AD 92-15-08
Unsafe Condition
Fatigue damage and subsequent reduced structural capability of the horizontal stabilizer attachment.
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Required Actions
Remove the normal maximum (second) detent for the reverse thrust control and install a modified detent in accordance with Fokker Service Bulletin SBF100-76-008. An alternative method of compliance or adjustment of the compliance time may be used if approved by the FAA.
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Compliance Time
Within 7 months after the effective date of this AD
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Affected Aircraft
FOKKER Model F28 Mark 0100 series airplanes; serial numbers 11244 through 11308, inclusive; 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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