Airworthiness Directive 2010-18-02

one-time
Official AD 2010-18-02 · FR doc 2010-21058 · 2010-08-25 · reciprocating engine

Airworthiness Directives; Thielert Aircraft Engines GmbH (TAE) Models TAE 125-01 and TAE 125-02-99 Reciprocating Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:

Which aircraft AD 2010-18-02 applies to

MakesThielert Aircraft Engines Gmbh (Tae)
ModelsTAE 125-01, TAE 125-02-99, TAE 125
Part-conditional02-7210-11001R13, 05-7211-K006001, 05-7211-K006002.

Applies to all serial numbers of TAE 125-01 (Centurion 1.7) engines if clutch assembly P/N 02-7210-11001R13 is installed, and all serial numbers of TAE 125-02-99 (Centurion 2.0) engines if clutch assembly P/N 05-7211-K006001 or P/N 05-7211-K006002 is installed. Installed on, but not limited to, Cessna 172 and (Reims-built) F172 series, Piper PA-28 series, APEX (Robin) DR 400 series, and Diamond Aircraft Industries Models DA40 and DA42 airplanes.

Whether AD 2010-18-02 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:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD 2010-18-02 complied with on your aircraft?

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.