AD 2014-23-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking in the lower spar of the nacelle pylon between ribs 9 and 10, which could result in reduced structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracks in the lower spar axis of the nacelle pylon between ribs 9 and 10 using eddy current and liquid penetrant methods. Repair any detected cracks, including reinforcing the lower spar with a doubler for certain crack lengths.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A300, A300-600, and A310 series airplanes, including specific models and serial numbers as detailed in the AD.
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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