Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE LOCK
2840-01-004-8834 An item used to maintain the position of a BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE in the proper place on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. This item eliminates axial movement of the blade.
Alternate Parts: 4036T72P02, 4036T72P02, 4036T72P02, 4036T72P02, 2840-01-004-8834, 01-004-8834, 2840010048834, 010048834
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 15, 1975 | 01-004-8834 | 50458 ( LOCK, TURBINE ROTOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-004-8834
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4036T72P02 | 22819 | AVIALL SERVICES, INC. |
| 4036T72P02 | 02653 | BERKSHIRE MANUFACTURED PRODUCTS,INC. |
| 4036T72P02 | 33617 | ELECTRO-METHODS INC |
| 4036T72P02 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-004-8834
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| STAGE NUMBER | 2 |
| MATERIAL THICKNESS | 0.036 INCHES MINIMUM AND 0.044 INCHES MAXIMUM |
| OVERALL WIDTH | 0.355 INCHES MINIMUM AND 0.365 INCHES MAXIMUM |
| OVERALL LENGTH | 1.265 INCHES MINIMUM AND 1.285 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | 2J-J84-94 |
| SPECIAL FEATURES | T.O. 2J-J85-94 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE,ACFT,MODEL NO. J85GE-21A |