Abstract: A system and related method operates to receive autopilot selection and monitor aircraft systems to control which autopilot is actively flying the aircraft. During certain flight operations in which a single autopilot is in use, the system reverts to the next available autopilot should the active and selected autopilot disconnect for any reason (e.g., faults and/or failures). The system maintains a redundant ability for pilot use of each pilot selectable mode of each autopilot channel including altitude hold, speed hold, heading hold, etc. For an indication to a pilot or remote operator that the system has reverted to a second autopilot, the system commands a momentary aural warning and a visual message/lights. For failures resulting in timely but necessary maneuver requirements, the system maintains autopilot control laws, control authority and roll authority.

Abstract: A charcoal igniter which has a thermal barrier attached to the top of the charcoal ignition chamber. The thermal barrier restricts airflow though the charcoal chamber and retains heat within the chamber to accelerate the burning process. The thermal barrier is perforated to allow air to flow through at a reduced rate to retain hot gas from ignition within the charcoal chamber. The thermal barrier may contain thermally resistive material, such as granulated or crushed lava roc which both retains heat to accelerate the ignition and improves safety by filtering exhaust gases to prevent ash and sparks from escaping. The thermally resistive material also acts to re-radiate heat back into the charcoal chamber to further accelerate the ignition of the charcoal. The charcoal igniter has a central charcoal chamber to hold charcoal and a top mounted thermal barrier to prevent heat from escaping.