AD 2000-20-15
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 and A300-600 | Airworthiness Directives; Airbus Model A300 and A300-600 Series Airplanes |
Unsafe Condition
Fatigue cracking of the rear fittings of fuselage frame FR40 at stringer 27, which could 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
Perform a high frequency eddy current (HFEC) inspection to detect cracks in the stiffeners at stringer 27 of the rear fitting of fuselage frame FR40, left and right, in accordance with specified Airbus Service Bulletins. Repetitive inspections or repair are required, as applicable. Alternatively, a modification can be installed to defer inspections for a certain period.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Varies by model and flight cycle/flight hour thresholds, as detailed in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300 and A300-600 series airplanes, on which Airbus Modification 11525 has not been accomplished, 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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