Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR
2840-01-281-2772 A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 37D401329G024, 2840-01-281-2772, 01-281-2772, 2840012812772, 012812772
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 21, 1988 | 01-281-2772 | 50591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-281-2772
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37D401329G024 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-281-2772
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | FSCAP |
| CRITICALITY CODE JUSTIFICATION | AAGAV$$AFEAT |
| REFERENCE DATA AND LITERATURE | T.O 2J-J85-64 |
| END ITEM IDENTIFICATION | ACGT ENG J85-GE-5J/-13D/-17A |