AD 2004-23-20
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B2 | Airworthiness Directives; Airbus Model A300 B2, A300 B4, A300 B4-600, and A300 B4-600R Series Airplanes; and Model A300 C4-605R Variant F and A300 F4-605R Airplanes |
Unsafe Condition
Cracking in the area surrounding certain fuselage attachment holes, which could result in a ruptured frame foot and reduced structural integrity of the airplane.
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Required Actions
Modify certain fuselage frames as specified in Airbus Service Bulletins A300-53-0271 and A300-53-6125. This modification terminates certain repetitive inspections.
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Compliance Time
Within the earlier of the flight-cycle and flight-hour grace periods specified in the service bulletins.
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Affected Aircraft
Airbus Model A300 B2, A300 B4, A300 B4-600, A300 B4-600R Series Airplanes; and Model A300 C4-605R Variant F and A300 F4-605R Airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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