If your operations demand part number 9940M50P03-110B, an item produced by General Electric Company and listed with the description “Shaft Turbine Aircraft Gas Turbi,” look no further than this page. At your convenience, you can complete the Request for Quote (RFQ) form below with details like your budget, desired quantity, and anticipated fulfillment timeline to receive customized procurement options on part number 9940M50P03-110B. Our representatives will happily treat you to competitive pricing and swift lead times upon their receipt and review of a completed form, regularly responding in 15 minutes or less.
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If you are interested, be sure to explore our website further for related CAGE Code 07482 items or other various products manufactured by General Electric Company. We also present a catalog of all related FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components parts that we currently carry for your perusal. Regardless of what you decide to purchase from us, we will work closely with you to provide dependable, authentic products while ensuring that we address every requirement possible. This being said, get started on requesting quotes for part number 9940M50P03-110B and any other NSN parts you need on Sky Forge Components to experience our unrivaled fulfillment services.
| 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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