Airworthiness Directive

AD 2016-04-04 Amendment 39-18398

Federal Aviation Administration · 14 CFR part 39

FR document
2016-03171
Amendment
39-18398
Published
2016-03-04
Models covered
1
Last live check
Not yet re-verified
AD

2016-04-04

FR doc 2016-03171

AD 2016-04-04Published 2016-03-04Effective 2016-04-08

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.

Full official 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.

Applies to 1 model in our index