Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-164-9087 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: 4056200, 2840-01-164-9087, 01-164-9087, 2840011649087, 011649087
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 21, 1983 | 01-164-9087 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-164-9087
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4056200 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-164-9087
| 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-F110-4; AUGMENTOR NOZZLE LEVER; BALANCE & CONVERGENT NOZZLE SEGMENT; 15 UNITS PER ASSY; 0.159-0.163 IN. DIA OF 1 HOLE; 0.190-0.192 IN. DIA THRU 2 LUGS |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW100/200 ACFT ENGINE |