Beechcraft 60 Duke

After obtaining a weather briefing in which he was informed of thunderstorms and current sigmets for his intended route of flight, the pilot elected to depart his home airport on a personal flight. At the time of departure, witnesses indicated the presence of thunderstorms adjacent to the airport. After trying to obtain his IFR clearance from charlotte, the pilot was issued his IFR clearance when approaching Columbia, SC. The pilot had deviated around at least one thunderstorm while approaching Columbia. The pilot had been cleared to climb to his requested altitude of 17,000 feet and had reached 16,400 when the radar return was observed to indicate a descent and then was lost. Witnesses on the ground reported seeing the airplane exit the clouds in flames. The evidence indicated that the horizontal tail had separated followed by the wings and other components of the airplane. No evidence of separation due to structural weakening from heating was found. All four occupants were killed.

The aircraft made a hard landing, ran off the right side of the runway and collided with the terrain. Subsequently, the plane erupted in flames and was destroyed, but the pilot and passengers were not injured.

Witnesses reported the aircraft took off and climbed to about 300 feet while in a wide left turn. According to witnesses, the wings were rocking and erratic engine sounds were noted. The aircraft was turning downwind when it abruptly pitched down, rolled left until inverted, descended and crash. Examination of the aircraft revealed no evidence of malfunction, although the left prop had less rotational damage than the right prop. Examination of aircraft records revealed the aircraft was inactive for about 9 years until it was returned to service less than a year before the accident. The aircraft accumulated about 17 hours since it was returned to service. The pilot stated to a witness before the accident that he had not done single engine operation in the aircraft. The aircraft was overloaded more than 200 lbs. All five occupants were killed.

The pilot had just climbed to 2,500 feet when the right engine started to sputter. When he placed the fuel selector in crossfeed, both engines quit. The pilot elected to land in a field leading to substantial damage to the nose, wings, and tail section of the aircraft. A post crash inspection of fuel system revealed no fuel in the tanks or the fuel metering units for either engine. The pilot stated after the accident that the last time he refueled the aircraft was several weeks before and that it had been flown several times since its last refueling.

The airplane was observed to approach the airport from the northwest. As it crossed the northeast end of the runway, it initiated a right turn to cross the runway about the midpoint to a position for a left downwind for landing on runway 5. Its altitude was estimated to be about 200-300 feet above the ground and the landing gear was down. The witness did not observe the airplane further. It collided with the ground about 0.4 miles from the threshold. The morning sun was about 10° above the horizon and was about 33° to the right of the runway centerline. It would have been in the pilot's face during his flight from the last departure point. The landing runway sloped upward from the landing threshold. The lower-than-normal traffic pattern, the sun's position in relation to the airplane flight path, and the runway slope could have caused the pilot to perceive his altitude as being higher than it actually was. All three occupants were killed.

On final approach to Virac Airport runway 24, in poor weather conditions, the twin engine aircraft struck the slope of a mountain and crashed 12 km from the airfield. All six occupants were killed, among them the politician Moises M. Tapia.

The pilot and his wife planned a 30 minutes pleasure flight to Lake Tahoe. Prior to departure the pilot failed to visually inspect the amount of fuel in the right wing tank. The tank was full. The tank's cap probably appeared to be secured when, in fact, because of a unique design characteristic, it was merely resting on top of the filler neck. Upon takeoff rotation the cap came off the filler neck and it was followed by a fuel spray. The pilot responded and stayed in a very low altitude and close-in traffic pattern. He attempted to land immediately. He lost control during the turn to final, stalled and collided with the pavement prior to reaching the threshold. Both occupants were killed.

Aircraft was destroyed during an attempted off airport emergency landing following a dual engine failure while leveling off at cruise flight. Pilot stated that left engine, then right engine surged and quit as he was leveling off at 9,000 feet msl. At the time of the engine failures the fuel totalizer was reading 60 gallons, but the aircraft fuel gauges were reading empty. Pilot broke out of overcast at 3,500 msl (about 1,200 feet agl) and was unable to find a suitable clear area to land before committing to an emergency landing in trees. Gear was down, flaps were up and neither engine was feathered at impact. Pilot stated that he knew he was out of gas when both engines quit and that he did not attempt an air start. Both occupants were seriously injured.

During arrival, the pilot reported a problem with his #1 nav, but said he would try to make an ILS approach. He said he would return to Pontiac, if his ILS did not work. ARTCC cleared him for the ILS runway 32 approach and instructed him to contact Pellston radio (FSS). At 1525, he called the FSS and reported he was 20 miles south. At approximately 1534, the FSS specialist heard an aircraft fly over, but did not know if it was N24RT. He asked the pilot if he was making a missed approach. The pilot gave a negative reply and reported he was picking up the glide slope, then said he was having trouble with his #1 nav. A witness about 6 miles north and west of the airport saw the aircraft on a northerly heading at about 200 feet agl. About one minute later, the aircraft collided with trees, crashed and burned approximately 8 miles from the airport at an approximately elevation of 900 feet. The airport elevation was 720 feet. The nav equipment was too badly damaged during the accident to be tested. According to the aircraft radio log, the last VOR check was on 9/10/83. The pilot had logged 5.4 hours of instrument time during the previous 6 months, but had not logged any approaches. All five occupants were killed.

The pilot stated that he experienced a loss of power in both engines, made an emergency landing in a cow pasture, and struck a cow on landing rollout. Due to the extent of post crash fire no determination could be made as to the nature of the malfunction of the engines described by the pilot.