Airworthiness Directive

AD 2015-17-20 80 FR 51935 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2015-21119
Amendment
39-18253
Published
2015-08-27
Effective
2015-10-01
Models covered
1
Last live check
2026-10-02
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AD

2015-17-20

FR doc 2015-21119 · 80 FR 51935

AD 2015-17-20Published 2015-08-27Effective 2015-10-01

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires removing from service any affected engine with certain GGT blades installed.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain serial number (S/N) GE Aviation Czech s.r.o. M601E-11, M601E-11A, and M601F turboprop engines with certain part number (P/N) gas generator turbine (GGT) blades, installed. This AD requires removing from service any affected engine with certain GGT blades installed. This AD was prompted by the determination that certain GGT blades are susceptible to blade failure. We are issuing this AD to prevent GGT blade failure, which could lead to engine failure and loss of the airplane.

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All GE Aviation Czech M601/H80 directives

Applies to 1 model in our index