Aerospace Performance Parts is pleased to offer immediate purchasing options for United Technologies Corporation part number 4077080-02, which you have taken interest in. This Vane Segment Compressor Aircraft Gas Turbine Engin item is listed alongside the NSN 2840-01-308-3717 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 4077080-02 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 2840-01-308-3717 part number 4077080-02 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-308-3717 Item Description: Vane Segment Compressor Aircraft Gas Turbine Engin | 2840 | 013083717 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4077080-02 | 3 | 2 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| MRC | Decoded Requirement | Clear Text Reply |
| CZBJ | Engine Section Location | COMPRESSOR |
| CRTL | Criticality Code Justification | APGF AND CZBJ AND FEAT |
| AGAV | End Item Identification | F100-PW-229 AIRCRAFT ENGINE |
| CXCY | Part Name Assigned By Controlling Agency | CASE AND STATOR,GAS TURBINE ENGINE |
| ABHP | Overall Length | 6.712 INCHES MINIMUM AND 6.716 INCHES MAXIMUM |
| MATT | Material | NICKEL ALLOY OVERALL |
| APGF | Design Type | COMPRESSOR |
| FEAT | Special Features | T.O. 2J-F100-54, FIG 88, IND 46; INCLUDES STGS 10-12; USED ONLY ON 4068722-801,-803,-806 AND -807 |
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