Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR SHROUD
2840-01-464-9811 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: 4086144, 2840-01-464-9811, 01-464-9811, 2840014649811, 014649811
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 17, 1999 | 01-464-9811 | 52545 ( SHROUD, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-464-9811
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4086144 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-464-9811
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 4 |
| DIAMETER | 16.550 INCHES NOMINAL |
| SPECIAL FEATURES | THIS REPAIR IS FOR OVERSIZE RIVETHOLE ELONGATION AND IS APPLICABLE TO SHROUDS HAVING EITHER HONEYCOMB OR FELTMETAL ABRADABLES |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100-220/220E |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SHROUD COMPRESSOR STATOR,FOURTH STAGE INNER REAR |