Short SC.7 Skyvan Variant

The pilot of Cessna 207A, N800GA, was returning to his company base, passing about 2 miles north of a remote airstrip that was along the route of flight. The airstrip did not have any control tower. [Communications around an uncontrolled airport are conducted on a common traffic advisory frequency (CTAF)]. The pilot of a Short SC7, N451SA, announced his departure from the same airstrip on the CTAF, and took off in a northerly direction. He then began a climbing right turn toward the same destination as the Cessna 207A was proceeding. The two airplanes collided in mid-air, about 1.49 nautical miles east-northeast of the airstrip, which was about 18.3 miles west of their destination. They were observed spiraling downward from about 800 ft above the ground. Both airplanes were found lying flat and upright on a frozen lake, entangled together at the accident site. The Cessna's burned wreckage was lying on top of (and positioned toward the aft third of) the burned wreckage of the Short SC7.

The pilot had flown this route in make and model airplane for nearly 4 years. He calculated 900 pounds of fuel were required for the flight, and saw 956 pounds on the fuel totalizer. The pilot was told by the ground controller of weather delays to his destination that ranged up to 2.5 hours. En route he was issued holding instructions with an EFC of 50 minutes later. After released from holding, 52 minutes after takeoff, the pilot was told that he was being vectored for a 35 mile final approach. The pilot then told the controller that he was fuel critical and the controller vectored him ahead of other airplanes. Ten minutes later, 84 minutes after takeoff, the controller asked his fuel status, and the pilot responded 'pretty low, seems like I'm losing oil pressure.' The pilot then advised the controller, 85 minutes after takeoff, that he shut down the right engine. He then declared an emergency and advised that he was not going to make the airport. Examination of the wreckage revealed the fuel tanks were intact, the fuel caps were secured, and the amount of fuel recovered from both tanks was 1.5 gallons, which was less than the specified unusable quantity. Company records showed that similar flights took about 48 minutes, and the airplane's average fuel flow was 580 pounds per hour.

The aircraft was dispatched at Hoogeveen Airport to perform local skydiving missions. While cruising at an altitude of 8,000 feet, both engines failed simultaneously. The crew ordered the skydivers to bail out and decided to return for an emergency landing. On final, the crew realized he could not make it and eventually completed an emergency landing in a potato field located about 500 metres short of runway. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

The pilot had departed a remote airstrip on the return portion of a cargo flight. An instrument flight plan was on file with the ARTCC. After departure, the pilot attempted to contact ARTCC to open his flight plan but communications were not established. The airplane struck mountainous terrain about 6 miles south of the departure airport. Radar data showed that after departure, the airplane climbed westbound and then turned southbound toward higher terrain. It circled southwest of the airport and turned eastbound while climbing to 5,300 feet msl. The airplane then turned southbound again toward the accident site. The last recorded radar data was at 5,200 feet msl. The airplane struck a ridgeline about 4,800 feet msl. Airmets were in effect for IFR conditions, low ceilings, mountain obscurations, rain, fog, and icing in clouds and in precipitation. A witness reported that when the airplane arrived at the airport, the airframe had a coating of ice. When the airplane departed, snow was falling at the airport.

The twin engine aircraft departed Hohenems-Dornbirn Airport on a local skydiving mission, carrying 23 skydivers and one pilot. After takeoff from runway 05, while climbing to a height of about 50 metres, the pilot encountered difficulties to gain height and elected to make an emergency landing when the right wing struck a tree. The aircraft stalled and crashed in an open field located 500 metres from the runway end. Four occupants, including the pilot, were injured. All 20 other occupants escaped uninjured. The aircraft was damaged beyond repair.

The twin engine aircraft departed Empuriabravia Airfield on a local skydiving mission. After all skydivers jumped, the pilot returned to the airport. On final approach, the pilot encountered engine problems and initiated a go-around procedure when the aircraft lost height, struck trees and crashed short of runway threshold. The pilot, sole on board, was killed.

On final approach to Vahun Airfield, at a height of 40 feet and at a speed of 77 knots, the twin engine aircraft adopted a high sink rate. The captain increased engine power when the aircraft rolled to the right, collided with trees and crashed few hundred metres short of runway. All 13 occupants were rescued and the aircraft was destroyed.

En route from Ba'kelalan to Marudi, weather conditions deteriorated and the visibility was poor due to heavy rain falls. The crew lost his orientation and due to fuel exhaustion, was forced to attempt an emergency landing. After landing in an open field, the aircraft struck a rock and crashed. One passenger was killed while 16 other occupants were rescued.

En route from Medan to Banda Aceh, the crew encountered poor weather conditions with limited visibility due to clouds. The crew informed ATC about his altitude at 8,500 feet when, three minutes later, the aircraft struck the slope of Mt Kapur located about 130 km northwest of Medan. The wreckage was found few hours later and all 14 occupants were killed.

The airplane rolled 200-300 feet before becoming airborne in a very nose high attitude. It maintained this attitude, made a right, then a left bank, and fell to the ground in a nose high attitude. The cargo consisted of eight 55-gallons drums of fuel, laid on their side and secured by one cargo strap running fore and aft and another cargo strap running diagonally across the barrels. The tie down ring ultimate strength rating was 1,600 pounds. The weight of the cargo was 2,863 pounds. Three of the cargo hooks associated with the cargo straps were found still attached to the tie down rings, and one hook and tie down ring were not located. Post-impact fire destroyed the cargo straps, and the barrels were strewn randomly through the cabin/cargo area. According to the manufacturer, the davis tie down ring installation is not approved by the manufacturer. The modification should have been accomplished under a supplemental type certificate. The logbooks showed only an entry. The certificated max gross weight was calculated to have been exceeded by 324.8 lbs. The pilot, sole on board, was killed.