AD 2013-23-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking in area 2 of the frame base fittings between frame 41 and frame 46, which could adversely affect the structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Check maintenance records to determine if certain repairs were done in area 1 of the frame base fittings. For affected airplanes, perform a detailed inspection for cracking in area 2 of the frame base fittings between frame 41 and frame 46, and repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 1,000 flight hours after the effective date of this AD.
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Affected Aircraft
Airbus Model A300 series airplanes, including Model A300 B4-600, B4-600R, and F4-600R series airplanes; and Model A300 C4-605R Variant F airplanes, on which repairs have been done as specified in Airbus Service Bulletin A300-53-0337 (original or Revision 01) or Airbus Service Bulletin A300-53-6111 (original up to Revision 05).
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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