AD 2011-10-06
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
Reduced structural integrity of the wings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Cold working of trellis boom drainage holes; repetitive detailed or rotating probe inspections for cracking in drain holes on the lower skin panel in the center wing box between frames 42 and 46, with corrective actions if necessary; repetitive eddy current inspections for cracking of the upper corner angle fitting and the vertical tee fitting at left and right frame 40, with corrective actions if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the applicable time specified in Table 1 of the AD, depending on configuration and usage (short or long range).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes, all serial numbers.
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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