Thank you for your interest in part number 9940M50P03-110B, a component manufactured by General Electric Company that we sell here on NSN Parts Finder. For your reference, this item is presented with the NSN 2840-01-475-3392 and features the description “Shaft Turbine Aircraft Gas Turbi.” To request a quote for part number 9940M50P03-110B, simply fill out the form below with key details like your budget, required quantity, and anticipated fulfillment timeline. Within 15 minutes of receiving and reviewing your submission, our staff members will present you with competitive purchasing options tailored to your needs. Alternatively, you are also welcome to give us a call or email, and we will gladly guide you through the quotation process or discuss any custom solutions you happen to be seeking.
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With a global supply chain and ample purchasing power, we can provide highly competitive pricing and swift lead times on numerous NSN 2840-01-475-3392 products. More than that, we exclusively procure our inventory from reliable manufacturers to guarantee quality, including this component from General Electric Company, which is associated with the CAGECode 07482. Keeping this in mind, get in touch with our specialists today to secure a quote on the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components part number 9940M50P03-110B.
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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