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ASTM WK35518

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Work Item: ASTM WK35518 - Revision of F2245 - 11 Standard Specification for Design and Performance of a Light Sport Airplane


Active Standard: F2245 - 13

Developed by Subcommittee: F37.20 | Committee F37 Home | Contact Staff Manager



1. Rationale

Confusion over the interpretation and use of the minimum useful load requirements and the emersion of electrical propulsion requirements have prompted a review of this section. The final goal is a revised set of language that is more clear and would allow potential provisions for electrical propulsion.


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; Performance--aircraft materials/applications; Safety precautions--consumer materials/applications; Stalling speeds; Static longitudinal stability; Takeoff ;

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Work Item Status:
Date Initiated:12-06-2011
Technical Contact: Severin Kempf

Status: Draft Under Development

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