Airworthiness Directives; General Electric Company (GE) CF34-1A, CF34-3A, and CF34-3B Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2009-11-30 · Effective 2010-01-04 · 74 FR 62481
Document
Document number
E9-28236
Federal Register citation
74 FR 62481
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2009-11-30
Effective date
2010-01-04
FAA docket
Docket No. FAA-2009-0328
Abstract
The FAA is adopting a new airworthiness directive (AD) for GE CF34-1A, CF34-3A, and CF34-3B series turbofan engines. This AD requires removing from service certain part number (P/N) and serial number (SN) fan blades within compliance times specified in this AD, inspecting the fan blade abradable rub strip on certain engines for wear, inspecting the fan blades on certain engines for cracks, inspecting the aft actuator head hose fitting for correct position, and, if necessary, repositioning the hose fitting. This AD results from a report of an under-cowl fire and a failed fan blade. We are issuing this AD to prevent failure of certain P/N and SN fan blades and aft actuator head hoses, which could result in an under-cowl fire and subsequent damage to the airplane.