6241140-12: LANDING GEAR,RETRACTABLE.
The LANDING GEAR,RETRACTABLE is a the manufacturer industrial component. Key specifications include design_type: MAIN LANDING GEAR, end_item_identification: AIRCRAFT CESSNA 650 CITATION VII, aircraft_for_which_designed: AIRCRAFT CESSNA 650 CITATION VII, gear_extension_and_retraction_method: MECHANICAL, part_name_assigned_by_controlling_agency: LANDING GEAR ASSY-RH, landing_shock_absorption_and_dissipation_method: AIR/OIL SHOCK STRUT. This part is cataloged in the U.S.
Government catalog under NSN 1620-01-723-9178, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| design_type | MAIN LANDING GEAR |
| special_features | LOCATION OF THE ITEM ON THE AIRCRAFT: LANDING GEAR - MAIN. EFFECTIVITY: FROM 7078 TO 7104. AIRCRAFT MISSION DESIGNATOR CODE: U.21. |
| end_item_identification | AIRCRAFT CESSNA 650 CITATION VII |
| aircraft_for_which_designed | AIRCRAFT CESSNA 650 CITATION VII |
| wheel_quantity_accommodated | 2 |
| gear_extension_and_retraction_method | MECHANICAL |
| part_name_assigned_by_controlling_agency | LANDING GEAR ASSY-RH |
| landing_shock_absorption_and_dissipation_method | AIR/OIL SHOCK STRUT |
| NSN | 1620-01-723-9178 |
| WHEEL QUANTITY ACCOMMODATED | 2 |
| DESIGN TYPE | MAIN LANDING GEAR |
| SPECIAL FEATURES | LOCATION OF THE ITEM ON THE AIRCRAFT: LANDING GEAR - MAIN. EFFECTIVITY: FROM 7078 TO 7104. AIRCRAFT MISSION DESIGNATOR CODE: U.21. |
| GEAR EXTENSION AND RETRACTION METHOD | MECHANICAL |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | LANDING GEAR ASSY-RH |
| END ITEM IDENTIFICATION | AIRCRAFT CESSNA 650 CITATION VII |
| AIRCRAFT FOR WHICH DESIGNED | AIRCRAFT CESSNA 650 CITATION VII |
| LANDING SHOCK ABSORPTION AND DISSIPATION METHOD | AIR/OIL SHOCK STRUT |
No substitute or cross-reference records for this part.