FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 23 > Section 505 - Supplementary conditions for skiplanes
section 23.499 |
section 23.507
In determining ground loads for skiplanes, and assuming that the airplane is resting on the ground with one main ski frozen at rest and the other skis free to slide, a limit side force equal to 0.036 times the design maximum weight must be applied near the tail assembly, with a factor of safety of 1.
[Amdt. 23-7, 34 FR 13090, Aug. 13, 1969]
   
Current page: FARs > Part 23 > Section 505 - Supplementary conditions for skiplanes
section 23.499 |
section 23.507
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