Aerospace Performance Parts is pleased to offer immediate purchasing options for Ferrotherm Corporation part number 1385M43G03, which you have taken interest in. This Shroud Segment Turbine Aircraft Gas Turbine Engine item is listed alongside the NSN 2840-01-146-7570 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 1385M43G03 or any other FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components components we carry from Ferrotherm Corporation under CAGE Code 01993, 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 2840-01-146-7570 part number 1385M43G03 today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-146-7570 Item Description: Shroud Segment Turbine Aircraft Gas Turbine Engine | 2840 | 011467570 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1385m43g03 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | Diameter | 37.530 INCHES NOMINAL |
| RDAL | Reference Data And Literature | T.O. 2J-F101-4, FIG 61, IND 12 |
| ABHP | Overall Length | 1.901 INCHES MINIMUM AND 1.911 INCHES MAXIMUM |
| CZBJ | Engine Section Location | TURBINE |
| AGAV | End Item Identification | F101 AIRCRAFT GAS TURBINE ENGINE |
| CZCJ | Stage Number | 2 |
| MATT | Material | CHROMIUM OVERALL |
| APGF | Design Type | AXIAL COMPRESSOR |
| MRC | Decoded Requirement | Clear Text Reply |
| CRTL | Criticality Code Justification | ABHP AND CZBJ AND MATT AND CZCJ |
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