AD Amdt-39-10649
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Model A300 Series Airplanes |
Unsafe Condition
Cracking in the forward canted frames between fuselage frames 47a and 48 from stringer 41 to STGR 43 could result in failure of the forward canted frame and consequent reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive inspections to detect cracks in the forward canted frames between fuselage frames 47a and 48 from stringer 41 to STGR 43. Perform temporary repair or replace the forward canted frame with a new frame if cracks are found.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A300 series airplanes as specified in the AD
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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