Airworthiness Directives; General Electric Company CF6-80E1 Series Turbofan Engines
airworthiness · Rule · Final rule; request for comments. · Published 2005-11-02 · Effective 2005-12-02 · 70 FR 66250
Document
Document number
05-21805
Federal Register citation
70 FR 66250
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company CF6-80E1 Series Turbofan
Publication date
2005-11-02
Effective date
2005-12-02
FAA docket
Docket No. FAA-2005-22701
Abstract
The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF6-80E1 series turbofan engines installed on Airbus Industrie A330 series airplanes. This AD requires a check of the holding torque of the thrust reverser actuation system (TRAS) locks, and if necessary a visual inspection of the TRAS lock flexible drive shafts, within 10 flight cycles after all aborted takeoffs in which the thrust reverser was deployed. This AD results from reports of operators finding several damaged TRAS lock flexible drive shafts during inspections and checks of the drive shafts. We are issuing this AD to prevent inadvertent in-flight deployment of the thrust reverser, which can result in loss of control of the airplane.