Airworthiness Directives; Enstrom Helicopter Corporation Model TH-28 and 480 Helicopters
airworthiness · Rule · Final rule. · Published 2001-12-11 · 66 FR 63915
Document
Document number
01-30499
Federal Register citation
66 FR 63915
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Enstrom Helicopter Corporation Model TH-28 and 480
Publication date
2001-12-11
FAA docket
Docket No. 2001-SW-27-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for Enstrom Helicopter Corporation (EHC) Model TH-28 and 480 helicopters. This AD requires establishing a life limit for certain upper and lower main rotor hub plates of 5000 hours time-in-service (TIS), creating a component history card or equivalent record, and replacing each main rotor hub plate (hub plate) having 5000 or more hours TIS with an airworthy hub plate. This AD is prompted by a recent reliability-based stress analysis that indicates a 5000-hour TIS life limit should be imposed on certain hub plates. The actions specified by this AD are intended to prevent failure of a hub plate, loss of control of the main rotor, and subsequent loss of control of the helicopter.