Airport (less than 10 km from airport)

For unknown reasons, the aircraft landed hard and bounced several times before landing firmly. On touchdown, the nose gear collapsed and the airplane slid for few dozen metres before coming to rest. All 21 occupants escaped uninjured while the aircraft was damaged beyond repair.

Following an uneventful flight from Moscow, the crew started a night approach to Dubai Intl Airport. Despite this was a non standard procedure, the captain requested that the landing gear circuit breaker be switched off so he could extend the flaps earlier and prior to gear extension. Later on approach, the flight engineer completed the checklist and mistakenly confirmed that gear were down after the crew forgot to turn the circuit breaker on again. The captain continued the approach without proceeding to a verification/confirmation that gear were down, causing the aircraft to land on its belly. It slid for few dozen metres and came to rest with both engines n°2 and 3 on fire as well as the rear part of the cargo compartment. All 321 occupants were evacuated safely while the aircraft was damaged beyond repair.

The approach to Kuujjuaq-Fort Chimo Airport was stable but slightly below the VASIS descent profile. Just before the flare when power was reduced to idle, the crew was surprised by how rapidly the aircraft decelerated. Touchdown on the runway was hard. After the engines were shut down at the terminal, the crew noted structural deformations around the nose wheel attachment point and on the wings, where the deformations caused fuel to leak. Runway 31 slopes upward 1.3%. The landing was made at twilight, and the runway environment appeared very dark to the crew due to the lack of reflection from the gravel surface.

After takeoff from runway 01 at Guatemala City-La Aurora Airport, while climbing to a height of 200 feet, the twin engine aircraft rolled left and right then stalled and crashed beside the runway, about 550 metres from its end. The copilot and four passengers were injured while eight other occupants including the captain were killed. The aircraft was totally destroyed.

On final approach to Goiânia-Santa Genoveva Airport, the crew encountered poor weather conditions with a limited visibility due to rain. The aircraft landed about 500 metres past the runway threshold but as it was misaligned, the right main gear touched down on the left side of the runway. The crew attempted to steer the plane back onto the runway when the right main gear collapsed. The aircraft went out of control, lost its right engine then its nose gear and came to rest on the runway. All 67 occupants evacuated safely.

On take off from runway 11 at St. John's, the crew felt the nose of the aircraft rise to a high-pitch attitude. The aircraft climbed to about 150 to 200 feet, and was about to enter cloud when the crew reduced power. The crew lowered the nose, and force-landed the aircraft on the runway. The main gear, wings, engines and fuselage sustained substantial structural damage. Weather conditions at the time of the crash were reported as: winds 090° at 25 knots gusting to 35 knots, horizontal visibility 1/2 statute mile in light rain and fog, vertical visibility 100 feet, temperature 15° Celsius, dew point 15° Celsius, altimeter 29.31 Hg., pressure dropping.

The privately owned and operated Beech UC45-J was flying out of an outfitter's camp located near Swan Lake, Yukon Territory. The aircraft departed the clay-and-gravel strip for Mayo with one pilot, two passengers, luggage, and a reported load of 800 pounds of moose and caribou meat. The aircraft accelerated down the runway in a normal fashion, with the tail becoming airborne first. The aircraft left the surface of the runway and began a steep climb, followed by a yaw and bank to the left. The aircraft entered the Pleasant Creek valley off the end of the runway in a near-vertical, nose-down attitude. An explosion occurred, followed by a plume of smoke. Two persons immediately attempted to rescue the pilot and the passengers but discovered the aircraft partly submerged in the creek and engulfed in flames from the post-crash fire. There were no survivors.

Shortly after takeoff from Chichén Itzá Airport runway 28, while climbing to a height of about 500 feet, the aircraft rolled to the right, stalled and crashed in a wooded area located about one km past the runway end, bursting into flames. The aircraft was totally destroyed by a post crash fire and all 19 occupants were killed, among them US and Canadian citizens and three Mexican, both pilots and a local tourist guide.

During the takeoff roll at Lubumbashi-Luano Airport, a deflector located on the right main gear failed. The crew continued the takeoff procedure and after liftoff, the right main gear could not be raised in its wheel well. Initially, the crew decided to continue to Kinshasa in a 'gear down' configuration but eventually decided to return to Lubumbashi for a safe landing. After touchdown, the aircraft deviated to the right of the runway centerline then veered off runway and came to rest in a ditch. All three crew members escaped uninjured while the aircraft was damaged beyond repair.

After takeoff, the pilot reported "an engine problem," but did not elaborate. A witness on the ground saw that the left engine was trailing smoke, but the engine was still operating, and did not sound like it was "missing". When asked by the tower controller if he required assistance, the pilot answered "no". The controller cleared the pilot for left traffic to a landing, and provided the current weather. There were no further transmissions from the pilot. Smoothed radar tracking data revealed that the airplane turned toward a left downwind, and leveled off at 1,400 feet msl (about 1,050 feet agl) and 156 knots. During the next 14 seconds, the airplane descended to 1,100 feet and increased airspeed to 173 knots. Then radar contact was lost. Witnesses observed the airplane variously in a right snap roll and a left wingover, followed by a sharp dive to the ground. The airplane had just undergone maintenance. During maintenance, unused oil was found in the left engine cowling, which the pilot admitted he had previously spilled. Following maintenance, the pilot was observed adding 3 additional quarts of oil to the left engine. The engine oil dipsticks were calibrated on both sides, with each side pertaining to the oil level in a specific engine. The side for the right engine was calibrated to read 1 3/4 quarts lower than the left engine. The airplane's wreckage was fragmented. No evidence of mechanical defect was found, nor was there any evidence of an extreme out-of-trim condition. There was also no evidence of engine failure, detonation, or pre-impact failure. The pilot held an airline transport pilot certificate. He reported 3,210 hours of flight time to the operator, and had recently been cleared to fly the airplane on 14 CFR Part 91 flights. The flight to the maintenance facility was the pilot's first solo flight in the airplane. An autopsy of the pilot revealed the presence of a prostate adenocarcinoma; however, according to his physician, the pilot was unaware of it.