Airworthiness Directive 2010-17-08

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Official AD 2010-17-08 · FR doc 2010-19840 · 2010-08-18 · airframe

Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series 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 2010-17-08 applies to

MakesAeromot-Industria Mecanico Metalurgica LtdaDiamond Aircraft IndustriesDiamond Aircraft Industries GmbhDiamond Aircraft Industries Inc.Hoac-AustriaIniziative Industriali Italiane S.P.A.Scheibe-Flugzeugbau Gmbh
ModelsAMT-200, HK 36 R Super Dimona, HK 36 TS, HK 36 TC, DA20-A1, DV 20 Katana, Sky Arrow 650 TC, SF 25C, HK 36, DA20, DV 20, Sky Arrow 650, SF 25
Part-conditional892230, 892232, 892540, 892235, 892236, 892545.

Applies to all serial numbers of the listed aircraft, certificated in any category, equipped with a Rotax Aircraft Engines 912 A series engine (912 A2 or 912 A3) with a fuel pump of one of the listed part numbers installed: P/Ns 892230, 892232, or 892540 (standard version), or P/Ns 892235, 892236, or 892545 (version including flexible fuel line). Type certificate holder/model/engine pairings: Aeromot-Industria Mecanico Metalurgica Ltda AMT-200 (912 A2); Diamond Aircraft Industries HK 36 R Super Dimona (912 A) and HK 36 TS (912 A3); Diamond Aircraft Industries GmbH HK 36 TC (912 A3); Diamond Aircraft Industries Inc. DA20-A1 (912 A3); HOAC-Austria DV 20 Katana (912 A3); Iniziative Industriali Italiane S.p.A. Sky Arrow 650 TC (912 A2); SCHEIBE-Flugzeugbau GmbH SF 25C (912 A2 or 912 A3).

Whether AD 2010-17-08 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 2010-17-08 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.