Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 1559M63G04, which you have taken interest in. This Disk And Hub Compressor Aircraft item is listed alongside the NSN 2840-01-447-2868 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 1559M63G04 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from General Electric Company under CAGE Code 07482, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-447-2868 part number 1559M63G04 today, knowing we will support all your operational needs with care.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-447-2868 Item PartTypeName: DISK AND HUB,COMPRESSOR,AIRCRAFT | 2840 | 014472868 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1559M63G04 | 3 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM |
ABMZ | DIAMETER | 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND FEAT |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SPOOL, COMPRESSOR ROTOR |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
FEAT | SPECIAL FEATURES | T.O 2J-F110-14, FIG 67, IND 5; REPL P/N 1559M63G02; HPCR STG 1-2 SPOOL OIL DRAIN HOLES ARE ENLARGED 1.48 LARGER THAN THE CURRENT ELLIPTICAL HOLES TO ALLOW BETTER DRAINAGE |
MATT | III MATERIAL | TITANIUM ALLOY OVERALL |
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