Airworthiness Directives; Bell Helicopter Textron Canada Model 407 Helicopters
airworthiness · Rule · Final rule. · Published 2005-02-10 · Effective 2005-03-17 · 70 FR 7016
Document
Document number
05-2589
Federal Register citation
70 FR 7016
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bell Helicopter Textron Canada Model 407
Publication date
2005-02-10
Effective date
2005-03-17
FAA docket
Docket No. 2004-SW-07-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada (Bell) Model 407 helicopters that requires creating a component history card or equivalent record for each crosstube assembly, converting accumulated run-on landings to an accumulated Retirement Index Number (RIN) count, and establishing a maximum accumulated RIN for certain crosstube assemblies. This amendment is prompted by fatigue testing, analysis, and evaluation by the manufacturer that determined that run-on landings impose a high stress on landing gear or crosstubes and may cause cracking in the area above the skid tube saddle. The actions specified by this AD are intended to prevent fatigue failure in a crosstube assembly due to excessive stress during run-on landings and subsequent loss of control of the helicopter.