AD Amdt-39-9992
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Model A320-111, -211, -212, and -231 Series Airplanes |
Unsafe Condition
Tail section of the fuselage at frames 68 and 69 striking the runway during takeoffs and landings could cause structural damage leading to fuselage depressurization during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Reinforce the tail section of the fuselage at frames 68 and 69 to prevent structural damage from runway strikes.
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, and -231 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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