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Airworthiness Directive E7-19686

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AD E7-19686 · 2007-10-09 · turboshaft engine

Airworthiness Directives; Turbomeca S.A. Artouste III B, Artouste III B1, and Artouste III D Turboshaft Engines; Correction

What this AD requires

The FAA is correcting airworthiness directive (AD) 2007-19-11. That AD applies to Turbomeca S.A. Artouste III B, Artouste III B1, and Artouste III D turboshaft engines. We published that AD in the Federal Register on September 21, 2007 (72 FR 53937). The AD number of the superseded AD, is incorrect in two places in the preamble, and in one place in paragraph (b). This document corrects those AD numbers. In all other respects, the original document remains the same.

Which aircraft AD E7-19686 applies to

MakesTurbomeca S.A. Artouste Iii B, Artouste Iii B1, And Artouste Iii D Turboshaft

Whether AD E7-19686 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 compliance — The specific action taken (inspected, replaced, modified) and to what revision.
Date — When the work was done.
Aircraft time — Total time in service / tach at compliance — how recurring next-due is computed.
Signature & certificate — The A&P/IA who returned it to service, with certificate number.
Is AD E7-19686 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.