Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR
2840-01-323-4301 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: 407908704, 4079087-04, 2840-01-323-4301, 01-323-4301, 2840013234301, 013234301
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 27, 1990 | 01-323-4301 | 50555 ( COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-323-4301
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4079087-04 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-323-4301
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 8.940 INCHES NOMINAL |
| DIAMETER | 24.401 INCHES MINIMUM AND 24.405 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-54; 7TH STAGE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |