AD 2011-10-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310-203 | Airworthiness Directives; Airbus Model A310-203, -204, -222, -304, -322, and -324 Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A310-203, -204, -222, -304, -322, and -324 Airplanes |
Unsafe Condition
Reduced structural integrity of the tail cone due to potential cracking and corrosion in the lower tail plane cut-out area.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the lower tail plane cut-out area for cracking, corrosion, and damaged sealant in specified areas. Perform eddy current inspections and rotating probe inspections as required. Take corrective actions such as repairing corrosion, replacing damaged sealant, removing cracking, and installing new components as necessary.
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Compliance Time
Within the applicable time specified in Table 1 of the AD, based on the airplane model and usage (short-range or long-range).
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Affected Aircraft
Airbus Model A310-203, -204, -222, -304, -322, and -324 airplanes, all serial numbers, except those on which Airbus modification 06146 has been done in production.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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