Airworthiness Directives; General Electric Company CF34-8C1/-8C5/-8C5B1/-8E5/-8E5A1, and CF34-10E Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 2008-02-28 · Effective 2008-04-03 · 73 FR 10647
Document
Document number
E8-3462
Federal Register citation
73 FR 10647
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2008-02-28
Effective date
2008-04-03
FAA docket
Docket No. FAA-2007-29001
Abstract
The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF34-8C1/-8C5/-8C5B1/-8E5/-8E5A1, and CF34-10E series turbofan engines with certain part number (P/N) and serial number (SN) fuel metering units (FMU) installed. This AD requires a onetime test of the FMU for a miswired (reversed polarity) condition of the input wires to the overspeed solenoid. This AD results from the discovery of miswired FMU overspeed solenoids in the field. We are issuing this AD to prevent the engine from failing to shutdown during an overspeed which may lead to uncontained engine failure.