| AIRCRAFT FOR WHICH DESIGNED | AIRCRAFT CESSNA 650 CITATION VII |
| DESIGN TYPE | MAIN LANDING GEAR |
| GEAR EXTENSION AND RETRACTION METHOD | MECHANICAL |
| LANDING SHOCK ABSORPTION AND DISSIPATION METHOD | AIR/OIL SHOCK STRUT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | LANDING GEAR ASSY-LH |
| SPECIAL FEATURES | LOCATION OF THE ITEM ON THE AIRCRAFT: LANDING GEAR - MAIN. EFFECTIVITY: FROM 7105 TO &ON. AIRCRAFT MISSION DESIGNATOR CODE: U.21. |
| WHEEL QUANTITY ACCOMMODATED | 2 |