User:Marc Lacoste/sandbox/Aircraft Specifications

Variants characteristics

General
Variant	major variants only with large differences between them
Crew	number of people required to operate the aircraft
Capacity	number of passengers the aircraft can carry. Multiple configurations possible
Cargo	cargo that can be carried by an aircraft : weight, possibly type and/or volume
Length	overall length of the airframe
Span	wingspan of fixed wing aircraft, or the main rotor diameter for rotorcraft
Height	overall height of an aircraft, landing gear extended
Area	Wing area of fixed wing aircraft, or the total area of all main rotors
Aspect ratio	wing aspect ratio of fixed wing aircraft
Weights
MTOW	Maximum takeoff weight
MLW	Maximum landing weight
MZFW	Maximum zero-fuel weight
OEW	Operating empty weight
Fuel capacity	in weight and/or volume
Engines
Engine type (X×)	manufacturer and model, wikilinked
Power or Thrust	rated
Performance
Maximum speed	maximum speed of the aircraft
Cruise speed	cruise speed of the aircraft
Range	maximum unrefuelled range of the aircraft
Endurance	maximum flight endurance of the aircraft
Ceiling	Maximum service altitude
Climb rate	the maximum rate of climb for a powered aircraft (or time to altitude)
Fuel consumption	fuel burn per distance or per hour

• Unit conversions should be those given by the source if possible to avoid rounding errors, or use the Template:Convert
• If necessary, speed in Mach should be converted with Template:Convert/Mach with a consistent altitude (e.g. ceiling)
• Rows can be added for other characteristics, like "Propeller type" or "Takeoff/Landing distance" in the appropriate section
• Rows can be hidden by putting them in comments if a characteristic isn't available