AD 98-09-26
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault Aviation | FALCON 2000 | Airworthiness Directives; Dassault Model Falcon 2000 Series Airplanes |
Unsafe Condition
Fatigue cracking of the fuel line at the pressure switch pickoff point, which could result in fuel leakage and potential engine fire.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the Airplane Flight Manual (AFM) Limitations and Abnormal Procedures Sections to provide procedures for monitoring and setting fuel booster pump pressure; perform repetitive visual inspections of fuel lines for fatigue cracking and leakage; conduct a one-time dye penetrant inspection of fuel lines, replace discrepant parts, and install new brackets between the pressure switch and fuel pump of engines 1 and 2.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
AFM revision must be completed within 5 days; the one-time inspection and bracket installation must be accomplished within 45 days.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Dassault Model Falcon 2000 series airplanes with serial numbers 2 through 49 inclusive, and 51.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.