AD 2001-08-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-620 | Airworthiness Directives; Airbus Model A300 B4-620, A310-203, A310-221, and A310-222 Series Airplanes |
Unsafe Condition
Fatigue cracking of fuselage frame 07 in the upper frame section assembly of the lateral cockpit windows, which could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a detailed visual inspection to detect cracking of fuselage frame 07 in the lateral cockpit windows. If cracking is found in 'area A,' perform a temporary repair followed by a permanent repair. If cracking is in 'area B' or both areas, perform a permanent repair. Repeat inspections as specified based on the repair actions taken.
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Compliance Time
Before the accumulation of 25,000 total flight cycles, or within 3,000 flight cycles after the effective date of this AD, whichever occurs later.
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Affected Aircraft
Airbus Model A300 B4-620, A310-203, A310-221, and A310-222 series airplanes; certificated in any category; as listed in Airbus Service Bulletin A300-53-6120 or A310-53-2109, both dated May 5, 2000; excluding airplanes on which Airbus Modification 3632 has been accomplished.
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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