Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-443-1669 An item used to maintain the position of a BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: 5068T94P02, 92306P02, 2840-01-443-1669, 01-443-1669, 2840014431669, 014431669
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 03, 1997 | 01-443-1669 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-1669
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 5068T94P02 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 92306P02 | 56878 | SPS TECHNOLOGIES, LLCDBA AEROSPACE DIVISION |
Technical Data | NSN 2840-01-443-1669
| Characteristic | Specifications |
|---|---|
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | GE F414-400 ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | LOCK,BLADE-COMPRESSOR ROTOR, STAGE 5,6 AND 7 |