# Airworthiness Directives; Raytheon Model DH.125, HS.125, BH.125, and BAe.125 (U-125 and C-29A) Series Airplanes; Model Hawker 800, Hawker 800 (U-125A), Hawker 800XP, and Hawker 1000 Airplanes
> **Rule** · Final rule; correction. · Published 2002-01-29 · Effective 2001-10-03 · 67 FR 4171
## Document
- **Document number:** 02-1966
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 67 FR 4171
- **Publication date:** 2002-01-29
- **Effective date:** 2001-10-03
- **FAA docket:** Docket No. 2000-NM-373-AD
## Abstract

This document corrects and clarifies information in an existing airworthiness directive (AD) that applies to certain Raytheon Model DH.125, HS.125, BH.125, and BAe.125 (U-125 and C-29A) series airplanes; Model Hawker 800, Hawker 800 (U-125A), Hawker 800XP, and Hawker 1000 airplanes. That AD currently requires an inspection for cracking or corrosion of the cylinder head lugs of the main landing gear actuator and follow-on/corrective actions. This document corrects and clarifies the affected airplane serial numbers. This correction is necessary to ensure that operators do not misinterpret which airplanes are subject to the requirements of this AD.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2002/01/29/02-1966/airworthiness-directives-raytheon-model-dh125-hs125-bh125-and-bae125-u-125-and-c-29a-series)
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