Aerospace Performance Parts is pleased to offer immediate purchasing options for United Technologies Corporation part number 701608, which you have taken interest in. This Disk Turbine Aircraft Gas Turbin item is listed alongside the NSN 2840-00-006-2791 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 701608 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from United Technologies Corporation under CAGE Code 77445, 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 2840-00-006-2791 part number 701608 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-006-2791 Item PartTypeName: DISK,TURBINE,AIRCRAFT GAS TURBIN | 2840 | 000062791 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 701608 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | ROCKWELL C35-40 HARDNESS; 1.482-1.493 INCH THICKNESS; 19.825-19.835 INCH OD; 101 BLADE SLOTS EQUALLY SPACED AROUND OD; 16 0.4205-0.4235 INCH HOLES EQUALLY SPACED ON 8 INCH CENTERLINE RADIUS; 16 0.437-0.440 INCH HOLES EQUALLY SPACED ON 8.0 I |
| MATT | MATERIAL | STEEL OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| ZZZV | FSC APPLICATION DATA | AIRCRAFT JET ENGINE,J57 |
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