Airworthiness Directives; Raytheon Model Hawker 800XP and 800 (Including Variant U-125A) Airplanes
airworthiness · Rule · Final rule. · Published 2003-03-26 · Effective 2003-04-30 · 68 FR 14530
Document
Document number
03-6966
Federal Register citation
68 FR 14530
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Raytheon Model Hawker 800XP and 800 (Including Variant U-125A)
Publication date
2003-03-26
Effective date
2003-04-30
FAA docket
Docket No. 2001-NM-18-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Raytheon Model Hawker 800XP and 800 (including variant U-125A) airplanes, that requires a one-time inspection to identify the bolts installed at certain locations in the wing or fuselage, and corrective actions if necessary. The actions specified by this AD are intended to prevent failure of certain attachment bolts due to manufacturing discrepancies, which could result in reduced structural integrity of the airplane, and loss of system function for flaps, controls, and landing gear. This action is intended to address the identified unsafe condition.