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The choice of which is the given first will depend on origin and period. A U.S. aircraft would have U.S. System of customary units given first (in the example of weight 'main' would be given in pounds (lb), and the value for 'alt' in kilograms (kg). Other aircraft are measured using the metric system, so they will have kg for 'main' and lb for ...
There is a long-standing convention within WikiProject:Aircraft that specifications for US, Canadian and UK aircraft (for the UK periods differ - e.g. RAF aircraft until post war used mph, FAA aircraft operated in knots) should be given as English units first, and all others as SI units first.
The names of the aircraft shown in the table are not necessarily those they carried when provided for evaluation as at this point an aircraft would usually be referred to as the Manufacturer X.XX/XX, e.g., the Avro B.35/46 – this is in addition to the manufacturer's own separate internal designation for the aircraft, e.g., Avro 698.
The Liberty XL2 is a two-seat, low-wing, general aviation aircraft manufactured from 2004–2011 by Liberty Aerospace of Melbourne, Florida. A derivative of the Europa XS kit plane , it serves both as a touring aircraft for private flyers and as a flight trainer .
The Use of Pilot Rating in the Evaluation of Aircraft Handling Qualities (PDF) (Technical report). NASA. NASA TN D-5153. Borchers, Paul F.; Franklin, James A.; Fletcher, Jay W. (January 1998). "Flight Research at Ames 1940-1997, Chapter 4 - Flying Qualities, Stability and Control, and Performance Evaluations". NASA SP-3300.
Data from Jane's all the World's Aircraft 1947 General characteristics Crew: 1 Capacity: 3 passengers Length: 21 ft 4 in (6.5 m) tail up Wingspan: 34 ft 2 in (10.41 m) Height: 6 ft 2 in (1.88 m) tail down Wing area: 140.2 sq ft (13.03 m 2) 160 sq ft (14.87 m 2) including wing area projected through fuselage Airfoil: Bellanca B Empty weight: 1,200 lb (544 kg) Gross weight: 2,100 lb (953 kg ...
Please use the {{Aircraft specs}} template when adding specifications. If an article lacks specifications, you can tag it with {{ Aero specs missing }} or add them yourself. If you are editing an article which uses an older specification template, please consider converting it to the current one, which automatically converts units to show both ...
The A-4 was rarely used for refueling in U.S. service after the KA-3 Skywarrior tanker became available aboard the larger carriers. The A-4 was also designed to be able to make an emergency landing, in the event of a hydraulic failure, on the two drop tanks nearly always carried by these aircraft.
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