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AD FAA-2007-0053

Airworthiness Directives; General Electric Company CF6-50, -80A1/A3, and -80C2A Series Turbofan Engines

Summary

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.

Directive Details

AD Number

FAA-2007-0053

Document Number

E8-975

Type

Rule

Publication Date

January 24, 2008

Effective Date

February 28, 2008

Affected Manufacturer

General Electric Company CF6-50, -80A1/A3, and -80C2A Series Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2007-0053

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for General Electric Company CF6-50, -80A1/A3, and -80C2A Series Turbofan →

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