We are pleased to offer procurement for General Electric Company part number 537L915 here on NSN Portal, a Case Fan Aircraft Gas Turbine En product that is listed with the NSN 2840-01-180-3085 for ease of identification. You have reached our Request for Quote (RFQ) form for this listing, where you are encouraged to submit details on your requirements to receive tailored purchasing options from our staff. As you will see, we ask that you offer key information on your pricing target, desired quantity, and more, as this will ensure that the representative who responds to your request is able to provide the most fitting solutions for your needs.
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Whether you procure part number 537L915 or other NSN products from our website, you can rest assured that we uphold full traceability for all items. For example, this particular listing traces back to General Electric Company through the CAGE Code 07482, as well as falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components based on having the NSN 2840-01-180-3085. Furthermore, every purchase will be delivered with any applicable qualifying certifications or manufacturer trace documentation as per our NO CHINA SOURCING pledge. If you are ready to experience why professionals rely on us for their needs, request a quote for part number 537L915 today and take advantage of our industry-leading services.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-180-3085 Item Description: Case Fan Aircraft Gas Turbine En | 2840 | 011803085 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
537l915 | 3 | 9 | D |
MRC | Criteria | Characteristic |
---|---|---|
ABMZ | DIAMETER | 94.700 INCHES NOMINAL |
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,TURBINE,AIRCRAFT GAS TURBINE ENGINE |
CZBJ | ENGINE SECTION LOCATION | FAN |
FEAT | SPECIAL FEATURES | 2ND STAGE; CASE ASSEMBLY |
MATT | III MATERIAL | STEEL OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF39-4, FIG 38 |
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