Airport (less than 10 km from airport)

After landing at Kupang-El Tari Airport, the twin engine aircraft went out of control, veered off runway, lost its left wing and came to rest. All six occupants escaped uninjured while the aircraft was damaged beyond repair.

According to the passenger, he and the pilot had just taken off, and as they were climbing out over an open water portion of a bay, the pilot said, 'here comes a gust.' Reportedly, the pilot added engine power, and the airplane began descending. The right wing started to dip, and the nose started to drop. The pilot had the control yoke turned all the way to the left, then yelled that they were going in. The airplane crashed in the water, and the passenger exited the airplane through the windshield. He did not see the pilot. The deceased pilot was found still strapped in his seat several days later, when a portion of the wreckage was recovered.

Just after liftoff from Mirny Airport, while in initial climb, the reverse thrust system deployed on the right engine. The aircraft banked right, causing the right wing tip to struck the runway surface. Out of control, the aircraft crash landed, veered off runway and came to rest against a building. All 12 occupants escaped with minor injuries while the aircraft was damaged beyond repair.

The DC-3C took off on runway 10L and immediately executed a right turn followed by a left turn back toward the airport declaring a fire aboard. Dark night visual meteorological conditions existed. Witnesses observed 'flames' or an 'orange glow' coming from the right engine. A small number of aluminum fragments identified from the aft edge of the right engine accessory cowling were found along the ground just short of the ground impact site. These fragments displayed signs of heat distress but no significant melting. An examination of the right engine and accessory section revealed no evidence of a preimpact fire, and sooting and metal splatter on the leading edge of the right horizontal stabilizer was minimal. Spectral analysis of radio transmissions revealed no evidence of significant divergence of engine RPM between the two engines. Postcrash propeller examination revealed approximate blade pitch angles of 18-19° and 30-32° for the right and left propellers respectively upon impact. Propeller slash mark dimensions associated with the right propeller resulted in propeller RPM of approximately 1,750 to 2,570 over a range of 68 to 100 knots respectively. The first officer advised the PIC (broadcasting over the tower frequency) 'we're gonna stall' approximately 10 seconds before the impact. The aircraft was in a left turn back toward runways 28 left and right when the right wing struck the ground and the aircraft cartwheeled to a stop. A postcrash fire destroyed the cockpit area and inboard right wing.

The crew was completing a local training at Orléans-Bricy AFB. Following several circuits, the crew was attempting a new approach by night when the aircraft struck power cables, lost height and crashed in a field located near Chevilly, few km from the runway threshold. All three crew members were injured and the aircraft was destroyed. It was reported that the crew was forced to shut an engine down few seconds prior to the accident while flying in icing conditions. Despite the aircraft was established on the ILS, the crew was descending at an insufficient altitude. At the time of the accident, the visibility was limited.

Shortly after takeoff from Banjarmasin-Syamsudin Noor Airport, while climbing, the crew informed ATC about an engine fire and was cleared to return for an emergency landing. On final approach, the aircraft became unstable, rolled left and right then lost height and crashed on a factory located 2 km short of runway. A passenger was seriously injured while 16 other occupants as well as two people in the factory were killed.

On final approach to Fort Chipewayn Airport, the twin engine aircraft was unstable and rolling left and right. Upon landing, the right propeller struck the runway surface. The right engine partially torn off and the right wing was severely bent. The aircraft came to a halt few dozen metres further. All 14 occupants escaped uninjured.

Learjet L36A (serial number 033), N14TX, was on an instrument flight rules (IFR) flight from Grand Rapids, Michigan, to Stephenville, Newfoundland. At 0216 Newfoundland standard time (NST1), N14TX was cleared by Gander Area Control Centre (ACC) for an approach to the Stephenville airport. The co-pilot contacted the St. John=s Flight Service Station (FSS) and advised that they would be conducting an approach to runway 28. The FSS specialist relayed the latest Stephenville weather observation and runway surface condition report to the aircraft and requested that the crew advise St. John=s FSS when they had landed. When the crew of N14TX did not report after landing at Stephenville, the St. John=s FSS specialist advised Gander ACC that the aircraft was missing, and a search was begun. Initial information received by the agencies searching for the missing aircraft did not include the aircraft=s last recorded radar position. The wreckage was located approximately three hours and ten minutes after the aircraft was reported missing, within the airport perimeter, close to the last observed aircraft radar position. The aircraft struck a service road embankment in an inverted, wings-level attitude. The two crew members were fatally injured. The accident occurred during the hours of darkness at approximately 0238 NST.

On final approach to Nyagan Airport, the crew realized he was not properly aligned with the runway but decided to continue. Upon touchdown, the right wing struck the runway surface. The aircraft rolled left and right for about 800 metres then veered off runway and came to rest in a ravine. All 15 occupants were injured, six seriously.

Shortly after takeoff, the pilot radioed the air traffic control tower declaring an emergency and stating his intent to return for landing. He stated that he had taken off with an external boarding ladder attached to the aircraft. Several witnesses reported that the aircraft's downwind leg was too close to the airport causing the aircraft to overshoot the turn to the final approach course, and that the pilot increased the aircraft's bank angle as he tried to align the aircraft with the landing runway. As the aircraft was intercepting the final approach course, it abruptly rolled inverted, the nose dropped, and the aircraft spiraled onto the roof of an industrial building. A Boeing 757 aircraft, landing on the same runway, had passed over the accident site 2 minutes and 17 seconds earlier. The B-757 was cleared to land before the accident aircraft received a takeoff clearance and was on the runway when the pilot declared the emergency and turned downwind. The local controller did not issue a wake turbulence advisory. Experienced MS760 pilots reported that the aircraft will exhibit no adverse performance or safety affects with the boarding ladder attached.