Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR
2840-01-369-6008 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: 408453001, 4084530-01, 408448001, 4084480-01, 408388001, 4083880-01, 407788001, 4077880-01, 2840-01-369-6008, 01-369-6008, 2840013696008, 013696008
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 29, 1992 | 01-369-6008 | 50555 ( COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-369-6008
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4084530-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4084480-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4083880-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4077880-01 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-369-6008
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 6.669 INCHES MINIMUM AND 6.679 INCHES MAXIMUM |
| DIAMETER | 21.935 INCHES MINIMUM AND 21.942 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE/CORE |