AD 94-26-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker Services | F27 Mark 100 | Airworthiness Directives; Fokker Model F27 Series Airplanes |
| aircraft | Fokker Services | F27 Mark 200 | Airworthiness Directives; Fokker Model F27 Series Airplanes |
| aircraft | Fokker Services | F27 Mark 300 | Airworthiness Directives; Fokker Model F27 Series Airplanes |
| aircraft | Fokker Services | F27 Mark 400 | Airworthiness Directives; Fokker Model F27 Series Airplanes |
| aircraft | Fokker Services | F27 Mark 500 | Airworthiness Directives; Fokker Model F27 Series Airplanes |
| aircraft | Fokker Services | F27 Mark 600 | Airworthiness Directives; Fokker Model F27 Series Airplanes |
| aircraft | Fokker Services | F27 Mark 700 | Airworthiness Directives; Fokker Model F27 Series Airplanes |
Unsafe Condition
Fatigue cracking and corrosion in transport category airplanes that are approaching or have exceeded their economic design goal, which have jeopardized the airworthiness of the affected airplanes.
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Required Actions
Accomplish structural modifications specified in Fokker Service Bulletins, including modifications of upper stringers in the outer wing prior to January 1, 1996 for airplanes with over 30,000 total landings, and perform x-ray inspections until modified or by the compliance date.
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Compliance Time
Prior to January 1, 1996 for airplanes with more than 30,000 total landings, with an x-ray inspection required before that date if not modified.
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Affected Aircraft
Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 airplanes.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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