Aircraft Performance Data from Conklin de Decker at AvBuyer.com

Aircraft Performance Data

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Aircraft
Performance
Data

Aircraft Make/Model:

Aircraft Category:

Guide Price:

» General Information

Variable cost per hour:

Engine manufacturer:

Engine model:

Number of engines:

» General Cabin Dimensions

Cabin height:

Cabin width:

Cabin length:

Cabin volume:

Door height:

Door width:

» Baggage

Variable cost per hour:

» Typical Passenger Seating

Crew:

Seats executive:

» Weights

Maximum take off weight:

Maximum landing weight:

Basic operating weight with crew:

Useable fuel:

Payload with full fuel:

Maximum payload:

» Performance Range

Range w/ seats full:

Maximum range:

V f r range seats full:

V f r maximum range:

» Balanced Field Length

Balanced field length:

» Landing Distance

Landing distance factored:

» Rate of Climb(Ft/Min)

Rate of climb all engines:

Rate of climb one engine out:

» Cruise Speed

Max cruise speed:

Normal cruise speed:

Long range cruise speed:

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Please note that this data should be used as a guide only, and not as the basis on which buying decisions are taken. If there are other ways in which we can improve the content or presentation of this information please contact us:

Editor, World Aircraft Sales Magazine
Email: editorial@avbuyer.com Tel: +44 (0)20 8255 4000 Fax: +44 (0)20 8255 4300

Data courtesy of Conklin & de Decker, Orleans, MA, USA
Email: dwyndham@conklindd.com Web: www.conklindd.com Tel: +1 508 255 5975

General Cabin Dimensions

Cabin Height, Width, and Length are based on a completed interior. On “cabin-class” aircraft, the length is measured from the cockpit divider to the aft pressure bulkhead (or aft cabin bulkhead if unpressurized). For small cabin aircraft, the distance is from the cockpit firewall to the aft bulkhead. Height and width are the maximum within that cabin space.

Cabin Volume is the interior volume, with headliner in place, without chairs or other furnishings.

Cabin Door Height and Width are the measurements of the main passenger cabin entry door.

Baggage

Internal baggage volume is the baggage volume that is accessible in flight by the passenger. This amount may vary with the interior layout.

External baggage volume is the baggage volume not available in flight (nacelle lockers, etc.).

Typical Passenger Seating

This is the typical crew and passenger seating commonly used on the aircraft. This is not the maximum certificated seats of the aircraft. These numbers may vary for different operations (Corporate, Commercial, EMS, etc.).

Weights

Maximum take-off weight is specified during aircraft certification.

Basic Operating Weight is the empty weight, typically equipped, plus unusable fuel and liquids, flight crew (see Typical crew/Pass Seating) and their supplies. Useable fuel is the useable fuel in gallons x 6.7 pounds per gallon (Jet fuel) or 6 pounds per gallon (AVGAS).

Payload - Full Fuel is the useful load minus the useable fuel. The useful load is based on the maximum ramp weight minus the basic operating weight.

Payload - Maximum is the maximum zero fuel weight minus the basic operating weight.

Performance Range

Range - SEATS FULL NBAA IFR Res (N.Mi.) - Seats Full is the maximum IFR range of the aircraft with all passenger seats occupied. This uses the NBAA IFR alternate fuel reserve calculation for a 200 N.Mi. alternate. This is used for jet and turboprop aircraft.

Range - TANKS FULL NBAA IFR Res (N.Mi.) - Tanks Full is the maximum IFR range of the aircraft with the maximum fuel on board and no passenger seats occupied. This uses the NBAA IFR alternate fuel reserve calculation for a 200 N.Mi. alternate. This is used for jet and turboprop aircraft.

Balanced Field Length

BFL is the distance obtained by determining the decision speed (V1) at which the take-off distance and the accelerate-stop distance are equal (fixed-wing multi-engine aircraft only). This is based on four passengers and maximum fuel on board (turbine aircraft). For single-engine and all piston fixed-wing aircraft, this distance represents the take-off field length at Maximum Take-off Weight (MTOW).

Landing Distance

For fixed-wing turbine aircraft, landing distance is computed using FAR 121 criteria. This takes the landing distance from 50/35 feet (depends on certification criteria) and multiplies that by a factor of 1.667. No credit is given for thrust reversers. Configuration is with four passengers and NBAA IFR Fuel Reserve on board. For fixed-wing piston aircraft, this figure is the landing distance over a 50 foot obstacle.

Rate of Climb (Ft/Min)

The rate of climb, given in feet per minute, is for all engines operating, at MTOW, ISA conditions. One Engine Out rate of climb is for one engine inoperative rate of climb at MTOW, ISA.

Cruise Speed

Max - (KTAS) is the maximum cruise speed at maximum continuous power. This may also be commonly referred to as High Speed Cruise. Normal cruise speed is the recommended cruise speed established by the manufacturer. This speed may also be the same as Maximum Cruise Speed. Long Range Cruise is the manufacturer’s recommended cruise speed for maximum range.

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