Rebound landing condition.

CFR · 2024-01-01 · US · Title 14

(a) The landing gear and its supporting structure must be investigated for the loads occurring during rebound of the airplane from the landing surface. (b) With the landing gear fully extended and not in contact with the ground, a load factor of 20.0 must act on the unsprung weights of the landing gear. This load factor must act in the

official document · source cfr-2024 · id 14:§ 25.487