Aerospace Performance Parts is pleased to offer immediate purchasing options for Kerns Manufacturing Corp part number 599452, which you have taken interest in. This Shroud Segment Turbine Aircraft item is listed alongside the NSN 2840-01-419-2013 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 599452 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from Kerns Manufacturing Corp under CAGE Code 93596, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-419-2013 part number 599452 today, knowing we will support all your operational needs with care.
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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