AD 2005-20-35
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Model A320-111 Airplanes |
Unsafe Condition
Fatigue cracking in the upper stringers of the center wing box, which could lead to loss of structural integrity of the wing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Continue repetitive inspections for cracking in the front and rear faces and at the crown fittings of the upper stringers of the center wing box between frame (FR) 36 and FR42, with revised thresholds and intervals. Perform applicable repairs as specified in the service information, using a repair method approved by the FAA or DGAC (or its delegated agent).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the revised intervals specified in the service information.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A320-111 airplanes, as identified in the most recent type certificate data sheet for the affected models.
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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