Airworthiness Directive 2018-10-01

one-time
Official AD 2018-10-01 · FR doc 2018-09466 · 2018-05-07 · turboshaft engine

Airworthiness Directives; Safran Helicopter Engines, S.A., Turboshaft Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A., Arriel 2E turboshaft engines. This AD was prompted by reports of ruptured front support pins on the accessory gearbox front support. This AD requires replacement of the accessory gearbox front support. We are issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2018-10-01 applies to

MakesSafran Helicopter Engines
ModelsArriel 2E, Arriel
Part-conditional0 292 11 715 0.

Applies to engines with front support, P/N 0 292 11 715 0, installed (pre-mod TU 197 configuration).

Whether AD 2018-10-01 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 2018-10-01 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.