Airworthiness Directives; Piper Aircraft, Inc. Model PA-28-161 Airplanes
airworthiness · Rule · Final rule. · Published 2010-12-28 · Effective 2011-02-01 · 75 FR 81417
Document
Document number
2010-31905
Federal Register citation
75 FR 81417
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Piper
Publication date
2010-12-28
Effective date
2011-02-01
FAA docket
Docket No. FAA-2010-1006
Abstract
We are adopting a new airworthiness directive (AD) for the products listed above that are equipped with Thielert Aircraft Engine GmbH (TAE) Engine Model TAE-125-01 installed per Supplemental Type Certificate (STC) No. SA03303AT. This AD requires installing a full authority digital engine control (FADEC) backup battery, replacing the supplement pilot's operating handbook and FAA approved airplane flight manual, and revising the limitations section of the supplement airplane maintenance manual. This AD was prompted by an incident where an airplane experienced an in-flight engine shutdown caused by a momentary loss of electrical power to the FADEC. We are issuing this AD to prevent interruption of electrical power to the FADEC, which could result in an uncommanded engine shutdown. This failure could lead to a loss of engine power.