AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2002-09-13 67 FR 31117 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-11523
Amendment
39-12746
Published
2002-05-09
Effective
2002-05-31
Models covered
1
Last live check
2026-09-30

Printed from https://aircraftdirectives.com/ad/2002-09-13 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2002-09-13

FR doc 02-11523 · 67 FR 31117

AD 2002-09-13Published 2002-05-09Effective 2002-05-31

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires you to do a one-time inspection of the fuel boost pump wiring inside and outside the boost pump reservoir, and repair or replace the wiring as necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Cessna Aircraft Company (Cessna) Model CESSNA 441 airplanes. This AD requires you to do a one-time inspection of the fuel boost pump wiring inside and outside the boost pump reservoir, and repair or replace the wiring as necessary. This AD is the result of several reports of chafing and/or arcing of the fuel boost pump wiring inside and outside the fuel pump reservoir. The actions specified by this AD are intended to detect and correct chafing and/or arcing boost pump wiring, which could result in arcing within the wing fuel storage system. Such failure could lead to ignition of explosive vapor within the fuel storage system.

More directives for Cessna 425/441 Conquest

  1. AD 2018-03-03 R1 Airworthiness Directives; Textron Aviation Inc. Airplanes 2018-05-08
  2. AD 2018-03-03 Airworthiness Directives; Textron Aviation Inc. Airplanes 2018-02-13
  3. AD 2005-20-25 Airworthiness Directives; The Cessna Aircraft Company Models 401, 401A, ... 2005-10-12
  4. AD 2003-09-09 R1 Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Ai... 2004-01-12
  5. AD 2003-09-09 Airworthiness Directives; Cessna Aircraft Company Models 441 and F406 Ai... 2003-05-01

All Cessna 425/441 Conquest directives

View on Federal Register (opens in a new tab) Search DRS manually for AD 2002-09-13 (opens in a new tab)

Applies to 1 model in our index