Airworthiness Directive 2018-02994

one-time
AD 2018-02994 · 2018-02-14 · turboprop engine

Airworthiness Directives; GE Aviation Czech s.r.o. Turboprop Engines

What this AD requires

We are adopting a new airworthiness directive (AD) for GE Aviation Czech s.r.o. M601D-11, M601E-11, M601E-11A, M601E-11AS, M601E- 11S, and M601F turboprop engines. This AD requires removal of certain power turbine (PT) disks installed on the affected engines. This AD was prompted by a design review by the manufacturer that determined PT rotors with certain disks have less overspeed margin than originally stated during product certification. We are issuing this AD to address the unsafe condition on these products.

Which aircraft AD 2018-02994 applies to

MakesGe Aviation Czech S.R.O.
ModelsM601D-11, M601E-11, M601E-11A, M601E-11AS, M601E-11S, M601F, M601
Part-conditionalM601-3220.6, M601-3220.7.

Applies to engines with power turbine (PT) rotors with disks, P/N M601-3220.6 or P/N M601-3220.7, installed.

Whether AD 2018-02994 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 2018-02994 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.