Lake, Sea, Ocean, River

The aircraft, operated by Aéropro, was on a visual flight rules (VFR) flight from Sept-Îles, Quebec, to Wabush, Newfoundland and Labrador. The pilot, who was the sole occupant, took off around 0630 eastern daylight time. Shortly before 0700, the aircraft turned off its route and proceeded to Grand lac Germain to fly over the cottage of friends. Around 0700, the aircraft overflew the southeast bay of Grand lac Germain. The pilot then overflew a second time. The aircraft proceeded northeast and disappeared behind the trees. A few seconds later, the twin-engine aircraft crashed on the frozen surface of the lake. The pilot was fatally injured; the aircraft was destroyed by impact forces.

The aircraft was parked on the small apron at North Caicos Airport while the pilot went home to collect some personal items. One of the intended passengers saw the aircraft arrive. He remained in the vicinity until the pilot returned, and reported that the aircraft was unattended in the intervening time. When the pilot returned, four of the five passengers were gathered near the aircraft, and the last passenger arrived soon afterwards. The pilot, a local man well-known to the passengers, appeared to be his normal self and in good spirits. As most inter-island travel in the TCI is by air, the passengers were also familiar with the operator’s aircraft and used to travelling by air. Some had flown frequently on VQ-TIU. The pilot supervised embarkation and gave an emergency briefing. One passenger reported that the pilot made a mobile telephone call, which he presumed to be to Air Traffic Control (ATC) at Providenciales to notify them of the proposed flight. Prior to seating himself at the controls, the pilot told the passengers that they may expect some turbulence. The aircraft taxied onto the runway at its eastern end and along its length for a departure from Runway 08. It was about one hour after sunset and outside the airport’s normal operating hours, so there were no ATC personnel on duty. The runway lights were operated by the operator’s station manager. The aircraft took off at 1840 hrs. Soon after takeoff the aircraft was seen to start a turn to the right, which was consistent with its routing to Grand Turk, some 54 nm to the south-east. However, the aircraft reached a relatively large angle of bank and started to descend. The descent continued until it crashed with significant forward speed into an area of very shallow water. The aircraft broke up on impact, with the fuselage section coming to rest nearly inverted but comparatively intact. All those on board survived the impact sequence with varying degrees of injury. However, the pilot died before he could receive specialist medical treatment.

The commercial certificated pilot prepared for a VFR cross-country nonscheduled cargo flight under Title 14, CFR Part 135, by preflighting the wheel-equipped airplane and starting the engine. The airplane had been parked on the airport ramp overnight, with an electric engine heater and an engine cover on. A portion of the flight was over ocean waters to a remote village. After engine start, the pilot contacted the company owner and reported that the engine oil pressure appeared to be low, but within the operating range. The owner and the pilot discussed the possible reasons, such as cold ambient temperatures, which was about -20 degrees F. The pilot then departed, and reported to his company that the engine pressure was good. About 10 minutes later, he declared an emergency and stated he was ditching in the water, about 18 miles west of the departure airport. Retrieved track data from the pilot's GPS showed the airplane's maximum altitude was 1,439 feet msl, while crossing the ocean in an area that was about 22 miles wide. A review of the manufacturer's maximum glide distance chart revealed that from an altitude of about 1,500 feet, the airplane could glide about 2.1 nautical miles. The airplane was located about two hours after the accident, floating nose down next to a segment of pan ice, about 8.8 miles from the initial accident location. The pilot was not recovered with the airplane, and subsequent searches did not locate him. Following recovery of the airplane, examination of the engine revealed a 8 X 5 inch hole in the top of the case, adjacent to the number 2 cylinder. The number 2 connecting rod was broken from its crankshaft journal, and broken from the bottom of the piston. The number 1 connecting rod bearing was missing from its normal position on the crankshaft journal and the rod had evidence of high heat. Evidence of oil starvation and high heat signatures to several crankshaft and connecting rod bearings was found throughout the engine, along with a large amount of fragmented bearing material. The pilot was not wearing any personal flotation equipment, and the expected survival time in the 29 degree F ocean water was about 30 minutes. The company's operations manual does not contain a written policy requiring pilot's to maintain sufficient altitude to reach shore when crossing ocean waters.

On 1 January 2007, a Boeing Company 737-4Q8 aircraft, registered PK-KKW, operated by Adam SkyConnection Airlines (AdamAir) as flight number DHI574, was on a scheduled passenger flight from Surabaya (SUB), East Java to Manado (MDC), Sulawesi, at FL350 (35,000 feet) when it disappeared from radar. The aircraft departed from Djuanda Airport, Surabaya at 05:59 Coordinated Universal Time (UTC) under the instrument flight rules (IFR), with an estimated time of arrival (ETA) at Sam Ratulangi Airport, Manado of 08:14. The fuel endurance on departure from Surabaya was hours 30 minutes, and the crew had flight planned for an alternate of Gorontalo (GTO). The pilot in command (PIC) was the pilot flying for the sector to Manado and the copilot was the monitoring/support pilot. There were 102 people on board; two pilots, 4 cabin crew, and 96 passengers comprised of 85 adults, 7 children and 4 infants.

The pilot was ferrying the aircraft from Tauranga to a Hamilton maintenance facility when one of the engines failed. The pilot elected to turn back to Tauranga but, shortly after, the remaining engine failed. The pilot carried out a forced landing into a tidal estuary. The aircraft incurred substantial damage to the nose landing gear. Subsequent CAA safety investigation determined that on an earlier flight, the aircraft's electrical system incurred a defect that rendered several electrical components unserviceable, including the two tip/main fuel tank selector valves. No engineering inspection or rectification ensued and the operator ferried the aircraft from Great Barrier Island unaware that the engines were being fed from the tip tanks only. The operator departed Tauranga for Hamilton under similar circumstances, reaching the vicinity of the Kaimai Ranges when the tip tanks became empty.

The aircraft departed Pie de la Cuesta AFB on a routine flight ro Santa Lucia AFB near Mexico City. Few minutes after takeoff, the aircraft went out of control and crashed in the sea about 9 km southeast of the airbase. All four crew members were killed.

Shortly after takeoff from Flamingo Bay, the single engine aircraft crashed in the sea few dozen metres offshore. The pilot was injured and the aircraft was destroyed.

The twin engine aircraft departed Canouan Island Airport at 1842LT on a short flight to Kingstown, Saint Vincent & Grenadines, carrying one passenger and one pilot. Shortly after takeoff, the pilot was instructed to report once passing over Bequia Island. Few minutes later, after passing Bequia Island, the pilot contacted ATC and reported he was at the altitude of 1,100 feet with an ETA in Kingstown in four minutes. At 1853LT, the aircraft crashed in unknown circumstances in the sea. The next morning, few debris were found floating on water and no trace of both occupants was ever found. The passenger was the Director of American Eagle for the Canouan Island. All SAR operations were abandoned few days later and the wreckage was not found.

The crew departed Cancún Airport for a routine maritime patrol flight over the Gulf of Mexico. After 5 hours of flight, while returning to his base and approaching the coast, the crew informed ATC that an engine failed. Few seconds later, the second engine stopped as well. The crew reduced his altitude and ditched the aircraft 3,5 km off Progreso, some 40 km north of Mérida. All 7 occupants were rescued while the aircraft was lost.

Shortly after takeoff from Rottnest Island Airport, while in initial climb, the twin engine aircraft suffered a bird strike and crashed in a salt lake located near the airport. The aircraft was destroyed upon impact and all six occupants were injured.