AD 2004-15-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker | F27 Mark 100 | Airworthiness Directives; Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 Series Airplanes |
Unsafe Condition
Possible separation of the engine from the airplane due to insufficient structural integrity of the engine-to-wing load path.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 24 months after the effective date, perform a one-time general visual inspection to determine the part numbers of the engine mounting frames, brace struts, and attachment fittings. Take corrective action as specified in Fokker Service Bulletin F27/54-53 before further flight. Ensure that any installed engine mounting frames, brace struts, or attachment fittings are appropriate for the airplane configuration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 24 months after the effective date
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fokker Model F27 Mark 100, 200, 300, 400, 500, 600, and 700 series airplanes, certificated in any category, on which one or more of the modifications specified in Fokker Service Bulletin F27/54-53 (dated February 15, 2002) have been performed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.