AD Amdt-39-10573
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 area 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
Conduct repetitive inspections for cracking in the transition and pick-up angles in the lower part of the center fuselage area. Perform corrective action if cracking is found. An optional terminating modification is available to cease repetitive inspections.
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 as specified by the foreign civil airworthiness authority's mandatory continuing airworthiness information.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.