AD 2009-11-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-202 | Airworthiness Directives; Airbus Model A330-202, -223, -243, -301, -322, and -342 Airplanes |
| aircraft | Aviat | Various | Airworthiness Directives; Airbus Model A330-202, -223, -243, -301, -322, and -342 Airplanes |
Unsafe Condition
Cracks appeared on the right and left sides between the crossing area of the keel angle fitting and the front spar of the Centre Wing Box (CWB). The new design modifications have caused interference between one fastener and the keel angle, impacting the structural integrity of the reprofiled area.
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Required Actions
Conduct a repetitive special detailed inspection using high frequency eddy current to detect cracking on the horizontal flange of the keel beam in the area of the first fastener hole aft of frame [FR] 40. Repair any detected cracks accordingly.
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Compliance Time
Within 12 months of the effective date
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Affected Aircraft
Airbus Model A330-202, -223, -243, -301, -322, and -342 airplanes; certificated in any category; serial numbers 0177, 0181, 0183, 0184, 0188, 0189, 0191, 0195, 0198, 0200, 0203, 0205, 0206, 0209, 0211, 0219, 0222, 0223, 0224, 0226, 0229, 0230, 0231, 0232, 0234, 0238, 0240, 0241, 0244, 0247, 0248, 0249, 0250, 0251, 0253, 0254, and 0255.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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