AD 2000-12-20
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A310 | Airworthiness Directives; Airbus Model A310 Series Airplanes |
Unsafe Condition
Fracture of the lead screw of the position 1 flap screw jack, which could result in failure of the tie bar and possible disconnection of the flap structure from the airplane.
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Required Actions
Within 18 months after the effective date, modify the position 1 flap screw jack in accordance with Airbus Service Bulletin A310-27-2075, Revision 02, dated February 8, 2000. As of the effective date, do not install a position 1 flap screw jack with part number 537G0000-02 unless modified in accordance with this AD.
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Compliance Time
Within 18 months after the effective date of July 28, 2000.
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Affected Aircraft
Airbus Model A310 series airplanes, certificated in any category, except those airplanes on which Airbus Modification 10855 or Airbus Service Bulletin A310-27-2075 has been accomplished.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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