AD Amdt-39-10602
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320 | Airworthiness Directives; Airbus Model A320 Series Airplanes |
Unsafe Condition
Fatigue cracking of the former junction at frame 68 of the aft fuselage could reduce structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive rotating probe inspections of fastener holes and adjacent tooling hole of the aft fuselage former junction. Perform corrective action if cracks are found. Optional terminating action for repetitive inspections may be performed.
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Compliance Time
Before further flight
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Affected Aircraft
Airbus Model A320 series airplanes subject to mandatory continuing airworthiness information from a foreign civil airworthiness authority.
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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