Thank you for your interest in NSN part number 599452 under NSN 2840014192013 on Click Aerospace. Click Aerospace is a website owned and operated by ASAP Semiconductor, offering customers access to an unparalleled inventory of premium parts that cater to a variety of industries and applications. Shroud Segment Turb is an item listed with the part number 599452, and FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components and it is manufactured by Electro Methods Inc having CAGE Code 33617. This item, alongside the rest of our listed NSN parts, is readily available for purchase through our website now. Get started on the purchasing process today by filling out and submitting an Instant RFQ as provided through our website. Once received, a member of our staff will reach out to you in 15 minutes or less to offer a personalized quote based on your individual needs.
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Click Aerospace is a leading independent distributor of NSN part 599452, and we can help you procure NSN components such as 2840014192013 and many more. The quality of our inventory is of the utmost importance to us, and thus we choose to only source our parts from global manufacturers like Electro Methods Inc. Get started with a competitive quote today when you submit an Instant RFQ and experience how we are revolutionizing the parts procurement process.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-419-2013 Item Description: Shroud Segment Turb | 2840 | 014192013 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
599452 | 3 | 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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