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  5. § 33.92
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14 CFR · Part 33

14 CFR § 33.92

Rotor locking tests.

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Read in Subpart F
Part 33 Contents
  • Subpart A: General
  • Subpart B: Design and Construction; General
  • Subpart C: Design and Construction; Reciprocating Aircraft Engines
  • Subpart D: Block Tests; Reciprocating Aircraft Engines
  • Subpart E: Design and Construction; Turbine Aircraft Engines
  • Subpart F: Block Tests; Turbine Aircraft Engines
  • Subpart G: Special Requirements: Turbine Aircraft Engines
  • Appendix A to Part 33: Instructions for Continued Airworthiness
  • Appendix B to Part 33: Certification Standard Atmospheric Concentrations of Rain and Hail
  • Appendix D to Part 33: Mixed Phase and Ice Crystal Icing Envelope (Deep Convective Clouds)

If continued rotation is prevented by a means to lock the rotor(s), the engine must be subjected to a test that includes 25 operations of this means under the following conditions:

(a)

The engine must be shut down from rated maximum continuous thrust or power; and

(b)

The means for stopping and locking the rotor(s) must be operated as specified in the engine operating instructions while being subjected to the maximum torque that could result from continued flight in this condition; and

(c)

Following rotor locking, the rotor(s) must be held stationary under these conditions for five minutes for each of the 25 operations.

Reflects the eCFR edition current as of September 29, 2026. Retrieved from ecfr.gov on October 16, 2026.

Primary Source

  • Official Source (14 CFR · Part 33)