The LANDING GEAR,RETRACTABLE is a the manufacturer industrial component. Key specifications include design_type: MAIN LANDING GEAR, special_features: CYL AND PISTON ASSY 1,TORQUE ARM 2,EXTENDED LG 31.711 IN.,COMPRESSED LG 23.211 IN.,RIGHT HAND IN, aircraft_for_which_designed: T-37, gear_extension_and_retraction_method: HYDRAULIC CYLINDER, landing_shock_absorption_and_dissipation_method: AIR/OIL SHOCK STRUT. This part is cataloged in the Federal Logistics Information System (FLIS) under NSN 1620-00-105-1581, 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 | CYL AND PISTON ASSY 1,TORQUE ARM 2,EXTENDED LG 31.711 IN.,COMPRESSED LG 23.211 IN.,RIGHT HAND IN |
| aircraft_for_which_designed | T-37 |
| wheel_quantity_accommodated | 1 |
| gear_extension_and_retraction_method | HYDRAULIC CYLINDER |
| landing_shock_absorption_and_dissipation_method | AIR/OIL SHOCK STRUT |
| NSN | 1620-00-105-1581 |
| LANDING SHOCK ABSORPTION AND DISSIPATION METHOD | AIR/OIL SHOCK STRUT |
| DESIGN TYPE | MAIN LANDING GEAR |
| GEAR EXTENSION AND RETRACTION METHOD | HYDRAULIC CYLINDER |
| WHEEL QUANTITY ACCOMMODATED | 1 |
| SPECIAL FEATURES | CYL AND PISTON ASSY 1,TORQUE ARM 2,EXTENDED LG 31.711 IN.,COMPRESSED LG 23.211 IN.,RIGHT HAND IN |
| AIRCRAFT FOR WHICH DESIGNED | T-37 |