Document

Airworthiness Directives; M7 Aerospace LLC Airplanes

We propose to adopt 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)...

We propose to adopt 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 proposed AD was prompted by detachment of the power lever linkage to the TPE331 engine propeller pitch control. This proposed AD would require installing a secondary retention device and repetitively inspecting the propeller pitch control for proper torque, with corrections as necessary. We are proposing this AD to correct the unsafe condition on these products.

Legal Citation

Federal Register Citation

Use this for formal legal and research references to the published document.

81 FR 95528

Web Citation

Suggested Web Citation

Use this when citing the archival web version of the document.

“Airworthiness Directives; M7 Aerospace LLC Airplanes,” thefederalregister.org (December 28, 2016), https://thefederalregister.org/documents/2016-30292/airworthiness-directives-m7-aerospace-llc-airplanes.