Mfg Part Number: 599452 | Manufacturer: Electro Methods Inc | NSN : 2840-01-419-2013 |
Item Name : Shroud Segment Turb | CAGE Code : 33617 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
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With cost savings and rapid lead times, our inventory of manufacturer Electro Methods Inc items like NSN 2840-01-419-2013 is organized to promote a procurement process that follows the motto: “as soon as possible, as simple as possible.” You can find Part 599452 listed next to the CAGE Code 33617 under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components or you can search for specific details to find any other product you have in mind. As quality is the cornerstone of our operations, all NSN parts are sourced reliably from trusted manufacturers and shipped to you alongside all applicable trace documentation. Furthermore, we are an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited enterprise with a strict No China Sourcing policy, ensuring the premium quality of our inventory. When you are ready to begin procuring any item, submit an RFQ or contact us via phone or email for one-on-one assistance.
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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