Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-374-4833 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: 4079610, 2840-01-374-4833, 01-374-4833, 2840013744833, 013744833
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 23, 1993 | 01-374-4833 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-374-4833
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4079610 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-374-4833
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5596 ASSN STD SINGLE MATERIAL RESPONSE |
| HARDNESS RATING | 36.0 ROCKWELL C NOMINAL |
| STAGE NUMBER | 6 |
| MATERIAL THICKNESS | 0.071 INCHES MINIMUM AND 0.078 INCHES MAXIMUM |
| OVERALL WIDTH | 0.701 INCHES MINIMUM AND 0.708 INCHES MAXIMUM |
| OVERALL LENGTH | 1.411 INCHES NOMINAL |
| REFERENCE DATA AND LITERATURE | 2J-F100-54,FIG 96,IND 51 |
| SPECIAL FEATURES | 44 UNITS PER ASSY; 1 PER 2 STATORVANES |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW229 ACFT ENG CORE |