AD Amdt-39-9557
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Model A320-111 Series Airplanes |
Unsafe Condition
Fatigue cracking can initiate from the fastener holes at the splicing cap at nose forward Frame 8.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the splicing cap at nose forward Frame 8 by cold expansion of the fastener holes and install new oversize fasteners.
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 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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