Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-134-4630 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: 4058916, 2840-01-134-4630, 01-134-4630, 2840011344630, 011344630
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 03, 1982 | 01-134-4630 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-134-4630
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4058916 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-134-4630
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| OVERALL LENGTH | 20.600 INCHES NOMINAL |
| OVERALL WIDTH | 5.535 INCHES MINIMUM AND 5.545 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-4; HEAT TREAT PER SPEC PWA 11-15 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW100/200 AIRCRAFT ENGINE |