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Standard Specification for Design and Performance of a Light Sport Airplane
STANDARD published on 1.5.2010
Designation standards: ASTM F2245-10
Note: WITHDRAWN
Publication date standards: 1.5.2010
SKU: NS-53339
The number of pages: 28
Approximate weight : 84 g (0.19 lbs)
Country: American technical standard
Category: Technical standards ASTM
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 (CD), Fixed-wing aircraft, Flight, Ground control stability, Lateral control, Lift coefficient (CL), Light sport airplane (LSA)--specifications, Load distribution limit, Longitudinal control, MAC (mean aerodynamic chord), Maximum empty weight
1. 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. |
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2. Referenced Documents | ||||||||||||||||
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