Abstract: A system and method for mounting engine control units. The engine control unit (ECU) mounting system is placed within a compartment of the light aircraft, aft of the firewall. The ECU mounting system uses a bracket that holds the electrical control units. The electrical control units are mounted through a firewall and are accessible via the adjacent compartment.
Abstract: A system and method for mounting engine control units. The engine control unit (ECU) mounting system is placed within a compartment of the light aircraft, aft of the firewall. The ECU mounting system uses a bracket that holds the electrical control units. The electrical control units are mounted through a firewall and are accessible via the adjacent compartment.