Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 9940M50P03-110B, which you have taken interest in. This Shaft Turbine Aircraft Gas Turbi item is listed alongside the NSN 2840-01-475-3392 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 9940M50P03-110B or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from General Electric Company under CAGE Code 07482, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2840-01-475-3392 part number 9940M50P03-110B today, knowing we will support all your operational needs with care.
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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