Thank you for taking interest in General Electric Company part number 9663M32G45, which is listed with the NSN 2840-01-408-6306 and a product description of “Case And Nozzle Assembly Turbine.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-408-6306 Item PartTypeName: CASE AND NOZZLE ASSEMBLY,TURBINE | 2840 | 014086306 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 9663M32G45 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TF-39 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND FEAT |
| CZBJ | ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| FEAT | SPECIAL FEATURES | INCLUDES STAGES 1-4 WITH ONE PIECE BACKING |
| RDAL | REFERENCE DATA AND LITERATURE | T.O.2J-TF39-4 FIGURE 63,INDEX 101 AND FIGURE 68 BREAKOUT |
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