Part No. : 305-390-902-0 | Alternate P/N : 3053909020 | Manufacturer : cfm international inc |
Item Name: nozzle segment turbine aircraft | NSN: 2840-01-187-3198 (2840011873198) | CAGE Code: 58828 |
FSC: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
If you require part number 305-390-902-0 from Cfm International Inc which is described as a Nozzle Segment Turbine Aircraft component ASAP Logistic Solutions is your sourcing solution. On this page, you can request a quote on part number 305-390-902-0 which is listed under the Federal Supply Class 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. To ensure that you only procure the exact item you need to be sure to note that this particular product is listed with the NSN 2840011873198 and was produced under the CAGE Code 58828. To learn more about this listing or to simply initiate the purchasing process, complete and submit the RFQ form on this page for part 305-390-902-0 today Within 15 minutes of receiving and reviewing a completed request based on the information you provide a member of our staff will contact you to provide a tailored solution to your comparison needs. 305-390-902-0
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-187-3198 Item Description: Nozzle Segment Turbine Aircraft | 2840 | 011873198 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
7 | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
305-390-902-0 | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
ABHP | OVERALL LENGTH | 169.7 MILLIMETERS NOMINAL |
ABMK | OVERALL WIDTH | 49.1 MILLIMETERS NOMINAL |
AGAV | END ITEM IDENTIFICATION | ACFT ENG F108 |
CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE SEGMENT ASSEMBLY-LPT STG 4 |
CZBJ | ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
FEAT | SPECIAL FEATURES | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE; MATL RENE 77 |
MATT | III MATERIAL | NICKEL ALLOY OVERALL |
RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14 FIG 72-54-00 IND 7-140D |
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