Positioning

The crew arrived at the airport about 20 minutes before the planned midnight takeoff time, after the pilot-in-command had spent the day moving furniture. A night watchman noted that the preflight inspection and takeoff roll to rotation/lift-off was normal. There was no post-takeoff radio call to either unicom or ATC, although the crew had filed an IFR flight plan. After taking off from runway 36, the aircraft crashed about 1.8 mile north of the runway. The wreckage was found after interruption of electrical power to a nearby city. Initial impact was with trees, while in a shallow/left/descending turn. An area of trees about 1/2 mile long was damaged by impact and fire. Before coming to rest, the aircraft hit a powerline support tower. There was evidence the aircraft was traveling at about 260 knots, when it crashed. No preimpact part failure or malfunction was found that would have resulted in the accident. Both pilots were killed.

The pilot landed the amphibian landing gear equipped aircraft on water with the wheels extended, and the aircraft flipped over to an inverted attitude on touchdown. The pilot, sole on board, was killed.

Before the flight, the pilots of 2 Beech 200 aircraft evaluated weather reports at a fixed base operation and made a computer weather inquiry. They departed Santa Monica, CA, on a positioning flight to Farmington, NM, without filing a flight plan. While en route, the lead aircraft was about 1 to 3 minutes ahead of the 2nd aircraft. The 2nd pilot reported they were at about 4,500 feet msl as they neared mountains and the clouds were about 1,000 feet above. As they continued eastward in a valley, the 2nd pilot heard the lead pilot report he was 'going up.' This was the last known transmission from the lead aircraft. The 2nd pilot continued his flight in VMC. Two days later, the lead aircraft was found, where it had crashed about 100 feet below the top of a 7,400 feet mountain ridge. Impact occurred on a heading of about 030°. The mountain ridge was oriented on headings of 060° 240°.

After conducting ground training all day, the instructor/director of operations and his trainee flew an EMB-110P1 to Memphis to exchange airplanes. Ground fog had started to form prior to departure. After exchanging airplanes, they made the return flight to Columbia. They obtained radar vectors to the final approach course for the SDF at Columbia. The thick fog resulted in a missed approach. During the missed approach, the runway was visible from above and the crew indicated that they would try for a VFR approach and landing. The airplane collided with trees 2,350 feet from the runway in a wings level attitude. The tops of the trees were broken 41 feet above the runway threshold altitude. The trainee had been without rest for at least 30 hours prior to the accident. One pilot was killed while the second was seriously injured.

On a positioning flight for crop-spraying operations to the airstrip of the sovkhoz (state farm) "Tatarski" when the pilot tried to make a pancake landing as he assumed the ground to be drenched. The aircraft lost speed on short final, causing the left wing to stall and to struck the ground. The aircraft cartwheeled and was damaged beyond repair. All three crew members escaped uninjured.

The pilot was to conduct a charter with passengers from Sydney to Wollongong, Nowra, Canberra and return to Sydney, departing Sydney at about 10.00am. Earlier that morning he positioned the aircraft at Sydney and had it refuelled. When the passengers arrived he explained that the weather in the various destinations was very poor and that there was a possibility they may not be able to land. However, he was prepared to give it a try. As the passengers were pressed for time, they could not afford to take a chance with the weather and so they decided to drive. They told the pilot that if he could land at Wollongong later that day they would continue the flight with him. However, they impressed on him that there was no pressure for him to depart immediately as they would not be in Wollongong for several hours. After driving for a short time, the passengers decided that the weather did not appear as if it would improve, and believed that it would be better to complete the journey by car. They contacted the charter company by phone to cancel the charter, but the pilot had already departed. The flight to Wollongong appears to have proceeded normally where the pilot reported commencing an NDB approach, and would call again at a specified time. This was the last message received from the pilot. Witnesses on the ground at Wollongong, and on a yacht 20 nautical miles to the east of Wollongong reported hearing an aircraft flying at approximately 1000 to 2000 feet in the low cloud and rain. There were no other known aircraft in the area. Later that day a helicopter discovered wreckage debris in the sea, which was confirmed as being from the aircraft. The search was discontinued due to very poor weather and visibility, and cancelled two weeks later when further efforts failed to locate any trace of the aircraft.

Witnesses reported aircraft was high during approach and landed nosewheel 1st about 1,600 feet beyond threshold, then became airborne and bounced 2 times. Pilot stated that before touchdown, he started to 'spool up' engines, but noted lack of response, then retarded throttles and landed. He said he applied brakes and selected 'full reverse' and noted no response. Reportedly, nosewheel 'skipped into air' while aircraft still had flying speed. With insufficient runway remaining to stop, he elected to stow reversers and began go-around. He noted no response from engines, tho aircraft had became airborne. Aircraft then settled beyond departure end of runway and crashed on rough terrain. Examination revealed engines had ingested twigs, grass and dirt. Reverse load limiters (l/l) on both engines were found in tripped position. Flight man stated that to avoid actuation of l/l, do not advance primary throttle after returning reverse thrust lever to stow until unlock light is out; maint required to reset actuated l/l. L/l was incorporated on thrust reverser to reduce engine power to idle, if inadvertently deployed in flight. During post-accident check, both engines were operated to 85% after l/l reset.

After takeoff from runway 20 at Oxford-Kidlington Airport, while climbing to an altitude of 1,500 feet, the pilot reduced engine power when the right engine failed. He informed ATC at Oxford Airport and was cleared to return. Shortly later, the right engine caught fire and the pilot attempted an emergency landing. The aircraft crash landed in a soft ground about 8 km south of the airport, bursting into flames. The pilot escaped uninjured.

For unknown reasons, the twin engine aircraft belly landed at Lisbon-Portela de Sacavém Airport and slid for few dozen meters before coming to rest. Both pilots were uninjured while the aircraft was damaged beyond repair.

En route from Dakar to Agadir, while cruising at the altitude of 11,000 feet, the aircraft was hit by a SAM-7 surface-to-air missile. An engine detached and out of control, the aircraft entered a dive and crashed in a desert area near Bir Moghreïn. All five occupants were killed. They were on their way to Agadir on behalf of the United States Agency for International Development.