Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-131-1207 A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.
Alternate Parts: 9004M17G34, 2840-01-131-1207, 01-131-1207, 2840011311207, 011311207
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 04, 1982 | 01-131-1207 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-131-1207
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9004M17G34 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-131-1207
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| DIAMETER | 31.410 INCHES MINIMUM AND 31.420 INCHES MAXIMUM |
| SPECIAL FEATURES | 58 CUTOUTS EQ SP CIRCUMFERENTIALLY AT BAND SLOTTING |
| CRITICALITY CODE JUSTIFICATION | AMATT$$ACZBJ$$ACZCJ$$AABMZ$$AMDCL |
| END ITEM IDENTIFICATION | ACFT ENG J79 |