Christiansted-Henry E. Rohlsen (ex Alexander Hamilton)

Following an uneventful cargo flight from Christiansted-Henry E. Rohlsen Airport, the crew completed the landing normally at San Juan-Luis Muñoz Marin Airport. While taxiing to the ramp, the nose gear collapsed and the aircraft came to rest. Both pilots escaped uninjured and the aircraft was damaged beyond repair.

The flight departed VFR, and when near the destination airport, was advised by air traffic control to hold VFR over the "plaza" and to make left 360 degree orbits. Several witnesses reported light rain was occurring at the time of the accident; there was no lightning or thunder. One witness located where the airplane came to rest reported observing the airplane emerge from the base of the clouds in a 45-degree left wing low and 20 degrees nose low attitude. He momentarily lost sight of the airplane but then noted it rolled to a wings level attitude. He also reported hearing the engine(s) "cutting in an out." Another witness located approximately 1/4 mile north of the accident site observed the airplane flying eastbound beneath the clouds in a right wing and nose low attitude, he also reported hearing the engine(s) sounding like they were "cutting in and out." A pilot-rated witness located an estimated 1,000 feet from where the airplane came to rest estimated that the ceiling was at 300 feet and there was light drizzle. He observed the airplane in a 45-degree angle of bank to the right and in a slight nose low attitude. He stated that the airplane continued in that attitude before he lost sight of the airplane at 250 feet. The airplane impacted trees then a concrete wall while in a nose and right wing low attitude. The airplane then traveled through automobile hoists/lifts which were covered by corrugated metal, and came to rest adjacent to a building of an automobile facility. Impact and a post crash fire destroyed the airplane, along with a building and several vehicles parked at the facility. Examination of the airplane revealed the flaps were symmetrically retracted and landing gears were retracted. No evidence of preimpact failure or malfunction was noted to the flight controls. Examination of the engines revealed no evidence of preimpact failure or malfunction; impact and fire damage precluded testing of several engine accessories from both engines. Examination of the propellers revealed no evidence of preimpact failure or malfunction. Parallel slash marks were noted in several of the corrugated metal panels that covered the hoists/lifts, the slashes were noted 25 and 21 inches between them. According to the airplane manufacturer, the 25 inch distance between the propeller slashes corresponds to an airspeed of 123 knots. Additionally, the power-off stall speed at the airplanes calculated weight with the flaps retracted and 48 degree angle of bank was calculated to be 122 knots. Review of NTSB plotted radar data revealed that the pilot performed one 360-degree orbit to the left with varying angles of left bank and while flying initially at 1,300 feet, climbing to near 1,500 feet, then descending to approximately 800 feet. The airplane continued in the left turn and between 1502:10 and 1502:27, the calibrated airspeed decreased from 160 to 100 knots. At 1502:27, the bank angle was 48 degrees, and the angle of attack was 26 degrees. Between 1502:30 and 1502:35, the true heading changed indicating a bank to the right. The last plotted altitude was 200 feet, which occurred at 1502:35. A NTSB weather study indicated that at the area and altitude the airplane was operating, NWS VIP level 1 to 2 echoes (light to moderate intensity) were noted. Additionally, the terminal aerodrome forecast (TAF) for the destination airport indicated that temporarily between 1400 and 1800 (the flight departed at approximately 1436 and the accident occurred at approximately 1503), visibility 5 miles with moderate rain showers, scattered clouds at 1,500 feet, and a broken ceiling at 3,000 feet.

As the flight made a visual approach to the airport from the south over the sea, at night, the pilot changed his navigation radio from the VOR to the ILS system for runway 10 and lost DME reading from the VOR located on a hill north of the localizer course. The localizer showed the flight was south of the localizer course, and without DME from the VOR the pilot believed he was much closer to the island and the airport than the aircraft actually was. As the pilot attempted to make visual contact with the airport and maintain clearance from the hills he allowed the aircraft to descend and crash into the sea about 3 miles southwest of the airport. The pilot had not filed a FAA flight plan for the scheduled commuter flight. The pilot had been flying the route for 5 days and had no previous experience in the area. The pilot reported he had no mechanical malfunctions with the aircraft systems, flight controls, or engines. No FAA Operations inspectors had conducted surveillance on the company's flight operations in the Caribbean since service had begun in December 1996.

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.

The aircraft crash landed during a touch and go landing. The pilot said that the aircraft was caught in a windshear or violent downdraft and would not climb. He did not say why he was doing a touch and go landing with 9 passengers on board. The pilots account of the accident was: after touchdown I raised the flaps and set takeoff power. At 103 knots and with 500 feet of runway remaining the aircraft was lifted off. At about 150 feet agl and climbing I started to raise landing gear but the aircraft started to sink so I left gear down. The trees were moving violently. I felt I was caught in a windshear because of a sharp drop in airspeed and the aircraft quit performing. The aircraft continued sinking and I decided on a controlled crash to save the passengers. A witness stated he (the pilot) took off without enough power. I saw the plane with its nose high and tail low and I lost the plane when it went into the trees. The aircraft hit several citrus trees at a shallow angle of descent 1,200 feet from the end of the runway. The aircraft went 150 feet through the trees and 350 feet on the ground before stopping. All 11 occupants escaped uninjured.

On final approach to Christiansted-Alexander Hamilton Airport, the twin engine airplane rolled to the left and descended until it crashed, bursting into flames. The aircraft was totally destroyed and all four occupants were killed.

After takeoff from Christiansted-Henry E. Rohlsen Airport, while climbing on a cargo flight to Miami, the crew declared an emergency after the engine n°3 caught fire. The crew was cleared to return for an emergency landing, was able to extinguish the fire and to feather the propeller. Then the crew encountered controllability problems and the captain decided to ditch the aircraft few km offshore. Two crew members were rescued while the copilot drowned. The aircraft sank about 45 minutes later.

After takeoff from Christiansted-Alexander Hamilton Airport, while in initial climb, the pilot reported engine problems and elected to return. He completed a turn when the airplane struck trees and crashed into the sea few dozen yards offshore. All 10 occupants were evacuated, among them three were seriously injured. The aircraft was destroyed.

The airplane crashed on the airport while executing a takeoff from the Alexander Hamilton Airport, Christiansted, St. Croix, USVI. There were 19 passengers and 2 crew members on board. The first officer and 7 passengers were killed, and the captain and 12 passengers were injured seriously. The aircraft was destroyed. Witnesses saw the aircraft assume a nose-high attitude shortly after takeoff. The aircraft then began to roll to a left then to a right wing-down attitude, followed by a momentary pitchdown. The aircraft then pitched up and oscillated to a left wing-down and then a right wing down attitude while losing altitude. It struck the ground while in a right wing-down attitude. The gross weight of the aircraft at takeoff was found to be 1,060 lbs over its maximum allowable takeoff weight of 12,499 lbs and the center of gravity was about 8 inches beyond the maximum allowable rear limit.