Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-179-3524 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: 9511M38P10, 9511M38P10, 9511M38P10, 9511M38P10, 2840-01-179-3524, 01-179-3524, 2840011793524, 011793524
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 17, 1984 | 01-179-3524 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-179-3524
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9511M38P10 | 75440 | BARNES GROUP INC.DBA BARNES AEROSPACE WEST CHESTER |
| 9511M38P10 | 02653 | BERKSHIRE MANUFACTURED PRODUCTS,INC. |
| 9511M38P10 | 58828 | CFM INTERNATIONAL, INC. |
| 9511M38P10 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-179-3524
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5537 ASSN STD SINGLE MATERIAL RESPONSE |
| STAGE NUMBER | 5 |
| MATERIAL THICKNESS | 0.007 INCHES MINIMUM AND 0.009 INCHES MAXIMUM |
| OVERALL WIDTH | 0.187 INCHES MINIMUM AND 0.212 INCHES MAXIMUM |
| OVERALL LENGTH | 10.226 INCHES NOMINAL |
| SPECIAL FEATURES | T.O. 2J-F110-4 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F108 |