Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR SHROUD
2840-01-484-2333 An item within a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE, designed to surround or partially surround a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It's primary purpose is to protect other components of the engine in the event of an impeller or rotor break up.
Alternate Parts: 431985401, 4319854-01, 2840-01-484-2333, 01-484-2333, 2840014842333, 014842333
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 23, 2001 | 01-484-2333 | 52545 ( SHROUD, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-484-2333
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4319854-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-484-2333
| Characteristic | Specifications |
|---|---|
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F119-PW-100 ENGINE ON F-22 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHROUD SEGMENT COMPRESSOR STATOR 4 STAGE |