Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR
2840-01-205-7705 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: 4062380, 2840-01-205-7705, 01-205-7705, 2840012057705, 012057705
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 11, 1985 | 01-205-7705 | 50555 ( COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-205-7705
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4062380 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-205-7705
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| DIAMETER | 20.740 INCHES MINIMUM AND 20.760 INCHES MAXIMUM |
| SPECIAL FEATURES | FOR STAGE 10 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-220 |