Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR CASE
2840-01-160-7250 A case that is an integral part of an ENGINE, GAS TURBINE, AIRCRAFT, designed to surround and protect a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 703173, 2840-01-160-7250, 01-160-7250, 2840011607250, 011607250
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 25, 1983 | 01-160-7250 | 50547 ( CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-160-7250
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 703173 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-160-7250
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| DIAMETER | 58.200 INCHES NOMINAL |
| SPECIAL FEATURES | HARDNESS RATE ROCKWELL C25-33 OR EQUIV. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O.2J-TF33-34 FIG 14, IND 1 |
| END ITEM IDENTIFICATION | TF33-PW-102 TURBINE FAN JET ENGINE,KC-135 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CASE REAR COMPRESSOR,INNER |