AC 33.74/92-1A - Turbine Engine Continued Rotation and Rotor Locking
33.74/92-1A - Turbine Engine Continued Rotation and Rotor Locking
- Date Issued
- July 23, 2003
- Responsible Office
- Provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the continued rotation and rotor locking requirements of part 33 of the Federal Aviation Regulations (FARs).
- AC33.74-92-1A.pdf (PDF)
|33.74-92||Turbine Engine Continued Rotation and Rotor Locking||02/14/1997|