De Havilland DHC-6 Twin Otter

The purpose of the flight was for the second pilot to perform an evaluation of the first pilot, who was recently designated by the operator as a backup pilot. Following several successful flights with and without passengers, the pilots discussed single engine operations, and the first pilot reduced the right engine's power to flight idle and feathered the propeller. During the final leg of the approach to landing, the airplane crossed over a fence near the runway threshold, and the first pilot pitched the airplane downward. The nose landing gear contacted the runway "hard," and the airplane began to bounce. After several bounces, the first pilot elected to abort the landing, increased power on the left engine to "full." As the first pilot pitched the airplane upward, it yawed to the right, "stalled," and impacted the ground.

The twin engine aircraft departed Timika-Moses Kilangin Airport at 1050LT on a 27-minutes flight to Enarotali, carrying 14 passengers and a crew of three. Some eight minutes into the flight, while cruising in poor weather conditions, the aircraft impacted hilly terrain. The wreckage was found two days later. The aircraft disintegrated on impact and all 17 occupants were killed. At the time of the accident, weather conditions were poor with low ceiling and rain falls.

On approach to Bimin-Wobagen Airport runway 30, the twin engine aircraft lost height and crashed in a wooded area. Both pilots (New Zealand citizens) were killed instantly and all 11 other occupants were injured, some seriously. They walk away to the village to find help and receive care. The aircraft has a single 11/29 grass/dirt runway located at an altitude of 1,767 metres and offer a 10° slope. Runway 29 is for landing only and runway 11 for takeoff only.

While descending to Ononge, the crew encountered poor weather conditions and decided to divert to the Yongai Airfield located about 27 km northeast of Ononge. Few minutes later, while cruising at an altitude of 2,286 metres in clouds, the twin engine aircraft struck the slope of a mountain. Rescuers arrived on scene a day later. The loadmaster was seriously injured while both pilots were killed.

The North-Wright Airways Ltd. DHC-6 Twin Otter, registration C-FMOL, was departing from an approximately 1,500 foot long gravel strip at Mile 222 of the Canol Road (near the Tsichu River), Canada. The takeoff was initiated to the north and into wind. Immediately after becoming airborne, the aircraft encountered a strong right cross-wind and settled back onto the strip. The left wheel contacted willows that had overgrown the edge of the strip. The aircraft veered left into the willows at about 60 knots, and began to decelerate. Prior to flying speed being regained, the aircraft rolled off the end of the strip and come to rest in a shallow creek. The right wing partially separated from the fuselage at impact and the forward fuselage, nose gear and right main gear sustained substantial damage. The pilot and first officer were uninjured. The purpose of the trip was to move hunting gear and outfitter supplies back to an airstrip at Mile 170 of the Canol Road (Godlin Lake). The aircraft was at or near gross weight at the time of the occurrence.

While descending to Lukla Airport from the south following a cargo flight from Kathmandu, the crew encountered poor visibility due to clouds when, at an altitude of 11,600 feet, the aircraft struck the slope of a mountain located near the Lamjura Pass, in the Solukhumbu district. The wreckage was found west of the airport and all three crew members were killed.

On final approach to Mulia Airport, during the last segment, the aircraft was caught by downdrafts and lost height, causing the nose gear to land first. The aircraft went out of control, ground looped and came to rest in a ditch. The pilot, sole on board, escaped uninjured while the aircraft was damaged beyond repair.

During the takeoff roll from a grassy runway (780 metres long), the pilot noted standing water on the ground. He attempted to take off prematurely to avoid these puddles but the aircraft stalled and crash landed. All three occupants escaped uninjured while the aircraft was damaged beyond repair.

The aircraft with a single pilot on board was performing firefighting operations in the vicinity of Lake Wicksteed, approximately 10 nautical miles north of Hornepayne, Ontario. The aircraft was scooping water from Lake Wicksteed for the nearby fire. The lake is approximately 7300 feet in length with gentle rising terrain along its shoreline. This was the third scooping from the lake, and the approach was flown in an easterly direction in light wind conditions. The pilot performed the inbound checks, lowered the water probes to begin filling the float water tanks, and touched down on the lake. Within a short time, he observed water spraying from the overflow vents located on top of the floats, indicating that the tanks were filled to capacity. He pressed a button on the yoke to retract the probes, and the aircraft immediately nosed over into the lake in a wings-level attitude and began to sink. The accident occurred at approximately 1800 eastern daylight time. The pilot extricated himself from the aircraft and held on to the side of the partially submerged aircraft. A witness to the occurrence immediately boarded a powered, aluminum boat and went to assist the pilot, while a second witness travelled to Hornepayne to notify the authorities and emergency services. Once the pilot reached the shore, he was taken to a nearby cottage where he remained until emergency services arrived. The aircraft came to rest on the bottom of the shallow lake in an inverted attitude with the floats above the surface of the water.

On final approach to Mulia Airport, the twin engine aircraft struck the ground and crashed few km short o runway. All four occupants were injured and the aircraft was damaged beyond repair.