Cessna 208B Grand Caravan

Shortly after takeoff from Xakanaka Airstrip on a taxi flight to the Pom Pom Camp located in the Okavango Delta, the single aircraft lost height and crashed, bursting into flames. The pilot and seven passengers were killed while four others were injured. The pilot was a British citizen as the seven passengers killed were respectively four Swedish, on British and two French. The aircraft was totally destroyed by a post crash fire. For unknown reasons, the aircraft caught fire shortly after takeoff.

The Air Tindi Ltd. Cessna 208B Caravan departed Yellowknife, Northwest Territories, at 1103 Mountain Daylight Time under visual flight rules as regularly scheduled flight Air Tindi 200 (8T200) to Lutsel K'e, Northwest Territories. When the aircraft did not arrive at its scheduled time, a search was initiated, and the aircraft was found 26 nautical miles west of Lutsel K'e, near the crest of Pehtei Peninsula. The pilot and one passenger were fatally injured, and two passengers were seriously injured. There was no post-impact fire, and no emergency locator transmitter signal was received by the Joint Rescue Coordination Centre or search aircraft.

A Cessna 208B Grand Caravan I was destroyed when it crashed in the Yahukimo District, Indonesia. Both crew members were killed. The airplane was being operated on a non-scheduled cargo flight from Wamena Airport to Kenyam Aerodrome in Papua, Indonesia. The flight was being conducted under visual flight rules (VFR) and the pilot reported to ATC that the planned altitude was 9,500 feet. On board the aircraft were two pilots, a manifested load of diesel drums and grocery items, and a non-manifested load of 25 bags of rice weighing 827 lb (375 kg). The takeoff weight, based on the manifested cargo and the additional load of rice was estimated by the investigation to be 9,681 lb (4,391 Kg) which was 619 lb (281 Kg) above the certificated maximum takeoff weight. Also, the aircraft Centre of Gravity (C of G) was outside the certificated C of G envelope. The aircraft took off from Wamena runway 15 at 12:17 local time. The aircraft was then flown along a track toward Kenyam which was consistent with the route used by other company pilots and previously flown by the pilot in command. The additional loading contributed to a reduced rate of climb during the flight which resulted in the aircraft being below 10,000 ft as it approached the high terrain. This altitude was 1,500 ft lower than the altitude specified in the operator's route guide for operations between Wamena and Kenyam, and lower than the altitude flown by other company pilots when operating in the area, including three other flights on the day of the accident which overflew the high terrain between 11,200 and 12,500 ft. At 12:29:43, as the aircraft approached the high terrain at an altitude of 9,538 ft, the airspeed commenced decreasing which was accompanied by the average rate of climb increasing to about 390 fpm. It is probable that the pilots recognized the proximity of the terrain and attempted to improve the aircraft's angle of climb by decelerating towards the best angle of climb speed of 72 kts. The recorded data showed that 31 seconds after the airspeed started to decrease, the engine power varied with a maximum engine torque of 1,675 ft/lb being recorded at 12:30:30 with changes in the other engine parameters being consistent with a selection of a higher power setting. This is likely to have been associated with the pilot's attempts to improve terrain clearance. The recorded data then showed the aircraft in a descending right turn for about 6 seconds. The altitude reduced over a period of 4 seconds from 9,865 ft to 9,728 ft at an average rate of descent of about 2,000 fpm. This turn was likely to have been initiated to either avoid cloud or improve terrain clearance. The aircraft subsequently commenced to roll to the left at 12:30:35 with the left roll continuing for the following 14 seconds. It was likely that the left turn was initiated to avoid either cloud or terrain. During the left turn, the angle of bank reached a maximum value of 46° and the aircraft descended from 9,728 ft to 9,045 ft at a high rate of descent. The airspeed also increased from 92 kts to 122 kts during the descent. The engine power was reduced to idle soon after the aircraft commenced descending which was most likely due to the handling pilot attempting to recover from the high descent rate and increasing airspeed. The recorded data indicated that three EGPWS alerts activated during the descent. The aircraft had stopped descending at 12:30:50 and had commenced climbing with a reducing left angle of bank when the airplane impacted terrain at an elevation of 9,100 feet.

