Item Name | Case Fan Aircraft Gas Turbine En |
Federal Supply Group (FSG) | Engines Turbines and Components |
Federal Supply Class (FSC) | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
National Item Identification Number (NIIN) | 01-167-2923 (011672923) |
NCB Code | USA (01) |
Manufacturer | General Electric Company |
Part Number | Manufacturer | Item Name | RFQ |
---|---|---|---|
9397M40 | general electric company | case fan aircraft gas turbine en | RFQ |
9397M40G01 | general electric company | case fan aircraft gas turbine en | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 23.433 INCHES MINIMUM AND 23.453 INCHES MAXIMUM |
ABMZ | DIAMETER | 95.930 INCHES MINIMUM AND 95.950 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ACFT ENG TF39 |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE AND NOZZLE ASSEMBLY,TURBINE,AIRCRAFT |
CZBJ | ENGINE SECTION LOCATION | FAN |
FEAT | SPECIAL FEATURES | 2ND STAGE; 1 PIECE EXTRUDED CASE REPLACED P/N 1288M61G01 AND REWORKED TO P/N 9397M40G02 |
MATT | III MATERIAL | ALUMINUM ALLOY OVERALL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS4150 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF39-4, FIG 38, IND 3 |
Relevant Components for NSN - 2840-01-167-2923, 2840011672923 | ||||
2825-00-790-8901 (2825007908901) | 2825-01-010-8535 (2825010108535) | 2825-00-371-7811 (2825003717811) | 2805-01-264-5598 (2805012645598) | |
2840-01-375-6452 (2840013756452) | 2805-01-130-2594 (2805011302594) | 2835-01-234-6845 (2835012346845) | 2805-01-714-1073 (2805017141073) | |
2840-00-837-2120 (2840008372120) | 2840-01-708-1715 (2840017081715) | 2840-01-200-9553 (2840012009553) | 2805-00-710-5355 (2805007105355) | |
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