Confederate Air Force

During taxi to takeoff the crew sensed an odor similar to an electrical fire, and smoke became apparent in the cockpit. Both generators and the battery master were secured. The right generator would not accept a load and smoke was coming from the right wing accessory jbox in the right wheel well. Three occupants deplaned and initially extinguished the fire, which reignited due to hot metal and compromised fuel/oil lines. All systems were secured and the pilot then evacuated the airplane, which was consumed by the fire. The pilot estimated that fire fighting equipment did not arrive for 20-25 minutes after the fire began. Faa inspectors were unable to determine the fire source from the burned wreckage. However, the operator's report stated that the right starter solenoid did not open after engine start causing the starter to remain linked to the electrical system. This resulted in a system overload and subsequent electrical fire. Both fuel and oil lines were routed through the right wheel well for cockpit indications.

The 70 years old pilot was flying a Douglas A-20 in a flight of 3 aircraft at an airshow (Confederate Air Force 'Airshow 88'). Afterflying on a southerly heading, the flight entered a procedure turn which involved a 90° left turn to the east followed by a 270° right turn back northbound. While maneuvering, the A-20 entered a right descending turn and subsequently crashed on level terrain in a relatively wings level descent. The main wreckage came to rest about 225 feet from the initial impact point. According to a pathological report, the pilot had severe coronary arteriosclerosis and suffered a heart attack.

Aerial photos were being taken of the mishap aircraft. Mission called for a simulated water landing (actual water landing prohibited) by flying as close as possible to water. Copilot at controls descended aircraft to about 6 feet, then gradually reduced clearance to 6-12 inches above water, airspeed 105 mph. Copilot inadvertently allowed aircraft to touch water. On touchdown, aircraft decelerated violently and broke up, ejecting several of the occupants and coming to rest inverted. Examination of aerial photos shows aircraft hull at touchdown was slightly nose down vice normal landing attitude; water contact made at location of nose landing gear doors. Photos show outward rupturing of forward hull structure, nose gear doors missing. Hull at rear of step showed two parallel, 3-feet long by 2-in wide, fore-to-aft and outboard-to-inboard penetrations. Floor of shallow lagoon known to have scattered debris from petroleum explorations; however, no positive determination of aircraft contact with submerged object could be made. Seven occupants were killed while three others were injured.

Following several technical modifications, among them the replacement of the right engine carburetor, the crew was in charge to conduct a post maintenance test flight. After takeoff, the right engine failed. The right propeller was not feathered and the aircraft stalled and crashed. Three crew members were killed while two others were injured.