AD Amdt-39-11362
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A321 | Airworthiness Directives; Airbus Model A321 Series Airplanes |
Unsafe Condition
Loss of structural integrity of the rear part of the fuselage structure due to an undetected tail scrape during landing or takeoff.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Reinforce the fuselage structure between frames 62 and 64.
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 A321 series airplanes, as specified in the AD.
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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