AD 81-15-07

Active

Tension-torsion Strap Assembly

Key Information
81-15-07
Active
August 25, 1981
Not specified
81-ASW-11
39-4164
Applicability
["Aircraft"]
["Rotorcraft"]
Kawasaki Heavy Industries, Limited
KV107-II KV107-IIA
Regulatory Text

81-15-07 KAWASAKI HEAVY INDUSTRIES, LTD. (KHI): Amendment 39-4164. Applies to Models KV107-II and KV107-IIA helicopters equipped with main rotor tension-torsion strap assemblies, P/N 107R2003-1, certificated in all categories (Airworthiness Docket No. 81-ASW-11).

Compliance required as indicated.

To prevent fatigue failure of the main rotor tension-torsion strap assemblies, remove from service tension-torsion strap assemblies, P/N 107R2003-1, on or before the accumulation of 27,800 hours' time in service and replace with a serviceable part that has less than 27,800 hours' total time in service.

This amendment becomes effective August 25, 1981.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents