AD 2000-04-14

final rule
Data completeness: 70%

Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines

AD Number
2000-04-14
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 99-NE-24-AD
FR Citation
65 FR 10698

Applicability

TypeManufacturerModelDetails
engine General Electric Company CF6-80C2 Series Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines

Unsafe Condition

High-pressure fuel leaks caused by improper seating of fuel tube flanges, which could result in an engine fire and damage to the airplane.

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Required Actions

Replace the fuel tube connecting the flowmeter to the Integrated Drive Generator (IDG) and the fuel tube(s) connecting the Main Engine Control (MEC) or Hydromechanical (HMU) to the flowmeter with improved fuel tubes. This must be done during on-wing maintenance when the fuel tubes are disconnected or at the next shop visit.

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

Compliance Time

At the next opportunity when the fuel tubes are disconnected for on-wing maintenance or at the next shop visit.

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Affected Aircraft

General Electric Company CF6-80C2 series turbofan engines, including models A1, A2, A3, A5, A8, A5F, B1, B2, B4, B6, B1F, B2F, B4F, B6F, B7F, and D1F, installed on but not limited to Airbus A300-600/600R, A310-200Adv/300, Boeing 747-200/300/400, 767-200ER/300/300ER/400ER, 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 6, 2026

Rights: U.S. Government Public Domain

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