Part Details | AIRCRAFT GAS TURBINE ENGINE FAN BLADE
2840-01-474-2341 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: 1359M81P05, 1359M81P04, 2840-01-474-2341, 01-474-2341, 2840014742341, 014742341
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 27, 2000 | 01-474-2341 | 50533 ( BLADE, FAN, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-474-2341
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1359M81P05 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1359M81P04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-474-2341
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | FAN |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | DOVETAIL |
| OVERALL LENGTH | 12.700 INCHES NOMINAL |
| OVERALL WIDTH | 6.600 INCHES NOMINAL |
| MATERIAL THICKNESS | 2.700 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-F118-4, FIG 17, IND 5 |
| END ITEM IDENTIFICATION | F118-100 ENGINE |