Airworthiness Directive · Amendment 39-9011 · General Electric Company Engines
General Electric Company Engines
This AD applies to General Electric Company CT7-5A2, CT7-5A3, CT7-7A, CT7-7A1, CT7-9B, CT7-9B1, CT7-9B2, CT7-9C, CT7-9D.
The models as the FAA's AD index lists them. The serial ranges, installed parts and exceptions are in the AD itself: read it at the FAA.
This amendment supersedes an existing airworthiness directive (AD), applicable to General Electric Aircraft Engines (GEAE) CT7 series turboprop engines, that currently requires a one-time ultrasonic inspection of a suspect population of propeller shafts for metallurgical defects, and if necessary, replacement with a serviceable part. This amendment extends the compliance time for the required ultrasonic inspection on certain propeller shafts. This amendment is prompted by information indicating that the equipment necessary to perform the ultrasonic inspection is less available than originally assumed. The actions specified by this AD are intended to prevent failure of the propeller shaft, which can result in separation of the propeller from the propeller shaft and possible damage to the aircraft.
