2006 purchase planning handbook - aviation...

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

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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

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112 Business & Commercial Aviation n May 2006

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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

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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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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-





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.

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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.



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

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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




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



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




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


ManufacturerModel




SpanInternal Length

HeightWidth

Power Engine



Zero FuelEOW


Max BaggageMax Fuel


Limits VNE

VNO

VA

Airport TO (SL elev./ISA temp)Performance TO (5,000’ elev. @25

0C)

VSO

VX

VY


Ceiling (ft) ServiceCruise Long TAS



Fuel FlowAltitude








Block TimeFuel Used


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




SINGLE-ENGINE PISTONS TURBOCHARGED

ManufacturerModel




SpanInternal Length

HeightWidth

Power Engine



Zero FuelEOW


Max BaggageMax Fuel


Limits VNE

VNO

VA


0C)

VSO

VX

VY

Climb Time to Climb/AltitudeInitial Gradient (ft/nm)

Ceilings (ft) CertificatedService

Cruise Long TASRange Fuel Flow


Rec’d TASFuel Flow


High TASSpeed Fuel Flow







Block TimeFuel Used


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.


SINGLE-ENGINE PISTONS PRESSURIZED

ManufacturerModel




SpanInternal Length

HeightWidth

Power Engine



Zero FuelEOW


Max BaggageMax Fuel


Limits VNE

VNO

VA

PSIAirport TO (SL elev./ISA temp.)Performance TO (5,000’ elev. @25

0C)

VSO

VX

VY



Sea-level CabinCruise Long TAS



Fuel FlowAltitude








Block TimeFuel Used


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




SpanInternal Length

HeightWidth

Power Engine



Zero FuelEOW


Max BaggageMax Fuel


Limits VNE

VNO

VA


0C)

VSO

VX

VY

Climb Time to Climb/AltitudeInitial Gradient (ft/nm)













Block TimeFuel Used


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.




MULTIENGINE PISTONS TURBOCHARGED

ManufacturerModel




SpanInternal Length

HeightWidth

Power Engines

Output (hp ea.)Inspection Interval


Zero FuelEOW


Executive PayloadMax Fuel

Payload – Max FuelAvailable Fuel w/Max Payload

Available Fuel w/Exec. PayloadLimits VNE

VNO

VA


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







Ranges Exec. Nautical MilesPayload Average Speed

Trip FuelSpecific Range/Altitude

Ferry Nautical MilesAverage Speed




500 nm RunwayBlock Time


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




SpanInternal Length

HeightWidth

Power Engines



Zero FuelEOW





VNO

VA


0C)


0C)

VMCA

VDEC

VXSE

VYSE




Engine-Out ServiceCruise Long TAS



Fuel FlowAltitude












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.


MULTIENGINE PISTONS PRESSURIZED

ManufacturerModel




SpanInternal Length

HeightWidth

Power Engines



Zero FuelEOW





VNO

VA


0C)


0C)

VMCA

VDEC

VXSE

VYSE




Engine-Out ServiceSea Level Cabin
















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




SpanInternal Length

HeightWidth

Power Engine

Output (shp)/Flat RatingInspection Interval


Zero FuelBOW




Available Fuel w/Exec. PayloadLimits VMO

VAPSI


0C)

VSOVXVY







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


600 nm RunwayFlight TimeFuel Used

Specific Range/Altitude1,000 nm Runway

Flight TimeFuel Used


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




SINGLE-ENGINE TURBOPROPSManufacturerModel




SpanInternal Length

HeightWidth

Power Engine

Output (shp)/Flat RatingInspection Interval


Zero FuelBOW





VAPSI


0C)

VSOVXVY







NBAA IFR Exec. Nautical MilesRanges Payload Average Speed(100 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude










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


$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.


ManufacturerModel




SpanInternal Length (OA/Net)

HeightWidth (max)/Width (floor)

Power Engines

Output (shp ea.)/Flat RatingInspection Interval


Zero FuelBOW





VAPSI


0C)

A/S (SL elev./ISA temp.)A/S (5,000’ elev. @ 25

0C)

VMCAVDECVXSEVYSE


Initial All-Engine Gradient (ft/nm)Initial Engine-Out Gradient (ft/nm)


Engine-Out ServiceSea-Level Cabin





NBAA IFR Max Nautical MilesRanges Payload Average Speed(100 nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude


Specific Range/AltitudeFull Fuel Nautical Miles(w/4 pax) Average Speed




Missions 300 nm Runway(4 pax) Flight Time




1,000 nm RunwayFlight TimeFuel Used


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



ManufacturerModel





HeightWidth (max)/Width (floor)

Power Engines

Output (shp ea.)/Flat RatingInspection Interval


Zero FuelBOW




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






Specific Range/AltitudeFull Fuel Nautical Miles(w/4 pax) Average Speed




Missions 300 nm Runway(4 pax) Flight Time






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


ManufacturerModel



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


Zero FuelBOW





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)









Specific Range/AltitudeFour Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel



Specific Range/AltitudeNBAA IFR 300 nm RunwayMissions Flight Time(4 pax) Fuel Used

Specific Range/Altitude600 nm Runway




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


ManufacturerModel







Power Engines



Zero FuelBOW







0C)






















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.




ManufacturerModel







Power Engines



Zero FuelBOW







0C)






















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.



ManufacturerModel







Power Engines

Output (lb ea.)/Flat RatingInspection Interval


Zero FuelBOW






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.




















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.


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


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



ManufacturerModel







Power Engines



Zero FuelBOW







0C)






















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.



ManufacturerModel







Power Engines



Zero FuelBOW







0C)























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




ManufacturerModel







Power Engines



Zero FuelBOW







0C)






















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.


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


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


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.


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




ManufacturerModel







Power Engines



Zero FuelBOW







0C)






















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.


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.



ManufacturerModel







Power Engines



Zero FuelBOW






Airport TO (SL elev.; ISA)Performance TO (5,000’ elev. @ 25

0C)


V2 @ SL, ISA, MTOWVREF w/4 Pax, NBAA IFR Res.









NBAA IFR Max Nautical MilesRanges Payload Average Speed(200-nm (w/avail. fuel) Trip Fuelalternate) Specific Range/Altitude


Specific Range/AltitudeEight Pax Nautical Miles(w/avail. Average Speedfuel) Trip Fuel



Specific Range/AltitudeNBAA IFR 1,000 nm RunwayMissions Flight Time(8 Pax) Fuel Used







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


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


FAR 25 A 77,1967/98

2007 dollars.

ULTRA-LONG-RANGE JETS


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