We are pleased to offer procurement for Kerns Manufacturing Corp part number 599452 here on NSN Portal, a Shroud Segment Turbine Aircraft product that is listed with the NSN 2840-01-419-2013 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 599452 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 Kerns Manufacturing Corp through the CAGE Code 93596, as well as falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components based on having the NSN 2840-01-419-2013. 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 599452 today and take advantage of our industry-leading services.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-419-2013 Item PartTypeName: SHROUD SEGMENT,TURBINE,AIRCRAFT | 2840 | 014192013 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
599452 | 1 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 1.496 INCHES MINIMUM AND 1.504 INCHES MAXIMUM" |
AGAV | END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE" |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV" |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SHROUD TURBINE STATOR,2 STAGE, ASSY OF" |
CZBJ | ENGINE SECTION LOCATION | TURBINE" |
CZCJ | STAGE NUMBER | 2" |
MATT | III MATERIAL | ALUMINUM ALLOY OVERALL" |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG32 IND2" |
ABHP | OVERALL LENGTH | 1.496 INCHES MINIMUM AND 1.504 INCHES MAXIMUM" |
AGAV | END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE" |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV" |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | SHROUD TURBINE STATOR,2 STAGE, ASSY OF" |
CZBJ | ENGINE SECTION LOCATION | TURBINE" |
CZCJ | STAGE NUMBER | 2" |
MATT | III MATERIAL | ALUMINUM ALLOY OVERALL" |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG32 IND2" |
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