Airworthiness Directives; Bell Helicopter Textron Canada Limited Model 206L, L-1, L-3, and L-4 Helicopters
airworthiness · Rule · Final rule. · Published 2002-12-23 · Effective 2003-01-27 · 67 FR 78153
Document
Document number
02-31752
Federal Register citation
67 FR 78153
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2002-12-23
Effective date
2003-01-27
FAA docket
Docket No. 99-SW-80-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron Canada Limited (BHTCL) model helicopters that currently requires removing the horizontal stabilizer supports and inspecting the edges of the tailboom skins around the horizontal stabilizer openings for a crack. This amendment requires checking and inspecting the tailboom for a crack and modifying or replacing the tailboom as necessary. This amendment also provides a terminating action, incorporates a more recent alert service bulletin (ASB), and increases the compliance time for performing the inspections. This amendment is prompted by several reports of cracks found during mandatory inspections. The actions specified by this AD are intended to detect a crack in the tailboom skin and to prevent separation of the tailboom and subsequent loss of control of the helicopter.