AD 2001-21-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker | F | Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Series Airplanes |
Unsafe Condition
Fatigue cracking of certain structural elements could adversely affect the structural integrity of the airplanes.
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Required Actions
Revise the Airworthiness Limitations Section (ALS) of the Instructions for Continued Airworthiness to incorporate Report SE-623, 'Fokker 70/100 Airworthiness Limitation Items and Safe Life Items,' dated June 1, 2000. No alternative inspections or intervals may be approved for the specified structural elements after this revision.
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Compliance Time
Within 30 days after the effective date of the AD.
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Affected Aircraft
All Fokker Model F.28 Mark 0070 and 0100 series airplanes, certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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