Airworthiness Directives; GE Aviation Czech s.r.o. Turboprop Engines
airworthiness · Rule · Final rule. · Published 2015-07-14 · Effective 2015-08-18 · 80 FR 40897
Document
Document number
2015-16584
Federal Register citation
80 FR 40897
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
GE Aviation Czech s.r.o. Turboprop
Publication date
2015-07-14
Effective date
2015-08-18
FAA docket
Docket No. FAA-2015-0482
Abstract
We are adopting a new airworthiness directive (AD) for certain serial number GE Aviation Czech s.r.o. M601E-11, M601E-11A, and M601F turboprop engines. This AD requires inspection of the reduction gearbox and supporting cone. This AD was prompted by the determination that wear or cracking, and subsequent misalignment of the quill shaft of the engine and the power turbine (PT) shaft, may lead to rupture of the quill shaft, overspeed of the PT, and uncontained engine failure. We are issuing this AD to prevent misalignment and rupture of the quill shaft, which could lead to overspeed of the PT, uncontained engine failure, and damage to the airplane.