We appreciate your interest in Cfm International Inc part number 9993M75G15, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 9993M75G15 is listed with the NSN 2840-01-253-1391 and description “Nozzle Segment Turbine Aircraft.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Cfm International Inc under the CAGE Code 58828 or that similarly fall under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 2840-01-253-1391 parts and Nozzle Segment Turbine Aircraft items your operations require, so request a quote today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-253-1391 Item PartTypeName: NOZZLE SEGMENT,TURBINE,AIRCRAFT | 2840 | 012531391 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1285M96G13 | 1 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 4.000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | ACFT.ENG. F108 |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | NOZZLE SEGMENT-HPT STATOR |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | TWO BLADE ASSEMBLY |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | TO. 2J-F108-14 |
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