Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-346-6558 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: 30972891, 3097289-1, 2840-01-346-6558, 01-346-6558, 2840013466558, 013466558
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 09, 1991 | 01-346-6558 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-346-6558
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3097289-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-346-6558
| Characteristic | Specifications |
|---|---|
| MATERIAL | COBALT ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5537 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 1 |
| MATERIAL THICKNESS | 0.440 INCHES NOMINAL |
| OVERALL WIDTH | 2.088 INCHES MINIMUM AND 2.096 INCHES MAXIMUM |
| OVERALL LENGTH | 0.310 INCHES MINIMUM AND 0.340 INCHES MAXIMUM |
| SPECIAL FEATURES | DOVETAIL SHAPE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | PACER DAWN |