AD 2007-07-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-601 | Airworthiness Directives; Airbus Model A300 B4-601, A300 B4-603, A300 B4-605R, A300 C4-605R Variant F, A310-204, and A310-304 Airplanes Equipped With General Electric CF6-80C2 Engines |
| engine | General Electric | CF6-80C2 | Airworthiness Directives; Airbus Model A300 B4-601, A300 B4-603, A300 B4-605R, A300 C4-605R Variant F, A310-204, and A310-304 Airplanes Equipped With General Electric CF6-80C2 Engines |
Unsafe Condition
Structural damage on the forward pyramid arm of an engine pylon due to chafing of the integrated drive generator (IDG) electrical harness against the structure of the pyramid arm.
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Required Actions
Perform a one-time detailed inspection for discrepancies of the IDG harness, harness bracket, retaining fasteners, and pyramid arm. Repair any damage found and protect the harness. Initiate new repetitive inspections as specified.
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Compliance Time
Within 10 days after May 13, 2004, or within 600 flight hours after May 13, 2004, depending on the incorporation of Airbus Modification 07591.
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Affected Aircraft
Airbus Model A300 B4-601, A300 B4-603, A300 B4-605R, A300 C4-605R Variant F, A310-204, and A310-304 airplanes equipped with General Electric CF6-80C2 engines without full-authority digital electronic control (FADEC), excluding airplanes on which Airbus Modification 13184 was done in production.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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