Landing (descent or approach)

The aircraft was damaged beyond repair when it veered off runway and the crew tried to get back on the runway without help. The aircraft went out of control, crossed the runway and hit the mast of a powerline and a parapet with more than 3.5 g, suffering structural damage. All 5 crew members and 22 passengers (19 of them illegal ones) escaped unhurt.

The Beechcraft 1900C, N87GL, was in its landing roll on runway 13, and the Beechcraft A90, N1127D, was in its takeoff roll on runway 04. The collision occurred at the intersection of the two runways. The flight crew of the Beechcraft 1900C had made appropriate efforts to coordinate the approach and landing through radio communications and visual monitoring; however they mistook a Cherokee pilot's transmission (that he was holding for departure on runway 04) as a response from the Beechcraft A90 to their request for the Beechcraft A90's intentions, and therefore mistakenly believed that the Beechcraft A90 was not planning to take off until after the Beechcraft 1900C had cleared the runway. The failure of the Beechcraft A90 pilot to announce over the common traffic advisory frequency his intention to take off created a potential for collision between the two airplanes.

The aircraft was approaching to land after completing a handling display during an Open Day at RAAF Richmond. At an altitude of about 800 feet, on the base leg for runway 28, both engines stopped simultaneously and without warning. As there was insufficient altitude to reach the field for a power off landing, the flaps and landing gear were retracted and a successful forced landing carried out into a cleared field short of the airfield. The crew evacuated the aircraft without injury.

The crew was completing a local training flight at Bahía Blanca-Comandante Espora Airbase. For unknown reasons, the aircraft landed on its belly and came to rest. Both pilots escaped uninjured.

The pilot was conducting the localizer approach to runway 15 when the aircraft overran the runway and struck an obstacle. According to the pilot, a loss of power occurred in both engines as he attempted to do a missed approach, and the airspeed subsequently decreased from 105 to 80 knots. The pilot reported that he pushed the nose over to avoid a stall, broke out of the clouds over the mid-point of the runway, landed long and continued off the end of the runway into terrain and a tower structure. A witness reported the 'aircraft broke out of the clouds just above the trees north of runway 5 and west of runway 15. Reportedly, the aircraft as being banked from a right to left to get aligned with runway 5, flaps appeared to be up, and the gear was down. The witness said the engines sounded to be at idle and at high rpm, and the aircraft appeared to be 50 feet above the ground at midfield when it went out of sight behind hangar.' The weather observed at the time of the accident was in part: ceiling 100 feet overcast, visibility 0.5 mile with fog and rain. The published landing minimums for the approach was ceiling 400 feet and visibility 0.75 mile. Recorded radar data of the flight indicated a descent below the minimum descent altitude at a constant airspeed. Both engines started immediately and ran during a postaccident check of the aircraft.

On approach to Ust-Nera Airport, following an uneventful flight from Khandyga, the crew mistook the new runway 85 (still under construction) for the operational runway 75 in poor visibility. When ATC realized this, they twice ordered the crew to go around but the crew failed to comply and touched down on runway 85. During the landing run, at a speed of 158 km/h, the captain attempted to go around but the check pilot aborted this attempt some seconds later. The confused flight engineer retracted the landing gear and the aircraft came to rest on its belly, suffering substantial damage. All 5 crew and 24 passengers escaped unhurt.

On final approach to Gods River Airport runway 27, the right main gear struck a snow berm located 105 metres short of runway threshold. The crew continued the approach and the aircraft landed 99 metres past the runway threshold. On touchdown, the right main gear collapsed. The aircraft slid fore few dozen metres then veered off runway to the right and came to rest. All seven occupants escaped uninjured while the aircraft was damaged beyond repair.

The approach to Flores-Santa Elena was completed in poor weather conditions. While descending at an altitude of 900 feet, the aircraft struck the slope of a mountain located 8 km from the runway threshold. All 14 occupants were killed, 13 citizen from Guatemala and one Mexican.

On final approach, the aircraft lost height and struck the ground short of runway threshold. The undercarriage were torn off and the aircraft bounced before coming to rest few dozen metres further. All 15 occupants escaped uninjured while the aircraft was damaged beyond repair. At the time of the accident, the total weight of the aircraft was nine tons above the maximum landing weight.

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.