Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK
2840-01-443-4080 An item having provisions on the outer periphery for attaching a designated number of BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 6854755, 23055555, 23008865, 2840-01-443-4080, 01-443-4080, 2840014434080, 014434080
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 09, 1997 | 01-443-4080 | 50567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-443-4080
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6854755 | 63005 | ROLLS-ROYCE CORPORATION |
| 23055555 | 63005 | ROLLS-ROYCE CORPORATION |
| 23008865 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-443-4080
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 5 |
| SPECIAL FEATURES | MATERIAL IS CARPENTER CUSTOM 450 FOR STGS 2-5; PROVIDES SUPERIOR CORROSION RESISTANCE AND REPLACES THE NICKEL CADMIUM PLATING, AMS5613; CADMIUM IS A HAZARDOUS MATERIAL AND WILL BE REMOVED FROM THE ITEM AND REPLACED W/CUSTOMER 450; COATED WITH IVADIZED ALUMINUM IAW AMS 2427 AND MCDONNEL DOUGLAS PROCESS SPEC 13143 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG T-56 (T.O. 2J-T56-14; COMPRESSOR ROTOR ASSEMBLY) |
