Airworthiness Directives; Kaman Aerospace Corporation Model K-1200 Helicopters
airworthiness · Rule · Final rule. · Published 2001-06-27 · 66 FR 34102
Document
Document number
01-16046
Federal Register citation
66 FR 34102
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Kaman Aerospace Corporation Model K-1200
Publication date
2001-06-27
FAA docket
Docket No. 2000-SW-50-AD
Abstract
This amendment adopts a new airworthiness directive (AD) for Kaman Aerospace Corporation (Kaman) Model K-1200 helicopters that requires reducing the life limit of the rotor shaft and teeter pin assembly and establishing a life limit for the flap clevis. This amendment is prompted by the discovery of cracks in parts that were returned to the manufacturer. The actions specified by this AD are intended to prevent failure of the rotor shaft, teeter pin assembly, or flap clevis due to fatigue cracks, and subsequent loss of control of the helicopter.