Thank you for considering General Electric Company part number 9940M50P03-110B, an item we carry that is listed with the NSN 2840-01-475-3392 and product description “Shaft Turbine Aircraft Gas Turbi.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number 9940M50P03-110B was specifically produced by General Electric Company under CAGE Code 07482, and with the NSN 2840-01-475-3392, it belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number 9940M50P03-110B today, knowing we will be in touch shortly after reviewing your information.
| 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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