Airworthiness Directive 2012-26-13
one-timeAirworthiness Directives; Thielert Aircraft Engines GmbH Reciprocating Engines
What this AD requires
We are superseding an existing airworthiness directive (AD) for all Thielert Aircraft Engines GmbH models TAE 125-01, TAE 125-02- 99, and TAE 125-02-114 reciprocating engines. That AD currently requires installation of full-authority digital electronic control (FADEC) software version 2.91. This new AD requires removing all software mapping versions prior to 292, 301, or 302, applicable to the TAE engine model. This AD was prompted by reports of possible power loss on airplanes equipped with TAE 125 engines. We are issuing this AD to prevent engine power loss or in-flight shutdown, resulting in reduced control of or damage to the airplane.
Which aircraft AD 2012-26-13 applies to
Installed in, but not limited to, Cessna 172 and (Reims-built) F172 series airplanes (EASA STC No. EASA.A.S.01527); Piper PA-28 series airplanes (EASA STC No. EASA.A.S.01632); APEX (Robin) DR 400 series airplanes (EASA STC No. A.S.01380); and Diamond Aircraft Industries DA 40, DA 42, and DA 42M NG airplanes.
Whether AD 2012-26-13 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.