Cessna 401

On approach to Cumaná-Antonio Jose de Sucre Airport, the twin engine aircraft crashed 8 km short of runway. One passenger was seriously injured while five other occupants were killed, among them German tourists.

The pilot had cancelled his ifr flight plan, and was proceeding to the airport visually. During his approach, the left engine quit, followed by the right engine. He then realized that he had failed to switch from the auxiliary fuel tanks to the main fuel tanks prior to the approach, and exhausted the auxiliary fuel supply. With insufficient altitude to attempt a restart, he force landed the airplane in a bean field short of the airport. After the airplane came to a stop, the occupants egressed, and the fuselage was consumed in a post-crash fire.

The accident occurred during the pilot's second attempt to fly to his destination. According to airport personnel, he did not refuel the airplane after he returned from the first attempt. He had onloaded 43.6 gallons of fuel before departing on the first flight. After departing Rutherfordton on the second flight, the airplane was observed about 400 feet above the ground and 4 miles north of Monroe. One witness reported that the right engine was sputtering as it flew overhead; seconds later, the airplane crashed into a wooded area. A wreckage examination disclosed that the fuel system was empty. No fuel was found in the left engine fuel flow divider. Airport personnel also reported the pilot was not knowledgeable of the aircraft fuel system. According to the owner's manual, the fuel consumption rate for cruise at 75% power was about 16 gallons per hour per engine. The pilot had operated the engines approximately 2 hours 10 minutes before they lost power. The pilot, sole on board, was killed.

Crashed in unknown circumstances on approach to Marsh Harbour Airport. All five occupants were injured and the aircraft was destroyed.

Crashed in unknown circumstances after takeoff from Cockburn Town Airport. The pilot, sole on board, was killed.

After takeoff, while in initial climb, the twin engine aircraft crashed in unknown circumstances. Both occupants were killed.

Approximately 5 1/2 minutes after departure and while the aircraft was climbing enroute, an unknown ignition source triggered an explosion of fuel/air vapor which existed within the interior of the left wing. Wing skin from the upper/lower wing surface was lost, however, the wing structure remained integral and the pilots continued to fly the aircraft executing a 180° course reversal back to McCarran-Intl Airport. Subsequent to the explosion a fire developed within the left engine area. As the aircraft continued back towards mccarran the airspeed gradually diminished and the landing gear were lowered. Shortly thereafter the left wing entered a stall condition brought about by a decrease of airspeed as well as the degradation of its lift developing capabilities due to the explosion induced damage. The aircraft then entered an uncontrollable left roll several hundred feet above ground from which a successful recovery could not be executed. Both occupants were killed.

The left engine failed in flight, forcing the pilot to reduce his altitude and to attempt an emergency landing when the aircraft crashed in a field near Soto la Marina, bursting into flames. The aircraft was destroyed and all eight occupants were killed, among them seven veterinarians.

The two commercial rated pilots were returning from a part 135 flight at night. The fuel tanks were inadvertently not switched from mains to auxiliary. Fuel starvation occurred when aircraft was at low altitude. Insufficient altitude remained to restart the engines. Aircraft impacted ground. A post accident fire erupted destroying the aircraft. Both pilots were seriously injured.

Aircraft took off in clear weather but below-freezing temperatures with heavy frost on aircraft surfaces. No preflight, run-up or warm-up performed. On initial climb, left engine power loss occurred for undetermined reason, but probably associated with temp/cold engine operation. Pilot turned into dead engine in apparent course reversal, failed to feather propeller and lowered landing gear during turn. Aircraft stalled, rolled inverted and crashed into residential area. Engine teardown revealed no mechanical defects. Post-mortem and toxicological tests revealed no physiological impairment. All three occupants were killed.