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Airworthiness Directives; M7 Aerospace LLC Airplanes

airworthiness · Rule · Final rule. · Published 2016-03-04 · Effective 2016-04-08 · 81 FR 11409

Document

Document number
2016-03171
Federal Register citation
81 FR 11409
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
M7 Aerospace LLC
Publication date
2016-03-04
Effective date
2016-04-08
FAA docket
Docket No. FAA-2015-3607

Abstract

We are adopting a new airworthiness directive (AD) for all M7 Aerospace LLC Models SA26-AT, SA226-T(B), SA226-AT, SA226-T, 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 information that the airplane flight manual (AFM) does not provide adequate guidance in the handling of engine failures, which may lead to reliance on the negative torque system (NTS) for reducing drag. This condition could lead the pilot to not fully feather the propeller with consequent loss of control. This AD requires inserting updates into the airplane flight manual (AFM) and/or the pilot operating handbook (POH) that will clearly establish that the NTS is not designed to automatically feather the propeller but only to provide drag protection. We are issuing this AD to correct the unsafe condition on these products.

Source

Authoritative
Federal Register document
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