AD 94-26-03
Unsafe Condition
Cracking in the area of the side stay attachment lugs of the fitting subassembly of the main landing gear (MLG) due to stress corrosion cracking, which could lead to damage to and/or failure of the MLG support structure.
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Required Actions
Conduct a one-time eddy current inspection to detect cracking in the MLG fitting subassembly side stay attachment lugs. Replace any cracked subassemblies with new or serviceable subassemblies. Provide credit for prior overhauls meeting specific criteria (e.g., performed within 12,000 cycles or 12 years, using specified maintenance manuals).
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Compliance Time
3 months after the effective date of the AD (January 26, 1995).
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Affected Aircraft
Fokker Model F28 Mark 1000, 2000, 3000, and 4000 series airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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