AD 2004-03-19
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Model A320-111, -211, and -231 Series Airplanes |
Unsafe Condition
Fatigue cracking in the transition and pick-up angles of the lower part of the center fuselage, which could result in reduced structural integrity of the wing-fuselage support and fuselage pressure vessel.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect for cracking in the transition and pick-up angles of the lower part of the center fuselage. Take corrective action if cracking is detected.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the reduced compliance time specified by this amendment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A320-111, -211, and -231 series airplanes.
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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