NSN 2840-00-798-2850
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE LOCK RING
2840-00-798-2850 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: 777886CL1, 777886CL1, 777886CL1, 503744CL1, 387276, 777886CL1, 2840-00-798-2850, 00-798-2850, 2840007982850, 007982850
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-798-2850 | 52365 ( LOCK RING, TURBINE NOZZLE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-798-2850
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 777886CL1 | 4V114 | A-1 MACHINING |
| 777886CL1 | 02382 | EDAC TECHNOLOGIES CORPORATIONDBA GROS-IT INDUSTRIES |
| 777886CL1 | 15152 | TIMKEN AEROSPACE TRANSMISSIONS, LLC |
| 503744CL1 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 387276 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 777886CL1 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-798-2850
| Characteristic | Specifications |
|---|---|
| MATERIAL | STEEL |
| OUTSIDE DIAMETER | 34.878 INCHES MINIMUM AND 34.908 INCHES MAXIMUM |
| OVERALL THICKNESS | 0.119 INCHES MINIMUM AND 0.123 INCHES MAXIMUM |
| STAGE NUMBER | 3 |
| REFERENCE DATA AND LITERATURE | 2J-TF33-34, FIGURE 28, INDEX 21 |
| SPECIAL FEATURES | MATL SPEC AMS 5731 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |