Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE LOCK RING
2840-01-124-0726 A round metallic item designed to retain a NOZZLE, NOZZLE ASSEMBLY, or NOZZLE SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE in a CASE AND NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may be a complete 360 degrees circle or a section thereof.
Alternate Parts: 777886CL8, 777886CL8, 777886CL8, 777886CL8, 2840-01-124-0726, 01-124-0726, 2840011240726, 011240726
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 27, 1981 | 01-124-0726 | 52365 ( LOCK RING, TURBINE NOZZLE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-124-0726
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 777886CL8 | 4V114 | A-1 MACHINING |
| 777886CL8 | 02382 | EDAC TECHNOLOGIES CORPORATIONDBA GROS-IT INDUSTRIES |
| 777886CL8 | 15152 | TIMKEN AEROSPACE TRANSMISSIONS, LLC |
| 777886CL8 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-124-0726
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| OUTSIDE DIAMETER | 34.878 INCHES MINIMUM AND 34.908 INCHES MAXIMUM |
| OVERALL THICKNESS | 0.147 INCHES MINIMUM AND 0.151 INCHES MAXIMUM |
| STAGE NUMBER | 3 |
| REFERENCE DATA AND LITERATURE | 2J-TF33-34, FIGURE 28, INDEX 21 |
| SPECIAL FEATURES | MATL AMS 5731 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |