Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-347-2260 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: 30972821, 3097282-1, 2840-01-347-2260, 01-347-2260, 2840013472260, 013472260
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 18, 1991 | 01-347-2260 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-347-2260
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3097282-1 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-347-2260
| Characteristic | Specifications |
|---|---|
| MATERIAL | COBALT ALLOY |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5537 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 2 |
| MATERIAL THICKNESS | 0.470 INCHES NOMINAL |
| OVERALL WIDTH | 0.310 INCHES MINIMUM AND 0.330 INCHES MAXIMUM |
| OVERALL LENGTH | 1.146 INCHES MINIMUM AND 1.156 INCHES MAXIMUM |
| SPECIAL FEATURES | DOVETAIL SHAPE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | PACER DAWN |