Airworthiness Directives; General Electric Company CF6-50, -80A1/A3, and -80C2A Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2008-01-24 · Effective 2008-02-28 · 73 FR 4057
Document
Document number
E8-975
Federal Register citation
73 FR 4057
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2008-01-24
Effective date
2008-02-28
FAA docket
Docket No. FAA-2007-0053
Abstract
The FAA is superseding an existing airworthiness directive (AD) for General Electric Company (GE) CF6-50, -80A1/A3, and -80C2A series turbofan engines, installed on Airbus A300, A300-600, and A310 series airplanes. That AD currently requires initial and repetitive inspections and checks of the thrust reverser actuation systems. This AD requires revised inspection thresholds and intervals, and would require the same actions and additional inspections of the thrust reverser actuation system locking features. This AD results from refined safety analyses performed on the thrust reverser systems by GE and Airbus. We are issuing this AD to prevent inadvertent in-flight thrust reverser deployment, which can result in loss of control of the airplane.