AD 2006-04-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A318-100 | Airworthiness Directives; Airbus Model A318-100 Series Airplanes, Model A319-100 Series Airplanes, Model A320-111 Airplanes, Model A320-200 Series Airplanes, and Model A321-100 Series Airplanes |
Unsafe Condition
Wear damage to the inboard flap trunnions after incorporation of the terminating modification, which could lead to loss of flap surface control and consequently result in the flap detaching from the airplane.
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Required Actions
Perform a detailed inspection of the inboard flap trunnions for any wear marks and of the sliding panels for any cracking at the long edges, and do any corrective actions as applicable, by accomplishing all of the applicable actions specified in the Accomplishment Instructions of Airbus Service Bulletin A320-57-1133, dated July 28, 2005.
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Compliance Time
Within 18 months after January 8, 2001 (the effective date of AD 2000-24-02).
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Affected Aircraft
Airbus Model A318-111 and -112 airplanes on which Airbus Modification 26495 has been incorporated in production; all Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111 airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, and -131 airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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