To receive competitive purchasing options on part number 1807M24 by General Electric Company, look no further than NSN Direct. For your reference, this item has the NSN 2840-01-444-7701 and is listed with the description “Blade Turbine Rotor Aircraft Gas.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other General Electric Company parts produced under the CAGE Code 07482, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number 1807M24, you can glean from the first four digits of its NSN 2840-01-444-7701 that it belongs to the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. This being said, do not hesitate to request quotes on part number 1807M24 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-444-7701 Item PartTypeName: BLADE,TURBINE ROTOR,AIRCRAFT GAS | 2840 | 014447701 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1807M24 | 6 | 9 | D |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 5.388 INCHES MINIMUM AND 5.400 INCHES MAXIMUM |
| ABMK | OVERALL WIDTH | 1.347 INCHES MINIMUM AND 1.352 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG TF39 |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| BGLW | BLADE ATTACHMENT METHOD | FIR TREE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| CZCJ | STAGE NUMBER | 2 |
| FEAT | SPECIAL FEATURES | THIS ITEM IS PART OF THE HT90 MODFOR THE TF39 ENGINE, EXTERNAL COATING PLATINUM ALUMINIDE, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 2, LEAD |
| MATT | III MATERIAL | ALUMINUM BLADE |
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