Airworthiness Directives; Bell Helicopter Textron Canada Model 206A, B, L, L-1, L-3, and L-4 Helicopters
airworthiness · Rule · Final rule; request for comments. · Published 2004-12-01 · Effective 2004-12-16 · 69 FR 69810
Document
Document number
04-26425
Federal Register citation
69 FR 69810
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2004-12-01
Effective date
2004-12-16
FAA docket
Docket No. 2004-SW-12-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) model helicopters. This action requires an initial inspection and, at specified intervals, certain repetitive checks and inspections of the tail rotor blade (blade) for a deformation, a crack, and a bent or deformed tail rotor weight (weight). Also, this action requires, before further flight, replacing each blade with an airworthy blade if a deformation, a crack, or a bent or deformed weight is found. This amendment is prompted by three reports of skin cracks originating near the blade trailing edge balance weight. This condition, if not detected, could result in blade failure and subsequent loss of control of the helicopter.