33.74/92-1A - Turbine Engine Continued Rotation and Rotor Locking

Date Issued
July 23, 2003
Responsible Office
ANE-110
Description
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).

Cancels

Number Title Date
33.74-92 Turbine Engine Continued Rotation and Rotor Locking 02/14/1997