Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR BLADE
2840-01-462-3954 An item mounted on a DISK, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the turbine section of an ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 4086361, 2840-01-462-3954, 01-462-3954, 2840014623954, 014623954
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 01, 1999 | 01-462-3954 | 50535 ( BLADE, TURBINE ROTOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-462-3954
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4086361 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-462-3954
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | BLADE SET 4086361 SUPERSEDES 4087101 (2840014456144PT) BY ATTRITION, NOTECHINICAL ORDER DATA AVAILABLE, 2 BLADES REQUIRED AND MUST BE SAME MOMENT WT WITHIN 0.050 OZ. IN. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F100299 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE SET TURBINE ROTOR, 1 STAGE |