The structure supporting any engine or auxiliary power unit must be designed for the loads including the gyroscopic loads arising from the conditions specified in §§
25.331, 25.341(a), 25.349, 25.351, 25.473, 25.479, and 25.481, with the engine or auxiliary power unit at the maximum rpm appropriate to the condition. For the purposes of compliance with this section, the pitch maneuver in §
25.331(c)(1) must be carried out until the positive limit maneuvering load factor (point A2 in §
25.333(b)) is reached.
[Amdt. 25-91, 62 FR 40704, July 29, 1997]![[FAR Part § 25.371: Gyroscopic loads -- FAA FARS, 14 CFR] -- Flightsim Aviation Zone - Number 1 Flight Simulation and Aviation Resource! Information, Tools, Downloads, Databases, FAQ, Aviation Humour, Glossaries, Directory, FS2006, Multimedia, Screenshots, Free Flight Planner, Weather Reports](/images/gui/header_logo.gif){kind=logo}
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