| DESIGN TYPE | MAIN LANDING GEAR |
| AIRCRAFT FOR WHICH DESIGNED | F-35 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| GEAR EXTENSION AND RETRACTION METHOD | HYDRAULIC CYLINDER |
| LANDING SHOCK ABSORPTION AND DISSIPATION METHOD | AIR/OIL SHOCK STRUT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ASSEMBLY MAIN LANDING GEAR STOVL, RIGHT HAND |
| PROPRIETARY CHARACTERISTICS | PACS |
| WHEEL QUANTITY ACCOMMODATED | 1 |