Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-179-3523 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: 9511M17P11, 9511M17P11, 9511M37P11, 9511M37P11, 9511M37P11QQ, 2840-01-179-3523, 01-179-3523, 2840011793523, 011793523
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 17, 1984 | 01-179-3523 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-179-3523
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9511M17P11 | 75440 | BARNES GROUP INC.DBA BARNES AEROSPACE WEST CHESTER |
| 9511M17P11 | 02653 | BERKSHIRE MANUFACTURED PRODUCTS,INC. |
| 9511M37P11 | 58828 | CFM INTERNATIONAL, INC. |
| 9511M37P11 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9511M37P11QQ | 085X4 | TURBINE KINETICS, INC. |
Technical Data | NSN 2840-01-179-3523
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5537 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 4 |
| MATERIAL THICKNESS | 0.007 INCHES MINIMUM AND 0.009 INCHES MAXIMUM |
| OVERALL WIDTH | 0.189 INCHES MINIMUM AND 0.214 INCHES MAXIMUM |
| OVERALL LENGTH | 9.910 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F110-4,COMPRESSOR STATOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F108 |