Airworthiness Directives; General Electric Company (GE); CT7-2D1 Turboshaft Engines.
airworthiness · Rule · Final rule; request for comments. · Published 2004-08-06 · Effective 2004-08-23 · 69 FR 47763
Document
Document number
04-17755
Federal Register citation
69 FR 47763
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2004-08-06
Effective date
2004-08-23
FAA docket
Docket No. FAA-2004-18758
Abstract
The FAA is adopting a new airworthiness directive (AD) for GE CT7-2D1 turboshaft engines. This AD requires replacing certain turbine stage 2 aft cooling plates, part number (P/N) 6064T0P02. This AD results from an uncontained failure of a turbine stage 2 aft cooling plate in a GE CT7 turboprop engine. We are issuing this AD to prevent a similar uncontained failure of turbine stage 2 aft cooling plates in GE CT7-2D1 turboshaft engines.