AD 94-02-03
Unsafe Condition
Corrosion and subsequent fatigue-related cracking of the attachment bolts on the horizontal stabilizer could lead to loss of stabilizer control.
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Required Actions
Replace two existing bolts (part number D03000-017) with new improved bolts (part number DO3000-021) and perform a functional test in accordance with Fokker Service Bulletin SBF100-27-037.
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Compliance Time
Prior to the accumulation of 13,500 total landings or within 12 months after the effective date of this AD, whichever occurs later
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Affected Aircraft
Fokker Model F28 Mark 0100 series airplanes, serial numbers 11244 through 11300 inclusive, 11303, 11306, 11308, 11310, and 11312 through 11314 inclusive; certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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