AD 2015-02-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-601 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking found in the pylon box due to stresses resulting from the pressure applied by the thrust reverser cowl bumpers, which could reduce structural integrity of the airplane.
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Required Actions
Conduct repetitive high frequency eddy current (HFEC) inspections for cracking in the pylon rib 5; replace all fittings if necessary, which terminates the repetitive HFEC inspections for the modified side only.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A300 B4-601, B4-603, B4-605R, F4-605R, and C4-605R Variant F airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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