11.6/10.7NA/NA150/NA2 CFMI
CFM56-7B2727,300/ISA+15°C
OC171,500171,000134,000126,000c95,96030,04075,5403,80071,7373,80345,50071,7370.820
FL 260/3409.0
5,9509,800
169,0476,123141116
2,33025/FL 370
NANA
41,00038,00020,50018,500
4524,799FL 3900.094470
5,710FL 3700.0823,167435
39,3800.080/FL 370
6,016442
66,7300.090/FL 410
6,098441
66,7800.091/FL 410
6,166441
66,8200.092/FL 410
3,6002 + 2710,610
0.094/FL 4104,2106 + 5530,280
0.099/FL 4105,865
13 + 3665,500
0.092/FL 410FAR 25 A 77,
1967/982007 dollars.
BoeingBBJ2
737-800$69,500,000 4+19/189
129.93.19
86.0/94.7/96.3129.541.2117.4
98.3/98.37.1
11.6/10.7NA/NA750/NA2 CFMI
CFM56-7B2727,300/ISA+15°C
OC174,700174,200146,300138,300c103,22035,08071,4803,80069,9821,49836,40067,6800.820
FL 260/3409.0
6,98512,850174,2005,606152122
2,50527/FL 370
NANA
41,00037,70020,00018,500
4545,084FL 3900.089470
5,937FL 3700.0792,227433
29,8200.075/FL 370
5,620445
64,7400.087/FL 410
5,580445
64,3700.087/FL 410
5,667445
64,7700.087/FL 410
3,6702 + 2611,300
0.088/FL 4104,7906 + 5132,370
0.093/FL 410NPNPNPNP
FAR 25 A 77,1967/98
2007 dollars.
ULTRA-LONG-RANGE JETS
B u s i n e s s A i r p l a n e s