Central America

The single engine aircraft was completing a local touristic flight with six passengers and a pilot on board. While flying at low altitude in the vicinity of the Samaná Bay, the aircraft collided with a coconut tree. The right wing was torn off and the aircraft crashed, killing all seven occupants. Weather conditions were good at the time of the accident.

After takeoff from San José-Tobías Bolaños Airport, en route to the Tortuguero National Park, while in initial climb, the aircraft stalled and crashed onto a house located in the district of Rohrmoser, about 3 km southeast of the airport. Four passengers were killed while 14 other occupants were injured, some seriously. Three people in the house, a nurse and two little girls were uninjured. Fifteen days after the accident, on January 30, the captain died from his injuries.

On December 31, 1999, at about 1055 Atlantic standard time, a Beech 99A, N491BB, registered to Alberta Aircraft Leasing Inc., operated by Bohlke International Airways, as a 14 CFR Part 135 on-demand air taxi, experienced a collapse of the main landing gear on landing at St. Barthelemy, (TFFJ) French Antilles. Visual meteorological conditions prevailed and no flight plan was filed. The airplane sustained substantial damage. The airline transport-rated pilot, copilot, and seven passengers reported no injuries. The flight originated from St. Croix, (STX) Virgin Islands, about 55 minutes before the accident. The accident was initially reported to the NTSB on January 5, 2000, by the FBI. The pilot stated they departed STX at about 1000. They had to make a 360-degree turn upon arrival at TFFJ due to other arriving traffic. They completed the descent arrival checklist and turned an 8- mile final. At a 1 1/2-mile final the flaps were lowered to the full down position, the propellers were set at 2,000 rpm, airspeed 95 knots, and all three landing gear lights were illuminated. On touchdown the airplane yawed to the left. Right rudder and aileron was applied with negative results. Power was increased and the airplane continued to yaw to the left. The airplane went off the left side of the runway and ground looped, separating the right main landing gear. The airplane came to a complete stop on its fuselage with the nose gear extended. They returned to the airplane on January 3, 2000. The airplane was lifted with a forklift and the left main landing gear was observed in the retracted position. A commuter pilot informed them that he observed the landing on the day of the accident. He stated he observed the left main landing gear moving forward and backwards.

While en route to the first schedule stop, the pilot heard a radio transmission that weather conditions in the vicinity of his next destination were 'bad.' Upon arriving, the pilot attempted to telephone Flight Service for a weather briefing and to file a flight plan. After efforts to contact Flight Service failed, the pilot elected to takeoff without a filing a flight plan. A few minutes into the flight, the pilot decided to return to the departure airport after the flight encountered deteriorating weather conditions that included heavy turbulence, and low ceilings. The airplane collided with trees as the pilot maneuvered the airplane. The post-accident examination of the airplane failed to disclose a mechanical malfunction or a component failure. The pilot did not report a mechanical problem with the airplane. A review of the en route flight charts disclosed that the terrain elevation at the departure point was approximately 24 feet. The terrain elevation at the approximate location of the accident site was 2,500 feet.

Following an uneventful flight from San Antonio, the pilot started a night approach to Monterrey-Del Norte. On final in good weather conditions, the twin engine aircraft crashed in unknown circumstances few km from the airfield. Both occupants were killed.

Leased from AOM French Airlines, the aircraft was completing a charter flight (service CU1216) from Havana to Guatemala City on behalf of Cubana de Aviacion, carrying 18 crew members and 296 passengers who were mostly young Guatemalan citizens studying medicine in Cuba. After touchdown on runway 19, the crew started the braking procedure but the aircraft was unable to stop within the remaining distance. It overran, went down an embankment and eventually crashed onto several houses located in the district of La Libertad. Both pilots, six other crew members, eight passengers and two people on the ground were killed. Also, 57 people were injured (among them 20 on the ground) while 261 other occupants escaped uninjured. The aircraft was destroyed.

The aircraft was completing a service from Tijuana to Mexico City with intermediate stops in Guadalajara and Uruapan, carrying 13 passengers and a crew of five. It departed Uruapan-General Ignacio López Rayón Airport runway 20 at 1859LT on the last leg to Mexico City. After liftoff, the crew was cleared to climb to 5,000 feet and while at an altitude of about 1,000 metres, the aircraft adopted a high angle of attack then stalled, entered a dive and crashed in an avocado plantation located 5,3 km from the airport. The aircraft disintegrated on impact and all 18 occupants were killed.

A Beechcraft 200 Super King Air, YV-385CP, crashed into the Atlantic Ocean about 9 miles southwest of Bimini, Bahamas, while on personal flight. Visual meteorological conditions prevailed in the area at the time, and an instrument flight rules flight plan was filed. The aircraft was destroyed, and the commercial-rated flight instructor and a pilot-rated passenger were both fatally injured. The flight originated from Fort Lauderdale International Airport, the same day, about 10:53. At 11:14, the pilot of YV-385CP told FAA ARTCC that he was experiencing an emergency, and he asked for immediate directions to Bimini. There were no further communications. According to radar information, at 11:13:33, the altitude was about 23,600 feet, and at 11:14:58 it had descended to 2,800 feet. Sound spectrum analysis of an FAA re-recording of communications between the pilot and ATC, indicated there were electronic signatures present, attributable to propeller noise, at cruise setting, for that type of aircraft. Records obtained from Venezuela indicated that earlier, YV-385CP had been involved in an accident, and had incurred extensive structural damage. The aircraft had been repaired in Venezuela, and was subsequently flown to the Unites States for additional repairs. Records obtained from the U.S. repair station indicated that the airplane incurred an extensive maintenance history, with needed repairs including damaged wiring, and leaks in the fuel system, as well as structural leaks, which had lead to several pressurization difficulties.

The four engine aircraft departed Santa Lucía AFB on a local training flight. While flying in clouds, the aircraft struck the slope of Mt La Paila (2,865 metres high) located about 57 km northeast of the airbase. All five crew members were killed.

On approach to a private airstrip located near Santa Catalina La Tinta, the twin engine aircraft crashed in unknown circumstances 300 metres short of runway. The aircraft was destroyed and all six occupants were killed. Weather conditions at the time of the accident were poor with low clouds and rain falls. Thunderstorm activity was reported all along the route.