Thank you for taking interest in General Electric Company part number 9940M50P03-110B, which is listed with the NSN 2840-01-475-3392 and a product description of “Shaft Turbine Aircraft Gas Turbi.” 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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Alongside part number 9940M50P03-110B, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Shaft Turbine Aircraft Gas Turbi part with the NSN 2840-01-475-3392. For example, you can browse other General Electric Company components that were produced under CAGE Code 07482 or listings that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 9940M50P03-110B and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-475-3392 Item PartTypeName: SHAFT,TURBINE,AIRCRAFT GAS TURBI | 2840 | 014753392 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 9940M50P03-110B | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| FEAT | Special Features | FRONT END STEPPED FROM 5.008 IN MIN AND 5.009 IN MAX O.D. SPLINED TEETH4.538 IN MIN AND 4.548 IN MAX I.D. AND5.2707 IN MIN AND 5.2712 IN MAX O.D.SECOND END 15.914 IN MIN 14.917 IN MAX.OD.SIX HOLES 0.262 IN MIN 0.269 IN MAX,DIA. 60 HOLES 0.251 IN MIN 0.252 IN MAX. |
| ABHP | Overall Length | 11.714 INCHES MINIMUM AND 11.724 INCHES MAXIMUM |
| MATT | Material | TITANIUM ALLOY SHAFT |
| CZBJ | Engine Section Location | HIGH PRESSURE COMPRESSOR |
| AGAV | End Item Identification | F100-100B 2J-F100-4 |
| CRTL | Criticality Code Justification | AGAV |
| MRC | Decoded Requirement | Clear Text Reply |
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