Airworthiness Directive · Amendment 39-10186 · General Electric Company CF6-50 and - 80C2 Series Turbofan Engines
General Electric Company CF6-50 and - 80C2 Series Turbofan Engines
General Electric Company (GE) CF6-50 and -80C2 series turbofan engine, installed on but not limited to Boeing 767 and 747 series, McDonnell Douglas DC-10 and MD-11, and Airbus Industries A300 and A310 series aircraft.
This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF6-50 and -80C2 series turbofan engines. This action requires removal from service of defective high pressure compressor rotor (HPCR) stage 3-9 spools, and replacement with serviceable parts. This amendment is prompted by a report of an uncontained failure of an HPCR stage 3-9 spool installed on a GE model CF6-80C2 turbofan engine. The actions specified in this AD are intended to prevent failure of the HPCR stage 3-9 spool, which can result in an uncontained engine failure and damage to the aircraft.
