Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT
2840-01-117-0323 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: 9662M43G05, 2840-01-117-0323, 01-117-0323, 2840011170323, 011170323
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 07, 1981 | 01-117-0323 | 50603 ( SHROUD SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-117-0323
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9662M43G05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-117-0323
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 1.493 INCHES MINIMUM AND 1.506 INCHES MAXIMUM |
| DIAMETER | 16.724 INCHES MINIMUM AND 16.736 INCHES MAXIMUM |
| SPECIAL FEATURES | WAS CASE,AXIAL COMPRESSOR,TURBINEENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF-39 |