Airworthiness Directive

AD 2015-23-01 Amendment 39-18317

Federal Aviation Administration · 14 CFR part 39

FR document
2015-28313
Amendment
39-18317
Published
2015-11-10
Models covered
1
Last live check
Not yet re-verified
AD

2015-23-01

FR doc 2015-28313

AD 2015-23-01Published 2015-11-10Effective 2015-12-15

Requires repetitively inspecting and lubricating the tail rotor (T/R) driveshaft splined fittings.

Full official abstract

We are adopting a new airworthiness directive (AD) for Sikorsky Aircraft Corporation (Sikorsky) Model 269A, 269A-1, 269B, 269C, 269C-1, 269D, and TH-55A helicopters. This AD requires repetitively inspecting and lubricating the tail rotor (T/R) driveshaft splined fittings. This AD was prompted by a report that the T/R driveshaft can disconnect due to deterioration of the splined coupling. The actions are intended to detect and prevent excessive wear of the splined coupling, which could lead to failure of the T/R driveshaft and subsequent loss of control of the helicopter.

Applies to 1 model in our index