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NSN 2910-00-659-0542 (2910006590542) Governor Turbine En Parts List

Alternative NSN: 2910-00-659-0542
Item Name:Governor Turbine En
FSG: 29 Engine Accessories
Federal Supply Class (FSC): 2910 Engine Fuel System Components Nonaircraft
NIIN: 006590542
NCB Code: USA (00)
Manufacturers: Alamo Aircraft Ltd , Hamilton Sundstrand Corporation , Solar Turbines Inc

ASAP Aerospace, owned and operated by ASAP Semiconductor, is the latest parts procurement platform for the aerospace and aviation industry. Customers can easily search our database to find NSN parts like Governor Turbine En 21616, 21616, 21616 of Solar Turbines Inc, Hamilton Sundstrand Corporation, Alamo Aircraft Ltd with NSN 2910-00-659-0542.

NSN 2910-00-659-0542, National Stock Number, is a 13-digit serial number assigned by the US DLA to an item that is bought, stored, and sold via the federal supply chain. Unlike part numbers, NSNs are not arbitrary and follow a specific classification system.


Part Number List for NSN 2910006590542

  • Part No Item Name Manufacturer QTY RFQ
    21616 Governor Turbine En Solar Turbines Inc Avl RFQ
    21616 Governor Turbine En Hamilton Sundstrand Corporation Avl RFQ
    21616 Governor Turbine En Alamo Aircraft Ltd Avl RFQ

Characteristics Data of NSN 2910006590542

MRCCriteriaCharacteristic
AMYNGovernor TypeCENTRIFUGAL
AGAVEnd Item IdentificationT41-9A AND T45M-13 GAS TURBINE ENGINES
AAXXMounting TypeFLANGE
ZZZVFsc Application DataFUEL SYSTEM,GAS TURBINE ENGINE,NONAIRCRAFT"
ASFCHydraulic ControlNOT INCLUDED
ASFESpark ControlNOT INCLUDED
ASFFSpeed Control TypeCONSTANT WITH OVERSPEED SHUTOFF
ASHDLever For Manual OperationNOT INCLUDED
RDALReference Data And LiteratureT.O.2G-T41M-4,FIG.11"
AJABDrive Shaft TypeSPLINED
AKCVDrive TypeGEAR
FEATSpecial FeaturesIMANUFACTURES SUGGESTED NAME - CONTROL ASSEMBLY,SPEED;C/O FUEL PUMP P/N 18518 (1),GOVERNOR P/N 21615 (1),GASKET P/N AN4045-1 (1),DRIVE SCREW P/N AN5350-4 (2),WASHER P/N AN960416L (4),NUT P/N AN310-4 (4)"
FTLDFunctional DescriptionA FUEL METERING DEVICE SPECIFICALLY DESIGNED TO BE USED ON A GAS TURBINE ENGINE THAT METERS THE PROPER QUANTITY OF FUEL TO BE FED INTO THE BURNERS OF THE ENGINE.IT INTEGERATES THE PARAMETERS OF INLET AIR TEMPERATURE,COMPRESSOR SPEED,COMPRESSOR DISCHARGE PRESSURE, EXHAUST GAS TEMPERATURE, AND THE ENGINE CONTROL UNIT"
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