AD 2007-11-12
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Corrosion between the scuff plates at exit and cargo doors and fatigue cracks originating from certain fastener holes located in adjacent structure, which could result in reduced structural integrity of the door surroundings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the lower door surrounding structure for cracks and corrosion; inspect for cracking of the holes of the corner doublers, the fail-safe ring, and the door frames of the door structures; repair if necessary; and perform a terminating modification for repetitive inspection of corner doublers, fail-safe ring, and door frames.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the compliance times specified in the AD, unless actions have already been done.
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Affected Aircraft
Airbus Model A310 series airplanes, certificated in any category, excluding those airplanes on which Airbus Modifications 5068, 7201, and 7298 have been incorporated in production.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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