Aerospace Performance Parts is pleased to offer immediate purchasing options for United Technologies Corporation part number 701415, which you have taken interest in. This Disk Compressor Aircraft Gas Turbine Engine item is listed alongside the NSN 2840-00-005-6766 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 701415 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 2840-00-005-6766 part number 701415 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-005-6766 Item Description: Disk Compressor Aircraft Gas Turbine Engine | 2840 | 000056766 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 701415 | 3 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | Diameter | 23.491 INCHES MINIMUM AND 23.501 INCHES MAXIMUM |
| MATT | Material | STEEL DISK |
| ABHP | Overall Length | 0.971 INCHES MINIMUM AND 0.982 INCHES MAXIMUM |
| FEAT | Special Features | 5.995-6.005 IN. ID; 16 0.437-0.440 IN. HOLES EQ SP ON 9.000 IN. CENTERLINE RAD.; 16 0.498-0.501 IN. HOLES EQ SP ON 9.000 IN. CENTERLINE RAD. |
| CRTL | Criticality Code Justification | AGAV |
| CQFM | Hardness Rating | 35.0 ROCKWELL C MINIMUM DISK AND 40.0 ROCKWELL C MAXIMUM DISK |
| MDCL | Material Document And Classification | AMS6304 ASSN STD SINGLE MATERIAL RESPONSE DISK |
| CZBJ | Engine Section Location | COMPRESSOR |
| AGAV | End Item Identification | J57 AIRCRAFT ENGINE |
| APGF | Design Type | AXIAL COMPRESSOR |
| MRC | Decoded Requirement | Clear Text Reply |
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