Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE LOCK
2840-01-005-0182 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: 3029T96P01, 3029T96P01, 3029T96P01, 3029T96P01, 2840-01-005-0182, 01-005-0182, 2840010050182, 010050182
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 18, 1975 | 01-005-0182 | 50458 ( LOCK, TURBINE ROTOR BLADE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-005-0182
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3029T96P01 | 8W686 | ATLAS STAMPING & MANUFACTURINGCORPORATION |
| 3029T96P01 | 9M944 | BARLOW METAL STAMPING, INC. |
| 3029T96P01 | 02653 | BERKSHIRE MANUFACTURED PRODUCTS,INC. |
| 3029T96P01 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-005-0182
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| STAGE NUMBER | 1 |
| MATERIAL THICKNESS | 0.036 INCHES MINIMUM AND 0.044 INCHES MAXIMUM |
| OVERALL WIDTH | 0.350 INCHES MINIMUM AND 0.360 INCHES MAXIMUM |
| OVERALL LENGTH | 0.900 INCHES MINIMUM AND 0.920 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | 2J-J85-94 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE,ACFT,MODEL NO. J85GE-21 |