AD 2001-09-17

Recurring final rule
Data completeness: 70%

Airworthiness Directives; CFM International (CFMI) CFM56-5C Turbofan Engines

AD Number
2001-09-17
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2001-NE-08-AD
FR Citation
66 FR 23541

Applicability

TypeManufacturerModelDetails
aircraft CFM International (CFMI) CFM56-5C Turbofan Airworthiness Directives; CFM International (CFMI) CFM56-5C Turbofan Engines

Unsafe Condition

Interference and chafing between the CJ9L and CJ10L harnesses and the fuel manifold, leading to fuel leakage on the hot section or in the primary fire zone of the engine, which may result in an engine fire and subsequent damage to the airplane.

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

Required Actions

Within 10 days after the effective date, perform an initial inspection of the fuel manifold for wear or chafing, and an initial inspection of the CJ9L and CJ10L harnesses for wear, correct installation, clamp wear, and minimum clearance between the harnesses and the fuel manifold. Repeat inspections of the fuel manifold, clamps, and the CJ9L and CJ10L harnesses every 500 hours time in service until new configuration clamps are installed on the harnesses.

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

Compliance Time

Within 10 days after the effective date of this AD

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Affected Aircraft

CFM International (CFMI) CFM56-5C turbofan engines installed on, but not limited to, Airbus Industrie A340 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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