AD 2002-10-08

Recurring final rule
Data completeness: 70%

Airworthiness Directives; General Electric Company CF6-80E1 Series Turbofan Engines

AD Number
2002-10-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NE-04-AD
FR Citation
67 FR 36090

Applicability

TypeManufacturerModelDetails
aircraft Airbus Industrie A330 Airworthiness Directives; General Electric Company CF6-80E1 Series Turbofan Engines
engine General Electric Company CF6-80E1 Series Airworthiness Directives; General Electric Company CF6-80E1 Series Turbofan Engines

Unsafe Condition

Service-induced hardware deterioration reduces the overall thrust reverser system protection against inadvertent deployment, which can result in loss of control of the airplane.

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

Required Actions

Initial and repetitive thrust reverser inspections and checks are required. Extended threshold and repetitive inspection intervals are allowed if an optional double p-seal configuration is installed.

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 CF6-80E1 series turbofan engines installed on Airbus Industrie A330 series airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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