AD 2007-05-14

final rule
Data completeness: 80%

Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines

AD Number
2007-05-14
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2006-23871
FR Citation
72 FR 9662

Applicability

TypeManufacturerModelDetails
aircraft General Electric Company (GE) CF6-80C2 Turbofan Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines

Unsafe Condition

Cracks in the weld-repaired area of the forward engine mount platform and forward engine mount yoke, which could lead to possible separation of the engine from the airplane.

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

Required Actions

Replace certain installed part number (P/N) and serial number (SN) cast titanium weld-repaired forward engine mount platforms and cast titanium forward mount yokes with a forged titanium or a non-welded cast titanium part.

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

Compliance Time

Before further flight.

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

Affected Aircraft

General Electric Company (GE) CF6-80C2 series turbofan engines with specific part numbers and serial numbers of the affected components.

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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