Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 9524M58P02, a General Electric Company item with the NSN 2840011469475 that is listed alongside the description “Hub Turbine Aircraft Gas Turbine.” If you are interested in part number 9524M58P02 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 9524M58P02 is specifically listed with the NSN 2840-01-146-9475, and this code can be used to determine that it falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, while tracing back to General Electric Company, this NSN part was specifically produced under CAGE Code 07482. With our services and dedication to simple procurement in mind, get started with us today!
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-146-9475 Item PartTypeName: HUB,TURBINE,AIRCRAFT GAS TURBINE | 2840 | 011469475 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
9524M58P02 | 1 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABMZ | DIAMETER | 13.430 INCHES MINIMUM AND 13.441 INCHES MAXIMUM |
AGAV | END ITEM IDENTIFICATION | ACFT ENG F101-GE-100 AND F110-GE-100 |
APGF | DESIGN TYPE | AXIAL COMPRESSOR |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SHAFT,TURBINE,AIRCRAFT GAS TURBINE ENGINE |
CZBJ | ENGINE SECTION LOCATION | TURBINE |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F101-4,FIG 56,IND 22 |
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