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
airworthiness · Rule · Final rule; correction. · Published 2002-01-29 · Effective 2001-10-03 · 67 FR 4171
Document
Document number
02-1966
Federal Register citation
67 FR 4171
Type
Rule
Action
Final rule; correction.
Category
airworthiness
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.