FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 25 > Section 489 - Ground handling conditions
section 25.487 |
section 25.491
Unless otherwise prescribed, the landing gear and airplane structure must be investigated for the conditions in §§ 25.491 through 25.509 with the airplane at the design ramp weight (the maximum weight for ground handling conditions). No wing lift may be considered. The shock absorbers and tires may be assumed to be in their static position.
[Doc. No. 5066, 29 FR 18291, Dec. 24, 1964, as amended by Amdt. 25-23, 35 FR 5673, Apr. 8, 1970]
   
Current page: FARs > Part 25 > Section 489 - Ground handling conditions
section 25.487 |
section 25.491
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