Thank you for taking interest in the Bogue Electric Manufacturing Co part number 599452, a Shroud Segment Turbine Aircraft product that we stock that is presented alongside the NSN 2840-01-419-2013 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 599452 specifically traces back to Bogue Electric Manufacturing Co through the CAGE Code 50748, a distinct identifier for one of their physical locations. Moreover, with the NSN 2840-01-419-2013, this listing falls within Federal Supply Code (FSC) 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 599452 here on Aero OEM Parts at your earliest convenience.
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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