AD 2009-04-10

final rule
Data completeness: 80%

Airworthiness Directives; General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 Series Turbofan Engines

AD Number
2009-04-10
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2008-0952
FR Citation
74 FR 7995

Applicability

TypeManufacturerModelDetails
engine General Electric Company CF6-80A Airworthiness Directives; General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 Series Turbofan Engines

Unsafe Condition

Critical life-limited rotating engine part failure, which could result in an uncontained engine failure and damage to the airplane.

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Required Actions

Revise the Airworthiness Limitations Section (ALS) of the manufacturer's Instructions for Continued Airworthiness (ICA) and, for air carrier operations, revise the approved continuous airworthiness maintenance program to add mandatory inspections of selected critical life-limited parts at each piece-part opportunity. Inspections must be performed in accordance with the instructions provided in the applicable manual provisions.

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Compliance Time

Within 180 days after the effective date of this AD.

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Affected Aircraft

General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 series turbofan engines installed on, but not limited to, Airbus A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series airplanes.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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