FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 121 > Section 279 - Control of engine rotation
section 121.277 |
section 121.281
(a) Except as provided in paragraph (b) of this section, each airplane must have a means of individually stopping and restarting the rotation of any engine in flight.
(b) In the case of turbine engine installations, a means of stopping the rotation need be provided only if the Administrator finds that rotation could jeopardize the safety of the airplane.
   
Current page: FARs > Part 121 > Section 279 - Control of engine rotation
section 121.277 |
section 121.281
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