[Note: Preliminary Copy as received by Aircraft Technical
AD: 2001-13-03 R1 Kaman Aerospace Corporation: Amendment 39-13123. Docket No.
Revises AD 2001-13-03, Amendment 39-12283, Docket No.
Applicability: Model K-1200 helicopters,
certificated in any category.
Compliance: 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
Special flight permits will not be issued.
This amendment becomes effective on May 27, 2003.