AD 99-02-12
Unsafe Condition
Heavy vibration and possible damage to the components of the main landing gear (MLG), and consequent reduced controllability of the airplane during takeoff or landing due to discrepancies of the components of the torque link apex joint and shimmy damper attachments of the MLG.
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Required Actions
Perform a one-time visual inspection of the torque link apex joint and shimmy damper attachments of the MLG in accordance with Fokker Service Bulletin SBF100-32-113. Repair or replace any discrepant component with a new or serviceable component prior to further flight. Submit inspection findings report within specified timeframe.
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Compliance Time
Within 45 days after the effective date of this AD (February 25, 1999).
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Affected Aircraft
Fokker Model F.28 Mark 0070 and 0100 series airplanes as listed in Fokker Service Bulletin SBF100-32-113, dated May 28, 1998.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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