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Airworthiness directives › 2003-20-07

AD 2003-20-07 Airworthiness Directives; General Electric Company (GE) CF6-80E1A2 Turbofan Engines

2003-11-03
2003-10-03
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Engine
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Applicability*9

This AD applies to General Electric Company (GE) CF6-80E1A2 turbofan engines with forward engine mount platforms part numbers (P/Ns) 1520M53G04 and 1846M24G15 installed. These engines are installed on, but not limited to Airbus Industrie A330 airplanes.

Compliance

You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done. Platforms Previously Inspected (f) For platforms that were inspected using a fluorescent penetrant inspection (FPI) before the effective date of this AD, repeat the FPI within 4,000 cycles-in-service-since last inspection (CSLI). Platforms Not Previously Inspected (g) For platforms that were not inspected using an FPI before the effective date of this AD, inspect the platform using an FPI at the next exposure, or before exceeding 6,360 cycles-since-new (CSN), whichever occurs first. Platform Repetitive Inspections (h) Repeat the FPI within every 4,000 CSLI. Alternative Methods of

Unsafe condition

This AD is prompted by revised analyses of forward engine mount loads by the airframe manufacturer. We are issuing this AD to prevent engine separation that could result from cracking of the forward engine mount platform.

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1