AD 88-05-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker Services | F.28 Mark 0070 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 0100 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 1000 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 2000 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 3000 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 4000 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
Unsafe Condition
Reduced directional control capability due to insufficient stops in the rudder pedal mechanism.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install stops in the rudder pedal mechanism per Fokker Service Bulletin F28/27-158 within six months after the effective date. Alternate means of compliance may be approved by the Manager, Standardization Branch, ANM-113.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within six months after the effective date of this AD
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Affected Aircraft
Fokker Aircraft Model F-28 series airplanes, Serial Numbers 11003 to 11231 inclusive, 11991 and 11992
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
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