Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT
2840-01-348-2306 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: 30913444, 3091344-4, 2840-01-348-2306, 01-348-2306, 2840013482306, 013482306
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 06, 1991 | 01-348-2306 | 50603 ( SHROUD SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-348-2306
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3091344-4 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-348-2306
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | INTERMEDIATE PRESSURE COMPRESSOR |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 1.088 INCHES MINIMUM AND 1.109 INCHES MAXIMUM |
| DIAMETER | 15.777 INCHES MINIMUM AND 15.787 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | PACER DAWN |