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Normas ASTM – AENOR
ASTM F2245-07a

ASTM F2245-07a

Standard Specification for Design and Performance of a Light Sport Airplane

Fecha:
2010-12-31 /Historical
Superseeded by:
Scope:

1.1 This specification covers airworthiness requirements for the design of powered fixed wing light sport aircraft, an airplane.

1.2 This specification is applicable to the design of a light sport aircraft/airplane as defined by regulations and limited to VFR flight.

1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory requirements prior to use.

Keywords:
fixed-wing aircraft; light sport airplane; Airworthiness; BHP (brake horse power); CAS (calibrated air speed); Controllability; Controllability and maneuverability; Design--aircraft materials/applications; Directional control; Drag coefficient (C<inf>D</inf>); Fixed-wing aircraft; Flight; Ground control stability; Lateral control; Lift coefficient (C<inf>L</inf>); Light sport airplane (LSA)--specifications; Load distribution limit; Longitudinal control; MAC (mean aerodynamic chord); Maximum empty weight; Performance--aircraft materials/applications; Safety precautions--consumer materials/applications; Stalling speeds; Static longitudinal stability; Takeoff
72,97
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