Caribbean Sea

While delivering the single-engine, turbine-powered airplane to Brazil during a multiple leg trip, the pilot decided to fly direct from his departure airport in Puerto Rico to his destination airport in Grenada instead of following the island chain and staying within power-off gliding distance of the shore. During the cruise portion of the flight, a total loss of engine power occurred over open water in visual meteorological conditions at 27,000 feet, about 119 miles west of a suitable landing area. During the loss of power, the engine torque indication dropped from the cruise power setting to 0 foot-pounds (ft-lbs) of torque, the engine then began to vibrate, and smoke began emanating from the engine. The pilot ditched the airplane, it sank, and it was not recovered. The pilot and the pilot-rated passenger were rescued by a French Navy helicopter. The pilot said that he had decided to take a direct route instead of staying closer to the island chain between the two airports because he had ferried 3 airplanes down to Brazil in the last year and that it was a judgment call and a calculated risk because the engine was reliable. At the airplane’s planned operating altitude of 27,000 feet, the airplane could have glided about 54 miles; if the route had been planned to take advantage of this glide distance, the pilot could have remained off shore island chain and taken a shorter, although not direct, route. Review of fueling documentation, the Pilot's Operating Handbook (POH), and statements made by the pilot and pilot-rated passenger also revealed that on the accident flight, good operating practices were disregarded. For instance, during fueling, the airplane which was not equipped with fuel heaters, had been topped off with fuel, but no fuel icing additive had been added, even though the pilot was planning to operate the airplane at 27,000 feet. The airplane was also operated in excess of the manufacturer's published weight limitations, and no power setting or performance information was available for climb and cruise operations in excess of these limitations. Furthermore, according to the pilot, before the loss of engine power, the torque was about 937 ft-lbs. According to the pilot-rated passenger, before the failure, the torque gauge was indicating about 980 ft-lbs. Review of the maximum cruise performance chart in the POH and Airplane Flight Manual (AFM) revealed that both of the stated torque settings exceeded the maximum torque setting listed on the chart. Operating the engine beyond the recommended power settings specified in the POH/AFM for a prolonged period will result in accelerated deterioration due to hot section component distress and will affect engine reliability and durability.

The pilot departed on a VFR flight behind another company airplane. About 5 minutes after takeoff, the pilot informed the pilot in the lead airplane that he was having a generator problem, and that he would monitor them. The lead airplane landed at a different airport, and waited for the other pilot to join him after dropping off his passengers at another airport. The pilot did not arrive at either airport. All shipping vessels along the airplane's expected course were requested to report any sightings. No contact was reported and the search was terminated. Aircraft damage and injuries are presumed.

The pilot stated he noted a loss of oil pressure and a partial loss of power of the right engine during cruise flight. The engine then lost power, and the pilot was unable to feather the right propeller. The airplane would not maintain altitude and the pilot ditched the airplane about 75 miles southeast of St Croix. After exiting the airplane, the pilot inflated a raft, and was found by rescue personnel about 4 hrs later. The airplane was not recovered.

While cruising by night on a cargo flight from Willemstad-Hato Airport to Miami-Intl Airport, the four engine aircraft entered an uncontrolled descent and crashed in the Caribbean Sea. Few debris floating on water and the dead body of the copilot were found about 210 km northwest of Curaçao Island. The aircraft was flying in poor weather conditions with thunderstorm activity and turbulences when the accident occurred.

The Beech 65-88 airplane was reported missing on February 7, 1988. It was on an IFR flight from Aruba to Santo Domingo, Dominican Republic. The airplane departed from Aruba approximately 1223Z. According to air traffic authorities in Santo Domingo, the airplanes last reported position was over the DUSAN intersection at 1340Z. The airplane has not been located, and remains missing. No additional information is available.

En route, the crew encountered an unexpected situation and was forced to ditch the aircraft in the Caribbean Sea. The crew of a boat was quickly on the scene and able to evacuate all three crew members alive. The airplane sank and was lost.

The flight departed Anguilla at 0803 ast. At 0805 the pilot radioed St. Maarten and filed a VFR flight plan to St. Thomas. The flight plan showed a direct route of flight at 4,500 feet msl with a time enroute of 45 minutes. The flight failed to arrive at the destination. Search efforts were suspended on October 23 with negative results. Pilots flying in the area on the accident date reported that at 0920 there was a line of thunderstorms extending northwest from St. Maarten to the Antigua area. The line of thunderstorms had a base as low as 1,000 feet with continuous heavy rain below. The aircraft damage and injuries are presumed.

The airplane was on a ferry flight from Guyana to Quebec (St Jean) following a 15 months period of storage in Guyana. While cruising south of Barbados Island, the crew informed ATC that an engine failed while the second was overheating. Few minutes later, the airplane crashed in the Caribbean sea about 77 km south of Bridgetown. SAR operations were initiated but eventually abandoned few days later as no trace of the aircraft nor the three crew members was found.
Crew:
Dave Holland, pilot,
Grant Davidson, pilot,
Richard Cusson, flight engineer.

En route from Santa Marta to Port-au-Prince, the twin engine airplane disappeared from radar screens and crashed in unknown circumstances into the Caribbean Sea. The airplane and both occupants were never found.

The four engine airplane departed San José-Juan Santamaría Airport at 1400LT on a cargo flight to Caracas, carrying one passenger, three crew members and a load of 16,330 kilos of frozen meat. While in cruising altitude over the Caribbean Sea, the airplane plunged into the sea in unknown circumstances, about 65 km east of Bocas del Toro, Panama. SAR operations were initiated but eventually suspended few days later as no trace of the airplane nor the four occupants was found.