Part Details | AIRCRAFT GAS TURBINE ENGINE FAN BLADE
2840-01-371-9462 An item mounted on a DISK, FAN, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the fan section of a ENGINE, GAS TURBINE, AIRCRAFT.
Alternate Parts: 1476M11P02, 2840-01-371-9462, 01-371-9462, 2840013719462, 013719462
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | FEB 26, 1993 | 01-371-9462 | 50533 ( BLADE, FAN, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-371-9462
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1476M11P02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-371-9462
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | FAN |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 11.348 INCHES MINIMUM AND 11.358 INCHES MAXIMUM |
| OVERALL WIDTH | 3.098 INCHES MINIMUM AND 3.102 INCHES MAXIMUM |
| DIAMETER | 18.924 INCHES MAXIMUM |
| SPECIAL FEATURES | MATL TITANIUM; STAGE 1; SLOT BLADE ATTACHMENT METHOD |
| REFERENCE DATA AND LITERATURE | 2J-F110-14 |
| END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT ENGINE |