Aerospace Performance Parts is pleased to offer immediate purchasing options for Curtiss Wright Controls Inc part number 415248N2, which you have taken interest in. This Propeller And Shaft item is listed alongside the NSN 2810-00-306-5940 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 415248N2 or any other FSC 2810 Gasoline Reciprocating Engines Aircraft Prime Mover and Components components we carry from Curtiss Wright Controls Inc under CAGE Code 0AHP5, 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 2810-00-306-5940 part number 415248N2 today, knowing we will support all your operational needs with care.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2810-00-306-5940 Item PartTypeName: PROPELLER AND SHAFT | 2810 | 003065940 | N | |||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | 0 | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
415248N2 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AGAV | END ITEM IDENTIFICATION | ACFT ENG R1820 |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | MATL STEEL PER AMS 6412; HARDNESS PER BRINELL 302 MIN AND 341 MAX; 14.364 IN. LONG; SHAFT STEPPED FROM 4.3200 IN. MIN AND 4.3205 IN. MAX OD TO 3.307 IN. MIN AND 3.312 IN. MAX OD; BORE 2.437 IN. MIN AND 2.438 IN. MAX DIA; INCLUDES BUSHING PA |
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