AD Amdt-39-14354
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A320-111 | Airworthiness Directives; Airbus Model A320-111 Airplanes, and Model A320-200 Series Airplanes |
Unsafe Condition
Tail cone triangles were not installed properly during production, resulting in possible mis-rigged elevator servo-controls, which could lead to excessive vibrations of the elevators, reduced structural integrity, and reduced controllability of the airplane.
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Required Actions
Perform a detailed inspection of each tail cone triangle within 800 flight hours after the effective date. If the position is not within specified limits, re-rig the elevator servo controls and adjust the elevator neutral setting within 3,500 flight hours after the inspection.
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Compliance Time
Within 800 flight hours after the effective date for inspection; within 3,500 flight hours after inspection for corrective actions.
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Affected Aircraft
Airbus Model A320-111, -211, -212, -214, -231, -232, and -233 airplanes, certificated in any category, as listed in Airbus Service Bulletin A320-27-1132, Revision 01, dated June 19, 2002.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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