6241209-2: SHOCK ABSORBER,DIRECT ACTION,LAN.
SHOCK ABSORBER,DIRECT ACTION,LAN. Key specifications include design_type: CAM, operation_method: HYDRAULIC, end_item_identification: AIRCRAFT CESSNA 650 CITATION VII, piston_end_connection_style: BEARING TYPE, cylinder_end_connection_style: TONGUE TYPE, part_name_assigned_by_controlling_agency: OLEO ASSY. This part is cataloged in the U.S.
Government catalog under NSN 1620-01-723-9206, 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 | CAM |
| operation_method | HYDRAULIC |
| special_features | LOCATION OF THE ITEM ON THE AIRCRAFT: LANDING GEAR - MAIN. EFFECTIVITY: FROM 0207 TO &ON. AIRCRAFT MISSION DESIGNATOR CODE: U.21. |
| end_item_identification | AIRCRAFT CESSNA 650 CITATION VII |
| piston_end_connection_style | BEARING TYPE |
| cylinder_end_connection_style | TONGUE TYPE |
| part_name_assigned_by_controlling_agency | OLEO ASSY |
| NSN | 1620-01-723-9206 |
| DESIGN TYPE | CAM |
| SPECIAL FEATURES | LOCATION OF THE ITEM ON THE AIRCRAFT: LANDING GEAR - MAIN. EFFECTIVITY: FROM 0207 TO &ON. AIRCRAFT MISSION DESIGNATOR CODE: U.21. |
| CYLINDER END CONNECTION STYLE | TONGUE TYPE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | OLEO ASSY |
| END ITEM IDENTIFICATION | AIRCRAFT CESSNA 650 CITATION VII |
| PISTON END CONNECTION STYLE | BEARING TYPE |
| OPERATION METHOD | HYDRAULIC |
No substitute or cross-reference records for this part.