VTOL.2225 Component
loading conditions
n/a
(a) The applicant must determine the loads acting upon all relevant structural components, including rotor assemblies, in response to:
(1) interaction of systems and structures;
(2) structural design loads;
(3) flight load conditions;
(4) ground and water load conditions; and
(5) limit input torque from lift/thrust units at any rotational speed.
(b) Reserved.
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