Charter/Taxi (Non Scheduled Revenue Flight)

On April 3, 2002, about 1210 eastern standard time, a Cessna 402B, N768WC, registered to and operated by Southstream Aviation, Inc., was ditched in Coral Harbor Lake, southwest of the Nassau International Airport, Nassau, Bahamas. Visual meteorological conditions prevailed at the time and a VFR flight plan was filed for the 14 CFR Part 91 personal flight to Bimini, Bahamas. The airplane was substantially damaged and the commercial-rated pilot and a passenger were not injured. The flight originated about 6 minutes earlier from the Nassau International Airport. According to the passenger who is a U.S. certificated pilot, the airplane was fueled before takeoff. He checked the fuel tanks for contaminants after fueling; none were found. The flight departed from runway 14, then when turning on course to Bimini, the left engine sputtered. The pilot reduced then increased power from the left engine which then quit. He noted at that time the manifold and fuel pressure indications were decreasing. The pilot then turned back towards the Nassau airport to return when the right engine quit. Unable to return to the airport, the pilot ditched the airplane in the lake; the airplane remained upright in the approximately 1-4 feet deep water. Both occupants exited the airplane unaided. The accident site was located approximately 2.6 nautical miles southwest of the Nassau International Airport.

The MU-300 on-demand passenger charter flight sustained substantial damage during a landing overrun on a snow/ice contaminated runway. The captain, who was also the company chief pilot and check airman, was the flying pilot, and the first officer was the non flying pilot. Instrument meteorological conditions prevailed at the time of the accident. Area weather reporting stations reported the presence of freezing rain and snow for a time period beginning several hours before the accident. The captain did not obtain the destination airport weather observation until the flight was approximately 30 nautical miles from the airport. The flight received radar vectors for a instrument landing system approach to runway 30 (5,401 feet by 100 feet, grooved asphalt). The company's training manual states the MU-300's intermediate and final approach speeds as 140 knots indicated airspeed (KIAS) and Vref, respectively. Vref was reported by the flight crew as 106 KIAS. During the approach, the tower controller (LC) gave the option for the flight to circle to land or continue straight in to runway 30. LC advised that the winds were from 050-070 degrees at 10 knots gusting to 20 knots, and runway braking action was reported as fair to poor by a snow plow. Radar data indicates that the airplane had a ground speed in excess of 200 knots between the final approach fix and runway threshold and a full-scale localizer deviation 5.5 nm from the localizer antenna. The company did not have stabilized approach criteria establishing when a missed approach or go-around is to be executed. The captain stated that he was unaware that there was 0.7 percent downslope on runway 30. The company provided a page from their airport directory which did not indicate a slope present for runway 30. The publisher of the airport directory provided a page valid at the time of the accident showing a 0.7 percent runway slope. Runway slope is used in the determination of runway performance for transport category aircraft such as the MU-300. The airplane operating manual states that MU-300 landing performance on ice or snow covered runways has not been determined. The airplane was equipped with a cockpit voice recorder with a remote cockpit erasure control. Readout of the cockpit voice recorder indicated a repetitive thumping noise consistent with manual erasure. No notices to airman pertaining to runway conditions were issued by the airport prior to the accident.

While cruising at an altitude of 3,000 feet on a charter flight from Cienfuegos to Cayo Coco, the single engine aircraft entered an uncontrolled descent and crashed in a prairie located near Santa Clara. The aircraft was totally destroyed and all 17 occupants were killed, among them 6 Canadians, five British, two German while all four crew members were Cuban. It was reported that the left upper wing detached while the aircraft was encountering strong winds.

During an instrument approach, upon descending to the prescribed minimum descent altitude, about 1/2 mile from the missed approach point, the pilot failed to maintain flying airspeed. The airplane stalled, rolled left, and in an uncontrolled descent collided with a commercial building 0.96 nm from the runway's displaced threshold. The accident occurred during the return portion of a round trip flight, while on final approach to the pilot's alternate airport due to a weather-induced diversion. Moderate intensity snow showers and freezing fog existed. During the initial approach, the reported visibility was 1 1/2 miles. About the time the pilot passed the final approach fix, the visibility decreased to 1/2 mile, but the pilot was not informed of the decrease below his 1-mile minimum requirement. The pilot had maintained the recommended 140-knot approach speed in the icing conditions until about 3 1/2 miles from the runway. Thereafter, the airplane's speed gradually decreased until reaching about 75 knots. After the airplane started vibrating, the pilot increased engine power, but his action was not timely enough to avert stalling. Company mechanics maintained the airplane. On previous occasions overheat conditions had occurred wherein the environmental ducting melted and heat was conducted to the adjacent pneumatic tube that provides deice air to the empennage boots. During the accident investigation, the deice tube was found completely melted closed, thus rendering all of the empennage deice boots dysfunctional.

