Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT
2840-01-146-7570 A stationary arched metal segment used to establish clearance and a seal for the tip of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE. The inner dimension may have open honeycomb or composition filled surface or may be formed by the knife edge metal protrusions of a SEAL RING, LABYRINTH, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 1385M43G03, 1385M43, 9526M77G02, 1385M43G03, 1385M43G03, 1385M43G03, 1385M43G03, 2840-01-146-7570, 01-146-7570, 2840011467570, 011467570
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 15, 1998 | 01-146-7570 | 50603 ( SHROUD SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-146-7570
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1385M43G03 | 01993 | FERROTHERM CORPORATION |
| 1385M43 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9526M77G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1385M43G03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1385M43G03 | 50554 | METRO MACHINE WORKS, INC. |
| 1385M43G03 | 50595 | TWIGG CORPORATION |
| 1385M43G03 | 16126 | UNISON ENGINE COMPONENTS INC.DBA UNISON ENGINE COMPONENTS |
Technical Data | NSN 2840-01-146-7570
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 1.901 INCHES MINIMUM AND 1.911 INCHES MAXIMUM |
| DIAMETER | 37.530 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AABHP$$ACZBJ$$AMATT$$ACZCJ |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F101-4, FIG 61, IND 12 |
| END ITEM IDENTIFICATION | F101 AIRCRAFT GAS TURBINE ENGINE |