14 CFR § 33.74 Airworthiness Standards: Aircraft Engines

§ 33.74 Continued rotation.

Current through Jul 24, 2026 · Read all of Part 33

⚠ 2 pending changes to Part 33

If any of the engine main rotating systems continue to rotate after the engine is shutdown for any reason while in flight, and if means to prevent that continued rotation are not provided, then any continued rotation during the maximum period of flight, and in the flight conditions expected to occur with that engine inoperative, may not result in any condition described in § 33.75(g)(2)(i) through (vi) of this part.

[Amdt. 33-24, 72 FR 50867, Sept. 4, 2007]

← § 33.73 Power or thrust response.§ 33.75 Safety analysis. →