Airworthiness Directive

AD 2017-07-01 Amendment 39-18839

Federal Aviation Administration · 14 CFR part 39

FR document
2017-05857
Amendment
39-18839
Published
2017-03-31
Models covered
1
Last live check
Not yet re-verified
AD

2017-07-01

FR doc 2017-05857

AD 2017-07-01Published 2017-03-31Effective 2017-05-05

Requires repetitively inspecting the propeller pitch control for proper torque, with corrections as necessary until required replacement or rework of the PPC assembly to have a threaded hole in the splined end of the shouldered…

Full official abstract

We are adopting a new airworthiness directive (AD) for certain M7 Aerospace LLC Models SA226-T, SA226-AT, SA226-T(B), SA226-TC, SA227- AC (C-26A), SA227-AT, SA227-BC (C-26A), SA227-CC, SA227-DC (C-26B), and SA227-TT airplanes. This AD was prompted by detachment of the power lever linkage to the TPE331 engine propeller pitch control. This AD requires repetitively inspecting the propeller pitch control for proper torque, with corrections as necessary until required replacement or rework of the PPC assembly to have a threaded hole in the splined end of the shouldered shaft and installation of a secondary retention device is done. We are issuing this AD to correct the unsafe condition on these products.

Applies to 1 model in our index