# Airworthiness Directives; Raytheon Model Hawker 800XP and Hawker 800 (U-125A) Series Airplanes
> **Rule** · Final rule. · Published 2000-11-14 · Effective 2000-12-19 · 65 FR 68069
## Document
- **Document number:** 00-28479
- **Category:** airworthiness
- **Manufacturer:** Raytheon Model Hawker 800XP and Hawker 800 (U-125A) Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 68069
- **Publication date:** 2000-11-14
- **Effective date:** 2000-12-19
- **FAA docket:** Docket No. 2000-NM-46-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Raytheon Model Hawker 800XP and Hawker 800 (U- 125A) series airplanes, that requires inspection of the wire bundle to relay "KT" on panel "JA" for correct routing, adequate clearance from the fuel cross-feed valve operating lever, and the presence of chafing; this amendment also requires corrective action, if necessary. The actions specified by this AD are intended to detect and correct chafing of the wire bundle exiting panel "JA" due to insufficient clearance from the fuel cross-feed valve operating lever. Such chafing of the wire bundle could result in a fire in the area of the fuel system in a confined space. This action is intended to address the identified unsafe condition.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/11/14/00-28479/airworthiness-directives-raytheon-model-hawker-800xp-and-hawker-800-u-125a-series-airplanes)
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