AD 2010-04-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Cracks around the wing top skin panels fastener holes at Rib 2 (LH or RH), between stringers 2 and 14, which may lead to degradation of the structure in this area.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Implement an inspection programme to detect any visible cracks in the wing top skin panels 1 and 2 along Rib 2. Repair any detected cracks appropriately.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes, certificated in any category.
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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