Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE CASE
2840-01-447-2846 A case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and protect a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: KDS 28404003, KDS 2840-4003, 1276M30G02, 1276M30G02, 2840-01-447-2846, 01-447-2846, 2840014472846, 014472846
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 31, 1997 | 01-447-2846 | 50553 ( CASE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-447-2846
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| KDS 2840-4003 | 3999F | DEFENSE ACQUISITION PROGRAMADMINISTRATION, R.O.K |
| 1276M30G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1276M30G02 | T0545 | TEI TUSAS MOTOR SAN.A.S. |
Technical Data | NSN 2840-01-447-2846
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 2.359 INCHES MINIMUM AND 2.383 INCHES MAXIMUM |
| SPECIAL FEATURES | USED ON THE NOZZLE ASSEMBLY AND SEGMENTS, SEALS AND SUPPORTS |
| CRITICALITY CODE JUSTIFICATION | AABHP$$ACZBJ$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F110-14, FIG 74, IND 17 |
| END ITEM IDENTIFICATION | ACFT ENG F110GE129 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COVER,COOLING AIR-HIGH PRESSURE TURBINE NOZZLE,OUTER |