Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-01-032-5863 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: 9182M25P01, 9182M25P01, 9182M25P01, 2840-01-032-5863, 01-032-5863, 2840010325863, 010325863
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 16, 1976 | 01-032-5863 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-032-5863
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9182M25P01 | 52677 | DOUGLAS MACHINE & TOOL CO INC |
| 9182M25P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 9182M25P01 | 28884 | TSS TECHNOLOGIES, INC.DBA TSS MEDICAL |
Technical Data | NSN 2840-01-032-5863
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| STAGE NUMBER | 2 |
| MATERIAL THICKNESS | 0.190 INCHES MINIMUM AND 0.210 INCHES MAXIMUM |
| OVERALL WIDTH | 0.400 INCHES MINIMUM AND 0.406 INCHES MAXIMUM |
| OVERALL LENGTH | 0.321 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | AIRCRAFT ENGINE MODEL NO. TF-39 |