AD 95-12-03
Unsafe Condition
Cracking in the frame strips at fuselage stations 14911 and 17011 due to fatigue-related stress, which could result in reduced structural integrity of the fuselage pressure vessel.
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Required Actions
Install reinforcement plates at left and right fuselage stations 14911 and 17011 in accordance with Fokker Service Bulletin SBF100-53-072. Alternative methods of compliance may be approved by the FAA.
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Compliance Time
Prior to the accumulation of 24,000 total flight cycles, or within 6 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 11371 inclusive.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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