Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR ROTOR
2840-01-339-9164 A single or multistage assembly designed to deliver air at the proper pressure, direction and velocity. It consists of disks, blades, hubs, and the like. It is the moving part of COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 907643710, 9076437-10, 2840-01-339-9164, 01-339-9164, 2840013399164, 013399164
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 04, 1991 | 01-339-9164 | 50587 ( ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-339-9164
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9076437-10 | 98748 | AIR FORCE UNITED STATES DEPARTMENTOF THE |
Technical Data | NSN 2840-01-339-9164
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| OVERALL LENGTH | 3.750 INCHES NOMINAL |
| DIAMETER | 20.000 INCHES NOMINAL |
| SPECIAL FEATURES | 2ND STAGE; BLADES ARE 15 IN. LONG; 3.840 IN. WIDE; ASSY USED TO DIRECT AIRFLOW |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF33-P7/100 JET ENGINE |