Sec. 25.489 - Ground handling conditions.
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]