Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE LOCK
2840-00-008-6168 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: 9080M68P01, 2840-00-008-6168, 00-008-6168, 2840000086168, 000086168
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 21, 1972 | 00-008-6168 | 50454 ( LOCK, COMPRESSOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-008-6168
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9080M68P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-008-6168
| Characteristic | Specifications |
|---|---|
| MATERIAL | NICKEL ALLOY |
| STAGE NUMBER | 2 |
| MATERIAL THICKNESS | 0.078 INCHES MINIMUM AND 0.082 INCHES MAXIMUM |
| OVERALL WIDTH | 1.530 INCHES NOMINAL |
| OVERALL LENGTH | 1.722 INCHES NOMINAL |
| SPECIAL FEATURES | 0.082 IN. THICK |
| CRITICALITY CODE JUSTIFICATION | AMATT$$AABHP$$AABMK |
| END ITEM IDENTIFICATION | ACFT ENG. TF-39 |