AD Amdt-39-12298
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 B4-601 | Airworthiness Directives; Airbus Model A300 B4-601, B4-603, B4-620, B4-605R, B4-622R, and F4-605R (Collectively Called A300-600) Series Airplanes |
Unsafe Condition
Fatigue cracking on the forward fittings in the radius of frame 40 adjacent to the tension bolts in the center section of the wings, which could result in reduced structural integrity of the wings.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform an ultrasonic inspection to detect cracking on the forward fittings in the radius of frame 40 adjacent to the tension bolts in the center section of the wings. If no crack is detected, repeat the inspection at intervals not to exceed 6,500 landings or 16,000 flight hours. If a crack is detected, install an access door, perform an eddy current inspection, and take further actions as specified, including blending out the crack or repairing it if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within specified intervals based on total landings or flight hours, as detailed in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A300 B4-601, B4-603, B4-620, B4-605R, B4-622R, and F4-605R series 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 6, 2026
Rights: U.S. Government Public Domain
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