AD 95-03-05
Unsafe Condition
Cracks in the cleats at left- and right-hand rib station 8200 of the wing due to improper installation of certain bolts, which could result in reduced structural integrity of the wing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time high-frequency eddy current inspection to detect cracks in the cleats at rib station 8200, and replace any cracked cleats with new cleats in accordance with Fokker Service Bulletin SBF100-57-018.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 16,000 total flight cycles or within 3 months after the effective date of this AD, whichever occurs later. Replacement must be done prior to further flight if cracks are detected.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fokker Model F28 Mark 0100 series airplanes listed in Fokker Service Bulletin SBF100-57-018, dated September 23, 1993, certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.