Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR
2840-00-819-6143 A single or multistage item designed to receive, compress, and deliver air to the combustion area at a required pressure and velocity. It consists of a CASE (3) AND VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 730784, 704274, 446074, 2840-00-819-6143, 00-819-6143, 2840008196143, 008196143
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1962 | 00-819-6143 | 50555 ( COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-819-6143
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 730784 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 704274 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 446074 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-819-6143
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| DIAMETER | 27.720 INCHES MINIMUM AND 27.740 INCHES MAXIMUM |
| SPECIAL FEATURES | STAGE 14; 19.320-19.330 IN. INSIDE DIAMETER; TO BE USED ONLY ON P3/5/9 ENGINE SERIES ONLY |
| CRITICALITY CODE JUSTIFICATION | AABMZ$$AFEAT$$ACZBJ |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG 17, IND 32 |
| END ITEM IDENTIFICATION | TF33-P3/5/9 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME NOZZLE ASSEMBLY,TURBINE,AIRCRAFT GAS TURBINE ENGINE |