AD 86-03-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker Services | F.28 Mark 0070 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 0100 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 1000 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 2000 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 3000 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
| aircraft | Fokker Services | F.28 Mark 4000 | Airworthiness Directives; FOKKER B.V. Model F28 Airplanes |
Unsafe Condition
Failure of pilot and copilot restraint harnesses due to inertia reel spring and mounting collar degradation, and illegible instruction placards on the service/emergency door under emergency lighting conditions.
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Required Actions
Replace inertia reel springs and mounting collars per Fokker Service Bulletin F28/25-93 and Teleflex Morse Limited Service Bulletin 25-00-185429. Modify the emergency lighting system per Fokker Service Bulletin F28/33-32. Alternate means of compliance may be used if approved by the FAA.
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Compliance Time
within the next 120 days after the effective date of this airworthiness directive
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Affected Aircraft
Fokker B.V. Model F28 Mark 0070, 0100, 1000, 2000, 3000, 4000 airplanes as indicated in the applicability statement of each service bulletin listed in this AD.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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