FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 27 > Section 691 - Autorotation control mechanism
section 27.687 |
section 27.695

Each main rotor blade pitch control mechanism must allow rapid entry into autorotation after power failure.
  
Current page: FARs > Part 27 > Section 691 - Autorotation control mechanism
section 27.687 |
section 27.695

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