AD 2004-14-09
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Model A320-111, -211, -212, and -231 Series Airplanes |
Unsafe Condition
Fatigue cracking of the lower surface panel on the wing center box, which could result in reduced structural integrity of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the lower surface panel on the wing center box for fatigue cracking, repair if necessary, and modify the lower surface panel as terminating action for repetitive inspections.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 3,500 flight cycles after the effective date of this AD, or prior to the accumulation of 20,000 total flight cycles, whichever is later.
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 on which Airbus Modification 22418 (reference Airbus Service Bulletin A320-57-1043) has not been done.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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