Part Details | AIRCRAFT GAS TURBINE ENGINE FAN BLADE
2840-01-472-5509 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: 1993M18P04, 1993M18P03, 2840-01-472-5509, 01-472-5509, 2840014725509, 014725509
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 07, 2000 | 01-472-5509 | 50533 ( BLADE, FAN, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-472-5509
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1993M18P04 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1993M18P03 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-472-5509
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | FAN |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | DOVETAIL |
| OVERALL LENGTH | 13.000 INCHES NOMINAL |
| OVERALL WIDTH | 3.750 INCHES NOMINAL |
| MATERIAL THICKNESS | 0.500 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F101-4, FIG17 IND8 |
| END ITEM IDENTIFICATION | F101GE102,B-1B ACFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | RUGGEDIZED STAGE 1 FAN BLADE |