AD 2000-10-18
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | Industrie Model A300 | Airworthiness Directives; Airbus Industrie Model A300, A300-600, and A310 Series Airplanes |
Unsafe Condition
Fatigue cracking in the lower spar axis of the engine pylons between ribs 6 and 7, which could result in reduced structural integrity of the engine pylon's lower spar and possible separation of the engine from the airplane.
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Required Actions
Perform internal eddy current inspections to detect cracks in the lower spar axis of the pylons between ribs 6 and 7. If cracks are found, stop-drill and repair as specified. Repeat inspections at specified intervals based on crack size and repair status.
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Compliance Time
Within 500 landings after June 28, 1996, or at specified intervals based on crack detection and repair actions.
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Affected Aircraft
Airbus Industrie Model A300, A300-600, and A310 series airplanes, as listed in Airbus Service Bulletins A300-54-0073 and A300-54-6014, Revision 1, dated March 28, 1994, and Model A310 series airplanes, except those on which Airbus Modification 10149 has been accomplished.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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