AD 91-13-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | A310-203 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310-200 Series Airplanes |
| aircraft | Airbus SAS | A310-221 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310-200 Series Airplanes |
| aircraft | Airbus SAS | A310-222 | Airworthiness Directives; AIRBUS INDUSTRIE Model A310-200 Series Airplanes |
Unsafe Condition
Reduced structural integrity of the fuselage due to potential cracks in the cabin floor structure between Frame 40 and Frame 46.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a visual inspection of the cabin floor structure between Frame 40 and Frame 46 prior to 12,000 landings or within 6 months after July 15, 1991, whichever is later. Repeat inspections at intervals not exceeding 3,000 landings. If cracks are found, replace the affected part or modify the area before further flight. Modification via Service Bulletin A310-53-2013 terminates inspection requirements.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 12,000 landings, or within 6 months after the effective date of this AD, whichever occurs later
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Affected Aircraft
AIRBUS INDUSTRIE Model A310-200 series airplanes, serial numbers 162 through 378, inclusive; on which Modification 4942 has not been incorporated
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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