Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE LOCK
2840-01-484-8274 An item used to maintain the position of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: 4321449, 2840-01-484-8274, 01-484-8274, 2840014848274, 014848274
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 09, 2001 | 01-484-8274 | 50458 ( LOCK, TURBINE ROTOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-484-8274
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4321449 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-484-8274
| Characteristic | Specifications |
|---|---|
| STAGE NUMBER | 5 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F119-PW-100 ENGINE ON F-22 AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | LOCK COMPRESSOR VANE 5TH STAGE |