AD 87-26-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker Services | F.28 Mark 0070 | Airworthiness Directives; FOKKER B.V. Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 0100 | Airworthiness Directives; FOKKER B.V. Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 1000 | Airworthiness Directives; FOKKER B.V. Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 2000 | Airworthiness Directives; FOKKER B.V. Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 3000 | Airworthiness Directives; FOKKER B.V. Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 4000 | Airworthiness Directives; FOKKER B.V. Model F-28 Series Airplanes |
Unsafe Condition
Failure of a cargo door hinge lugs could cause sudden decompression of the airplane.
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Required Actions
Visually or dye penetrant inspect the cargo door hinge lugs for cracks in accordance with Fokker Service Bulletin F28/52-a/100, Revision 1. Replace any cracked lugs with a serviceable part prior to further flight. An alternate means of compliance or adjustment of compliance time may be used with FAA concurrence.
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Compliance Time
within 120 flight hours after the effective date of this AD
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Affected Aircraft
FOKKER B.V. Model F-28 series airplanes as listed in Service Bulletin F28/52-a/100, Revision 1, dated June 19, 1987
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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