The aircraft was completing a charter flight from Khartoum to Heglig on behalf of an oil company, carrying 12 passengers and four crew members. On final approach in good weather conditions, the aircraft was too low and struck the ground short of runway 34 threshold. The aircraft bounced then landed hard, causing the undercarriage to be torn off. The aircraft slid on its belly, veered off runway and came to rest in bushes. Al 16 occupants evacuated safely while the aircraft was damaged beyond repair. Wind was gusting to 23 knots at the time of the accident.

The aircraft was parked on the international departures apron at FALA, ready for a flight from FALA to Blantyre. The pilot assumed that the engineer had pressurised the hydraulic accumulator and therefore did not inspect it himself. When the passengers arrived, the pilot got in the aircraft and began the internal pre-start checks. The co-pilot removed the chocks after boarding the passengers, closed the door and then started to brief the passengers. At that moment the pilot noticed that the aircraft was rolling forward. Attempts to stop the aircraft were unsuccessful, the aircraft rolled forward, narrowly missed a hangar and a parked Bell Long-ranger helicopter next to the hangar, crossed the taxiway and finally stopped when entering a ditch between the taxiway and the runway. The pilot was the holder of a valid transport pilot’s licence and had the type endorsed in his licence. The operation of the hydraulic system was found to be satisfactory. The hand pump was used to pressurise the system after which the brakes could be applied successfully.

The twin engine aircraft was completing a charter flight from Caracas to Los Roques, carrying 12 passengers and two pilots, among them seven Italian tourists. Over the Los Roques Island, the crew encountered technical problems and attempted to ditch the aircraft off Larga Island. All 14 occupants were quickly rescued while the aircraft sank by a depth of four metres and was damaged beyond repair.

On Saturday, 19 January 2002, at 0931, ZK-SEV, a Cessna 207, took off from Te Anau Aerodrome for Milford Sound Aerodrome. At about 1000 the aircraft collided with the side of a mountainous valley, approximately 4400 feet above sea level and 500 metres southeast of Gertrude Saddle, some 11 kilometres from Milford Sound. The pilot and 5 passengers on board died in the collision. The aircraft probably had not reached a suitable altitude to safely cross over Gertrude Saddle, and the pilot probably left his decision too late to turn back in the valley in order to gain more height.

On January 18, 2002 at 1440 eastern standard time, a Britten-Norman BN2-A, N616GL, operated by Fly BVI Inc,. under the provision Title 14 CFR Part 135, as a sightseeing flight, ditched off Beef Island, British Virgin Islands, following a loss of engine power on both engines. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was substantially damaged. The air transport pilot and his passengers were not injured. The flight departed Beef Island, British Virgin Islands, at 1400. According to the pilot, during a sightseeing tour the airplane experience a total loss of power on both engines at the same time. The pilot contacted the Beef Island control tower and declared an emergency and gave his position report. He then stated his intentions to ditch the airplane off the coast of Beef Island, British Virgin Islands. The airplane came to rest in six feet of water near the shoreline. During the examination of the airplane by personnel from the Department of Civil Aviation, British Virgin Islands, approximately 23 gallons of fuel were discovered in each fuel tank.

The twin engine aircraft departed Quito-Mariscal Sucre Airport at 1038LT on a charter flight to Nueva Loja-Lago Agrio Airport, carrying 21 oil workers and and five crew members on behalf of the Texaco Oil Company. While cruising under VFR mode at an altitude of 15,500 feet, the crew was instructed by ATC to change heading to 094° in order to descent to Nueva Loja for a landing on runway 23. But the crew failed to comply with this instruction and continued straight ahead. Few minutes later, the crew started the descent in foggy conditions when the aircraft struck the slope of Mt El Tigre located in the south part of Colombia, near the border with Ecuador. The wreckage was found three days later at an altitude of 4,500 metres. The aircraft disintegrated on impact and all 26 occupants were killed.