Christiansted

The airplane was making a public use flight between two islands for the purpose of transporting residents of a correctional facility to court hearings. During descent to the destination airport, at an altitude of approximately 1,400 feet, both engines started surging. The pilot's attempts to restore normal engine power were unsuccessful, and he ditched the airplane in ocean water with both engines still surging. The airplane stayed afloat as he and the passengers exited, and then it sank. The airplane was not recovered from the ocean, precluding its examination and determination of the reason for the dual loss of engine power.

The flight was being handled as a VFR aircraft by air traffic control, was given a discreet transponder code, and was radar contact at an altitude of 4,500 feet. The pilot requested a VFR descent from 4,500 feet, and was cleared to "…descend unrestricted west bound." Radar and radio contact were lost at an altitude of 2,700 feet. The controller tried to re-establish radio contact with the airplane's pilot 10 times before initiating search and rescue efforts. A U.S. Coast Guard helicopter found the wreckage, using the aircraft's emergency locator transmitter. The next day a ground search for the aircraft was halted because of hazardous terrain. Search and rescue personnel had to be airlifted into the crash site to remove the victim. A police helicopter was vectored to the crash site by ATC about an 1 1/2 hours after contact was lost with the flight, and the pilot reported that he could not fly near the crash site because of fog. He reported the ceiling about 2,400 feet. The aircraft impacted in heavily wooded, mountainous terrain at the 2,700-foot level of a 3,524-foot mountain. Toxicology test showed that venlafaxine and desmethylvenlafaxine drugs were found in the pilot's blood, and the levels found were consistent with the recent ingestion of more than 10 times a normal dose of venlafaxine.

After departure from San Juan, the pilot of N405MN contacted the FAA San Juan Approach Control, was identified on radar by the controller, and told to climb to 7,000 feet. About 1 minute later, the pilot is told to proceed direct to St. Croix. About 4 minutes later, the pilot requested radar vectors to St. Croix, and was told to fly heading 140 degrees. Radar data showed the flight leveled at the cruise altitude of 7,000 feet at about 0444. At about 0453:36, the pilot requested a lower altitude, and was cleared to 2,000 feet. The pilot acknowledged the clearance, and no further transmissions were received from the pilot. The flight began descent from 7,000 feet at about 0454. At 0454:29, the aircraft's transponder reports the flight is at 6,500 feet. At 0454:41, the transponder reports the flight is at 5,600 feet, and at 0454:49, at 4,000 feet. At 0454:53, the transponder reports the flight is at 1,100 feet. The flight is not observed on radar after this. No other aircraft or radar returns are observed near the flight as it began it's descent. One main landing gear tire, wheel, and brake assembly; the left wing lower skin from the area above the wing flap; the left wing baggage compartment door; the right nose baggage compartment door; the cabin floor cover; and some items from the U.S. mail cargo, were recovered floating in the ocean, at points north of the last observed radar contact with the airplane, on the day of the accident and in the days after the accident. The recovered components had damage from being separated from the airplane. None of the recovered components had any fire, heat, or soot damage. The remainder of the airplane was not located and recovered. The depth of the sea in the area of the accident site was reported by the Coast Guard to be about 6,000 feet. U.S. Post Office personnel reported the flight carried 1,517 pounds of U.S. mail. No hazardous materials were in the mail. A 75-pound pouch of mail was recovered from the ocean and identified as having been placed on N405MN. The weather at the time of the accident was reported to scattered clouds with visibility 10 miles.

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.

On April 7, 1996, about 0600 Atlantic standard time, N143SA, a De Havilland DH6, operated by Dolphin Express Airlines crashed on takeoff roll at Virgin Gorda Airport, British Virgin Islands. The flight was a 14 CFR Part 135 scheduled international passenger commuter flight. Visual meteorological conditions prevailed at the time and a VFR flight plan was filed. The airplane was substantially damaged and the captain, first officer, and eight passengers reported no injuries. One passenger received minor injuries. The flight was originating at the time of the accident. The captain stated the while on takeoff roll the airplane veered sharply to the left and she could not exercise directional control. The airplane then departed the runway and crashed through a fence, ripping one wing off the airplane. The airplane was equipped with a CVR that is being removed for further readout.

The pilots lost aileron control shortly after takeoff while in a left turn. The left turning tendencies of the aircraft could not be corrected and the aircraft crash landed in the Caribbean Sea. Post crash inspection of the aircraft revealed the left aileron control cable was trapped within a bundle of electrical wires and cables. This occurred when an electrical cable from a reverse current relay in the right wing to the main junction box in the left cabin area at the center wing was changed and secured. The aileron cable chafed through the protective cover of the large electrical cable. When contact was made with the metal electrical cable the aileron cable arched at several points and separated at two different points causing a loss of aileron control. A passenger was killed while 14 other occupants were rescued.

Flight 901A departed the ramp in Vieques about 0755 with eight passengers aboard, all of whom had reserved seats and purchased tickets for Flight 901. The pilot of Flight 901A contacted the UNICOM as he taxied out to the takeoff end of runway 09. The UNICOM operator informed hym that there was no other traffic in the area. According to a mechanic at the airport, after takeoff, the airplane appeared to climb out normally; however, he said that as the airplane turned left in a crosswind departure pattern, it appeared to lose power when about 200 feet above the ocean. He stated that the airplane then gained about 50 feet, while in a nose-high attitude, and that he then heard the engines develop more power, before the plane descended into the ocean. The airplane had crashed into the ocean north of the departure end of runway 09 and about 1/2 mile off shore. The aircraft was destroyed and all nine occupants were killed.

The four engine airplane was completing a cargo flight from Christiansted to Charlotte Amalie, carrying two passengers and three crew members. While on a night visual approach to runway 09 at Charlotte Amalie-Harry S. Truman Airport, the made a 360° turn to avoid traffic when the airplane lost altitude and crashed into the sea about two miles short of runway threshold. Both passengers were injured while all three crew members were killed.

The seaplane was engaged in a test flight out from Christiansted on behalf of the FAA. While flying off Christiansted, the pilot encountered engine problems and decided to ditch the aircraft few miles offshore. All three occupants were rescued while the aircraft was damaged beyond repair.

While approaching Charlotte Amalie Airport on a cargo flight from Christiansted, the aircraft went out of control and crashed into the sea few km offshore. SAR operations were initiated but eventually abandoned after few days as no trace of the aircraft nor the pilot was found.