Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-171-0840 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: 9511M37P02, 9511M37P02, 9511M37P02, 2840-01-171-0840, 01-171-0840, 2840011710840, 011710840
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 03, 1984 | 01-171-0840 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-171-0840
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9511M37P02 | 75440 | BARNES GROUP INC.DBA BARNES AEROSPACE WEST CHESTER |
| 9511M37P02 | 02653 | BERKSHIRE MANUFACTURED PRODUCTS,INC. |
| 9511M37P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-171-0840
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5537 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 3 |
| MATERIAL THICKNESS | 0.009 INCHES MINIMUM AND 0.011 INCHES MAXIMUM |
| OVERALL WIDTH | 0.085 INCHES MINIMUM AND 0.110 INCHES MAXIMUM |
| OVERALL LENGTH | 10.689 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F110-4 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F101 |