AD 2000-24-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A319 | Airworthiness Directives; Airbus Model A319, A320, and A321 Series Airplanes |
Unsafe Condition
Chafing and resultant wear damage on the inboard flap drive trunnions or on the protective half-shells, which could result in failure of the trunnion primary load path, adversely affect the fatigue life of the secondary load path, and lead to loss of the flap.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the protective half-shell (area 1) and trunnion (area 2) for wear or debonding, depending on the airplane model and modifications installed. For airplanes without a protective half-shell, inspect areas 1 and 2 of the inboard flap trunnion for wear. Perform follow-on repetitive inspections and/or corrective actions as applicable, based on the findings of the initial inspection.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 500 flight hours after September 27, 1999, or as specified based on the airplane model and modifications installed.
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Affected Aircraft
Airbus Model A319, A320, and A321 series airplanes, certificated in any category, except those on which Airbus Modification 26495 has been accomplished.
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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