Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT
2840-01-326-0825 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: 1275M45G03, 1385M19G03, 1385M19G03, 1317M75G01, 1275M45G03, 2840-01-326-0825, 01-326-0825, 2840013260825, 013260825
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 18, 1990 | 01-326-0825 | 50603 ( SHROUD SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-326-0825
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1275M45G03 | 75440 | BARNES GROUP INC.DBA BARNES AEROSPACE WEST CHESTER |
| 1385M19G03 | 01993 | FERROTHERM CORPORATION |
| 1385M19G03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1317M75G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1275M45G03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-326-0825
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.785 INCHES MINIMUM AND 1.800 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.038 INCHES MINIMUM AND 0.044 INCHES MAXIMUM |
| DIAMETER | 15.158 INCHES MINIMUM AND 15.162 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F110GE100 AIRCRAFT ENGINE |