AD 91-07-10
Unsafe Condition
Main landing gear (MLG) vibration and subsequent failure of the MLG due to wire harness brackets and torque link (TL) subassemblies not meeting requirements.
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Required Actions
Replace MLG wire harness assembly brackets per Fokker Service Bulletin F100-32-034 within 180 days. Install torque link (TL) dampers and TL subassemblies per Dowty Rotol Service Bulletin F100-32-34 within 180 days. Alternative methods may be approved by the FAA.
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Compliance Time
Within 180 days after the effective date of this AD
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Affected Aircraft
FOKKER Model F-28 Mark 0100 series airplanes with serial numbers 11244 through 11266, 11268 through 11283, 11286, 11289, 11291 through 11293, 11295, 11297, 11300, 11303, and 11306.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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