AD 2013-13-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A319-112 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracks on the left-hand and right-hand sides of the continuity fittings at the front windshield lower framing.
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 for any cracking on the left-hand and right-hand sides of the windshield central lower node continuity fittings. Repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 4,500 flight cycles after the effective date of this AD, or before the accumulation of 34,000 total flight cycles since the airplane's first flight, whichever occurs later.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A319-112, -113, and -132 airplanes; Model A320-211, -212, -214, -231, and -232 airplanes; and Model A321-111 and -131 airplanes, with specific serial numbers listed in the AD.
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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