AD 2003-09-09 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | Reims Aviation S.A. | 441 | Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Airplanes |
| aircraft | Cessna Aircraft Company | Reims Aviation S.A. | F406 | Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Airplanes |
Unsafe Condition
Chafing and/or arcing of the fuel boost pump wiring could result in arcing within the wing fuel storage system, leading to ignition of explosive vapor within the fuel storage system.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Repetitively inspect the fuel boost pump wiring inside and outside the boost pump reservoir and repair or replace the wiring as necessary. Eventually install an improved design wire harness and fuel boost pump or install protective sleeving modification for boost pump lead wires as terminating actions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Initially within the next 25 hours time-in-service or 60 days after May 31, 2002, whichever occurs first. Repetitive inspections every 200 hours time-in-service thereafter.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Aircraft Company and Reims Aviation S.A. Models 441 and F406 airplanes affected by AD 2002-09-13 or subsequent ADs.
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
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