AD 2014-19-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Airplanes |
Unsafe Condition
Fatigue cracking in the transition and pick-up angles between Frame (FR) 35 and FR36 in the lower part of the center fuselage area, 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
Install washers between the transition pick-up angle and the pin nuts, and perform related investigative and corrective actions if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
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, including those added to the applicability of AD 2004-03-19.
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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