| DESIGN TYPE | NOSE GEAR |
| AIRCRAFT FOR WHICH DESIGNED | F-35 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| GEAR EXTENSION AND RETRACTION METHOD | MECHANICAL |
| LANDING SHOCK ABSORPTION AND DISSIPATION METHOD | RIGID |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | NOSE LANDING GEAR, STRUCTURE |
| PROPRIETARY CHARACTERISTICS | PACS |
| WHEEL QUANTITY ACCOMMODATED | 1 |