Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR SHROUD
2840-01-080-8265 An item within a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE, designed to surround or partially surround a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It's primary purpose is to protect other components of the engine in the event of an impeller or rotor break up.
Alternate Parts: 4053291, 4052350, 4052250, 2840-01-080-8265, 01-080-8265, 2840010808265, 010808265
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 02, 1979 | 01-080-8265 | 52545 ( SHROUD, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-080-8265
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4053291 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4052350 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4052250 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-080-8265
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| DIAMETER | 16.950 INCHES MINIMUM AND 16.954 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F100-14 FIG213 IND 20 |
| END ITEM IDENTIFICATION | ACFT ENG F100 |