§29.351. Yawing conditions. — Inbound Citations
14 C.F.R. § 29.351
Statutory Authority
Cited by 4 regulations in release Current.
Citations to 14 U.S.C. § 29.351 as a whole
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(2) The steady-state sideslip angles established by § 29.351;
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(c) The rotor structure must be designed to withstand the following loads prescribed in §§ 29.337 through 29.341 and 29.351:
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(1) The critical loads prescribed in §§ 29.337 through 29.341, and 29.351;
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(a) The critical flight loads in §§ 29.337 through 29.341, and 29.351;