AD 2004-15-08
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 lead to structural failure and compromise the integrity of the airplane.
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Required Actions
Revise the Airworthiness Limitations section of the Instructions for Continued Airworthiness to incorporate updated Airworthiness Limitation Items, Safe Life Items, and Certification Maintenance Requirements. The revision must include Fokker Services B.V. Report SE-623, Issue 2, dated September 1, 2001, and Report SE-473, Issue 5, dated July 16, 2001.
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Compliance Time
Within 6 months after the effective date of this AD (August 31, 2004).
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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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