Is AD 2016-06-09 a recurring Airworthiness Directive?

No — AD 2016-06-09 is a one-time directive. Verify it was complied with in the aircraft's records.

Which aircraft does AD 2016-06-09 apply to?

AD 2016-06-09 applies to Turbomeca — models Makila 2A, Makila 2A1, Makila. Serial/part conditions may narrow it to specific aircraft.

Airworthiness Directive 2016-06-09

one-time

Official AD 2016-06-09 · FR doc 2016-06372 · 2016-03-22 · turboshaft engine

Airworthiness Directives; Turbomeca S.A. Turboshaft Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for certain Turbomeca S.A. Makila 2A and 2A1 turboshaft engines. This AD requires tightening the nut attaching the swivel union to the engine power turbine module M04. This AD was prompted by two occurrences of commanded in-flight shutdown following low oil pressure warning. We are issuing this AD to prevent loosening of the nut and oil leakage from the low-pressure oil system, which could lead to in-flight shutdown of the engine and forced landing.

Which aircraft AD 2016-06-09 applies to

MakesTurbomeca

ModelsMakila 2A, Makila 2A1, Makila

Applies only to engines that have incorporated Turbomeca S.A. Service Bulletin No. 298 79 2831, Version B, dated Nov 13, 2015, or earlier.

Whether AD 2016-06-09 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 2016-06-09 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.