AD 2007-26-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Model A300 Airplanes; and Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes) |
Unsafe Condition
Fatigue cracking of the left and right upper radius at frame 47, which could propagate and result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Retain existing repetitive inspections to detect cracking of the upper radius of the forward fitting of frame 47, reduce inspection thresholds and repetitive intervals, and add related investigative and corrective actions. Provide an optional terminating action for airplanes with cracking within certain limits, and implement a post-repair inspection program following the optional terminating action.
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Affected Aircraft
All Airbus Model A300 B2 and B4 series airplanes; all Model A300 B4-600, B4-600R, and F4-600R (collectively called A300-600) series airplanes; and Model C4-605R Variant F Airplanes.
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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