Piper PA-61 Aerostar (Ted Smith 601)

While in normal cruise on a flight from Panama City to Fort Myers, the twin engine airplane entered an uncontrolled descent. Due to overload failure, it partially disintegrated in the air, losing its left wing and tail section before crashing in an uninhabited area located near Wilma. Both occupants were killed.

En route from Chattanooga to Birmingham, while in cruising altitude, the twin engine entered an uncontrolled descent and crashed in an open field. The pilot, sole on board, was killed.

The aircraft was engaged on the return segment of a flight from Perth to Teutonic Bore, with an intended refuelling stop at Leonora. After embarking the two passengers and their baggage, the pilot started the engines and taxied for a take-off into the north, on the 1350 metre long main strip. The weather conditions were fine with a northerly surface wind of about 7 knots. The initial part of the take-off run was apparently normal but, after travelling some 400 metres and at about the point of rotation, one of the passengers noted an engine power surge. The take-off was continued, the aircraft became airborne and shortly afterwards the landing gear was retracted. After the aircraft had slowly climbed straight ahead to an altitude of about 200-300 feet above ground level, the passenger heard a marked change in the engine noise and felt the aircraft decelerating. The extent of the power loss and the absence of any yawing force indicated both engines had lost power simultaneously. Level flight straight ahead was reportedly maintained for an estimated 10 seconds and then the aircraft entered a descending left turn. At about this time the pilot, in response to a query from the passenger, advised that he intended to return to the airstrip but then stated "we're going down", or words to that effect. The terrain in the area was generally firm and flat. It was lightly covered with scrub and there was occasional small trees but a safe landing with only minimal damage was possible. When VH-KXY struck the ground the gear and flaps were retracted and the rate of descent was high. The aircraft was in a level attitude but yawed approximately 45 degrees to the right. After the initial impact, the aircraft slid across the ground on a track of 220 degrees magnetic for 67 metres before coming to rest. There was no post-impact fire. One passenger was able to exit via the cabin door by his own efforts. The other occupants were trapped in the wreckage and were rescued some 30 minutes later by persons who attended the accident. The pilot died shortly after being removed from the aircraft.

The twin engine airplane departed San Jose Municipal Airport on a local aerial photography mission, carrying one passenger and one pilot. En route, the airplane stall, entered a spin and crashed in flames. The aircraft was totally destroyed and both occupants were killed.

The pilot, sole on board, was completing a solo practice flight in the vicinity of Bishop Airport. While flying at low height, he lost control of the airplane that stalled and crashed in a field. The aircraft was destroyed and the pilot was killed.

Shortly after takeoff from runway 24 at Teterboro Airport, while climbing, one of the engine caught fire after the exhaust pipe separated. The pilot lost control of the airplane that crashed in flames in Carlstadt, less than 1,2 mile from the runway end. The aircraft was destroyed and all three occupants were killed.

Few minutes after takeoff from Aspen-Pitkin County-Sardy Field Airport, while climbing, the pilot reported engine malfunction and was cleared to return for an emergency landing. Shortly later, the airplane went out of control and crashed in flames. The aircraft was destroyed and all four occupants were killed.

On final approach to Columbus-Ohio State University Airport in clouds, the twin engine airplane stalled and crashed in flames. All three occupants were killed. Icing conditions were forecasted.

While in cruising altitude on a flight from San Antonio to Lake Charles, the twin engine airplane went out of control, entered a dive and crashed near New Braunfels, Texas. The aircraft was totally destroyed by impact forces and a post crash fire and both occupants were killed.

After lift-off at 85 knots, the pilot noted a positive rate of climb before retracting the landing gear and flaps. He then felt the aircraft sink and noted a high indicated rate of descent. Although full power was applied the descent continued until the aircraft struck the runway in a slightly nose-up attitude. The aircraft slid across the overrun area and through a fence before coming to rest. Fire broke out and engulfed the wreckage. At the time of the accident the aircraft weight was more than 200 kg above the maximum allowable and the centre of gravity was 142 mm forward of the forward limit. The pilot had been unable to retain control of the aircraft during the initial climb phase when the flaps were retracted at a relatively low airspeed.