# Airworthiness Directives; Cessna Aircraft Company Model CESSNA 441 Airplanes
> **Rule** · Final rule; request for comments. · Published 2002-05-09 · Effective 2002-05-31 · 67 FR 31117
## Document
- **Document number:** 02-11523
- **Category:** airworthiness
- **Manufacturer:** Cessna
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 67 FR 31117
- **Publication date:** 2002-05-09
- **Effective date:** 2002-05-31
- **FAA docket:** Docket No. 2002-CE-17-AD
## 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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2002/05/09/02-11523/airworthiness-directives-cessna-aircraft-company-model-cessna-441-airplanes)
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