Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE LOCK
2840-01-004-8114 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: 4036T72P01, 4036T72P01, 4036T72P01, 4036T72P01, 4036T72P01, 2840-01-004-8114, 01-004-8114, 2840010048114, 010048114
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 15, 1975 | 01-004-8114 | 50458 ( LOCK, TURBINE ROTOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-004-8114
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4036T72P01 | 9M944 | BARLOW METAL STAMPING, INC. |
| 4036T72P01 | 02653 | BERKSHIRE MANUFACTURED PRODUCTS,INC. |
| 4036T72P01 | 33617 | ELECTRO-METHODS INC |
| 4036T72P01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 4036T72P01 | 0URD3 | NEWBERRY INDUSTRIES INC |
Technical Data | NSN 2840-01-004-8114
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| STAGE NUMBER | 2 |
| MATERIAL THICKNESS | 0.036 INCHES MINIMUM AND 0.040 INCHES MAXIMUM |
| OVERALL WIDTH | 0.355 INCHES MINIMUM AND 0.365 INCHES MAXIMUM |
| OVERALL LENGTH | 1.165 INCHES MINIMUM AND 1.185 INCHES MAXIMUM |
| SPECIAL FEATURES | FOR STAGE 2 |
| CRITICALITY CODE JUSTIFICATION | AABHP$$AABMK$$AFEAT$$AAGAV |
| END ITEM IDENTIFICATION | ENGINE,ACFT,MODEL NO. J85GE-13 AND J85GE-17A |