AD 96-12-14
Unsafe Condition
Fatigue cracks can develop in the lower right-hand wing skin at the attachment bolt holes of the fueling adapter, leading to reduced structural capability of the wing and fuel leakage.
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Required Actions
Reinforce the lower right-hand wing skin at the fueling adapter by installing a new stringer and new internal and external doubler plates in accordance with Fokker Service Bulletin SBF100-57-008, Revision 2.
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Compliance Time
Prior to the accumulation of 12,000 total landings, or within 60 days after the effective date of this AD, whichever occurs later.
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Affected Aircraft
Fokker Model F28 Mark 0100 series airplanes with serial numbers 11244 through 11286 inclusive, 11289, 11290 through 11293 inclusive, 11295, 11297, 11300, 11303, 11306, 11308, 11310, and 11312.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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