Airworthiness Directive 2001-08-14

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Official AD 2001-08-14 · FR doc 01-11456 · 2001-05-08 · turboshaft engine

Airworthiness Directives: Turbomeca S.A. Arrius Models 2B, 2B1, and 2F Turboshaft Engines; Correction

What this AD requires

This document makes a correction to Airworthiness Directive (AD) 2001-08-14 applicable to Turbomeca S.A. Arrius models 2B, 2B1, and 2F turboshaft engines, that was published in the Federal Register on April 26, 2001 (66 FR 20910). The amendment number of 39-12191 used in this AD is incorrect. This document corrects that amendment number. In all other respects, the original document remains the same.

Which aircraft AD 2001-08-14 applies to

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Whether AD 2001-08-14 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 2001-08-14 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.