Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, and 230 Helicopters
airworthiness · Rule · Final rule. · Published 2004-10-05 · Effective 2004-11-09 · 69 FR 59541
Document
Document number
04-22265
Federal Register citation
69 FR 59541
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-10-05
Effective date
2004-11-09
FAA docket
Docket No. 2004-SW-04-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) model helicopters that requires certain inspections of the main rotor yoke (yoke) for a crack, fretting, or buffer deterioration. If a crack is found, the AD requires replacing the yoke with an airworthy yoke before further flight. If fretting or buffer deterioration are found, the AD requires further inspecting the main rotor hub assembly (hub assembly) and repairing or replacing any unairworthy parts. Also, the AD requires a torque inspection of the flapping bearing retaining nuts at specified intervals. This amendment is prompted by the discovery of a crack in a yoke. The actions specified by this AD are intended to prevent failure of the yoke and subsequent loss of control of the helicopter.