AD Amdt-39-10360
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Model A320-111, -211, -212, - 214, -231, -232, and -233 Series Airplanes |
Unsafe Condition
Fatigue cracking in the wing/fuselage joint cruciform fittings could result in reduced structural integrity of the wing/fuselage.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform repetitive ultrasonic inspections to detect fatigue cracking in the wing/fuselage joint cruciform fittings and perform 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, -212, -214, -231, -232, and -233 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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