A Cessna 208B and a Cessna 207 collided in flight in daylight visual meteorological conditions. The Cessna 208B and the Cessna 207 were both traveling in an easterly direction. According to the Cessna 207 pilot, the airplanes departed from two neighboring remote Alaskan villages about the same time, and both airplanes were flying along similar flight routes. While en route, the Cessna 207 pilot talked with the Cessna 208B pilot on a prearranged, discreet radio frequency, and the two agreed to meet up in flight for the return to their home airport. The Cessna 207 pilot said that the pilot of the Cessna 208B flew his airplane along the left side of her airplane while she was in level cruise flight at 1,200 feet mean sea level and that they continued to talk via the radio. Then, unexpectedly and unannounced, the pilot of the Cessna 208B maneuvered his airplane above and over the top of her airplane. She said that she immediately told the Cessna 208B pilot that she could not see him and that she was concerned about where he was. She said that the Cessna 208B pilot then said, in part: "Whatever you do, don't pitch up." The next thing she recalled was seeing the wings and cockpit of the descending Cessna 208B pass by the right side of her airplane, which was instantly followed by an impact with her airplane's right wing. She said that after the collision, the Cessna 208B passed underneath her airplane from right-to-left before beginning a gradual descent that steepened as the airplane continued to the left. It then entered a steep, vertical, nose-down descent before colliding with the tundra-covered terrain below followed by a postcrash fire. Unable to maintain level cruise flight, the Cessna 207 pilot selected an area of rolling, tundra-covered terrain as a forced landing site. An examination of both airplanes revealed impact signatures consistent with the Cessna 208B's vertical stabilizer impacting the Cessna 207's right wing. A portion of crushed and distorted wreckage, identified as part of the Cessna 208B's vertical stabilizer assembly, was found embedded in the Cessna 207's right wing. The Cessna 208B's severed vertical stabilizer and rudder were found about 1,000 feet west of the Cessna 208B's crash site.

The single engine aircraft departed Canoas AFB in Porto Alegre at 1145LT on a flight to Rio de Janeiro-Galeão Airport, carrying six officers and two pilots on behalf of the 5th Air Transport Squadron. While cruising over the State of Santa Catarina, the crew encountered limited visibility due to poor weather conditions when the aircraft impacted a mountain near Bom Jardim da Serra. The aircraft disintegrated on impact and all 8 occupants were killed.

The Beaver Air Services Limited Partnership Cessna 208B (registration C-FMCB serial number 208B1114), operated by its general partner Missinippi Management Ltd (Missinippi Airways), was departing Pukatawagan, Manitoba, for The Pas/Grace Lake Airport, Manitoba. At approximately 1610 Central Daylight Time, the pilot began the takeoff roll from Runway 33. The aircraft did not become fully airborne, and the pilot rejected the takeoff. The pilot applied reverse propeller thrust and braking, but the aircraft departed the end of the runway and continued down an embankment into a ravine. A post-crash fire ensued. One of the passengers was fatally injured; the pilot and the 7 other passengers egressed from the aircraft with minor injuries. The aircraft was destroyed. The emergency locator transmitter did not activate.

The pilot, sole on board, departed Barra do Vento Airport on a ferry flight to Boa Vista-Atlas Brasil-Cantanhede Airport, Roraima. Shortly after rotation, he noticed abnormal vibrations. At the same time, the 'door warning' light came ON on the instrument panel. He decided to land back but lost control of the airplane that veered off runway to the right and collided with an earth mound, bursting into flames. The aircraft was totally destroyed by a post crash fire and the pilot was seriously injured.

The single engine aircraft departed Lensk at 0813LT on a flight to Bratsk. While cruising at 4,200 metres over the cloud layer, the engine failed. The crew elected to divert to Kirensk Airport but was unable to maintain a safe altitude. Eventually, the captain attempted an emergency landing when the aircraft impacted trees and crashed in a wooded area located 37 km west of Kirensk. All nine occupants were injured and the aircraft was damaged beyond repair.

Shortly after takeoff from Felipe Carrillo Puerto Airport, while in initial climb, the single engine airplane entered an uncontrolled descent and crashed nose first in a wooded area located past the runway end. The aircraft was destroyed and all 9 occupants were killed, among them 7 members of the campaign team of the candidate for Governor of Quintana Roo, Roberto Borge.