AD 2015-02-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A300 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Cracking in the rear spar web of the wings between Ribs 1 and 2, due to fatigue-related high shear stress, which could affect structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the aft face of the wing rear spar in the area adjacent to the build slot on both Left Hand (LH) and Right Hand (RH) wings using eddy current inspection. Repair any detected cracks as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Airbus Model A300 series airplanes; Model A300 B4-600, B4-600R, and F4-600R series airplanes; and Model A300 C4-605R Variant F airplanes, including those with Airbus Modification 12102 embodied in production and those with Airbus Service Bulletin A300-57-6063 (Airbus mod 11130) embodied in service.
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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