airworthiness · Rule · Final rule. · Published 2017-03-31 · Effective 2017-05-05 · 82 FR 15982
Document
Document number
2017-05857
Federal Register citation
82 FR 15982
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
M7 Aerospace LLC Models
Publication date
2017-03-31
Effective date
2017-05-05
FAA docket
Docket No. FAA-2016-9531
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.