Airport (less than 10 km from airport)

Following an uneventful flight from Tyumen, the aircraft was approaching Khanty-Mansiysk Airport by night and poor weather conditions due to snow falls and a visibility limited to 5,300 metres with a cloud base at 400 metres. On final approach, the aircraft descended below the MDA when it landed at a speed of 190 km/h on an helipad located 159 metres to the left of the runway and 950 metres from its threshold. The aircraft collided with three parked helicopters and crashed. Both pilots, a third crew member and two passengers were killed. The aircraft as well as three helicopter registered RA-22313, RA-25144 and RA-25939 were destroyed.

The aircraft was completing a cargo flight from Santiago de Chile to Buenos Aires, carrying eight crew members and a load of 30 tons of fish. On final approach to Buenos Aires-Ezeiza-Ministro Pistarini Airport runway 11, at a speed of 151 knots, the crew quickly extended flaps to 14°, 25°, 40° and finally 50°, causing the aircraft to nose down and enter a rapid descent until it struck the ground 750 metres short of runway threshold. Upon impact, the aircraft broke in three and caught fire. Both pilots were killed while six other occupants were injured.

Propair flight 450, a Swearingen SA226TC (serial number TC-215E) with 13 persons on board, was on a charter flight from La Grande Rivière, Quebec, to Puvirnituq, Quebec. The co-pilot was in the right-hand seat and was flying the aircraft. Following an instrument approach to runway 19, the aircraft broke through the cloud layer and the co-pilot switched to visual for the final approach. As soon as the nose gear touched down on landing, the aircraft veered left. The co-pilot applied full right rudder and throttled back to GROUND IDLE in preparation for reversing thrust. A short time later, the pilot-in-command took the controls of the aircraft and left the throttle levers on GROUND IDLE. He then observed that the aircraft was drifting further to the left and that, even when he applied full right rudder, he was unable to correct the drift. As a last resort, he pressed the PARK button for the nosewheel steering system, but the aircraft continued its course toward the runway edge and crashed at the bottom of the embankment. The investigation established that the aircraft left the runway about 2,000 feet from the threshold after turning left 90 degrees relative to the runway centre line. The nose gear and main landing gear separated from the aircraft when the aircraft fell from the runway shoulder to the bottom of the embankment.

The aircraft, a Piper PA-31-350 Navajo Chieftain (hereafter referred to as a Chieftain), took off at 1113 Atlantic daylight saving time on a charter flight from Port-Menier, Quebec, to Bangor, Maine, with one pilot and seven passengers on board. As the aircraft was approaching Charlo, New Brunswick, the pilot reported to Moncton Air Traffic Control Centre that his aircraft had a rough-running engine, and that he would be making an emergency landing at Charlo airport. While the pilot was apparently manoeuvring to land the aircraft, it crashed three miles west of the runway, in the community of Eel River Crossing. All eight occupants of the aircraft received fatal injuries.

Prior to takeoff from a private turf airstrip (1400'x 90'), the pilot adjusted the left engine's fuel pump. On takeoff roll the left engine began surging. The pilot continued the takeoff. The pilot lifted off at approximately 1000' and pulled back on the yoke to get over the trees on the left side of the airstrip. The airplane drifted to the left. The pilot said he stalled the airplane and should have pushed the yoke forward to gain airspeed. The Pilot Operating Handbook indicted a takeoff roll of approximately 2,500 feet was needed on a dry paved surface.

After landing in a wet runway surface, the twin engine aircraft was unable to stop within the remaining distance and overran. There were no casualties but the aircraft was damaged beyond repair. The exact date of the accident remains unknown, somewhere in October 1996.

The twin engine aircraft was completing a local post maintenance flight with one pilot and two mechanics on board. Shortly after takeoff, while climbing to a height of 210 feet, the aircraft entered an uncontrolled descent and crashed. All three occupants were killed. According to the representatives of the owner of the airplane, recent maintenance had been performed on the engines, propellers, and the nose landing gear.

After touchdown at Cuiabá-Marechal Rondon Airport, the crew started the braking procedure. After few seconds, the crew deactivated the reverse thrust system when control was lost. The aircraft veered off runway to the right, lost its undercarriage and came to rest few dozen metres further. All 15 occupants escaped uninjured while the aircraft was damaged beyond repair.

En route from Mitú to La Pedrera, weather conditions deteriorated. As the crew was unable to receive a last weather bulletin for the destination airport, he decided to divert to Taraira. Following a waiting period on the ground, the crew decided to takeoff but the soft runway surface was wet. Unable to gain sufficient speed, the crew abandoned the takeoff procedure but the aircraft overran and came to rest. All three occupants escaped uninjured while the aircraft was damaged beyond repair.

The aircraft was completing a cargo flight from Luanda to Lucapa on behalf of Hellier International Ltd, carrying 13 passengers, six crew members and a load of 12,6 tons of fish. After touchdown by night at Lucapa Airport, the crew started the braking procedure when the runway light system failed. The crew lost control of the airplane that overran and came to rest against a house located 60 metres further. Six passengers trapped in the cargo hold were killed as well as one people in the house.