Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE SHROUD SEGMENT
2840-01-430-2595 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: 9526M77G03, 9526M77, 2840-01-430-2595, 01-430-2595, 2840014302595, 014302595
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 25, 1996 | 01-430-2595 | 50603 ( SHROUD SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-430-2595
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9526M77G03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9526M77 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-430-2595
| 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 |
| SPECIAL FEATURES | MAT IS HASTALLOY X; HONEYCOMBED; ITEM IS PREGROUND; SUPERSEDED P/N 9526M77G02 PER CID 808396 |
| CRITICALITY CODE JUSTIFICATION | AMATT$$ACZBJ$$ACZCJ$$AABHP$$AABMZ |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F101-4, FIG 61, IND 12 |
| END ITEM IDENTIFICATION | F101 AIRCRAFT GAS TURBINE ENGINE |