Thank you for taking interest in the General Electric Company part number 1385M43G03, a Shroud Segment Turbine Aircraft Gas Turbine Engine product that we stock that is presented alongside the NSN 2840-01-146-7570 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 1385M43G03 specifically traces back to General Electric Company through the CAGE Code 07482, a distinct identifier for one of their physical locations. Moreover, with the NSN 2840-01-146-7570, this listing falls within Federal Supply Code (FSC) 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 1385M43G03 here on Aero OEM Parts at your earliest convenience.
| 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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