Charter/Taxi (Non Scheduled Revenue Flight)

On February 2, 2005, about 0718 eastern standard time, a Bombardier Challenger CL-600-1A11, N370V, ran off the departure end of runway 6 at Teterboro Airport (TEB), Teterboro, New Jersey, at a ground speed of about 110 knots; through an airport perimeter fence; across a six-lane highway (where it struck a vehicle); and into a parking lot before impacting a building. The two pilots were seriously injured, as were two occupants in the vehicle. The cabin aide, eight passengers, and one person in the building received minor injuries. The airplane was destroyed by impact forces and postimpact fire. The accident flight was an on-demand passenger charter flight from TEB to Chicago Midway Airport, Chicago, Illinois. The flight was subject to the provisions of 14 Code of Federal Regulations (CFR) Part 135 and operated by Platinum Jet Management, LLC (PJM), Fort Lauderdale, Florida, under the auspices of a charter management agreement with Darby Aviation (Darby), Muscle Shoals, Alabama. Visual meteorological conditions prevailed for the flight, which operated on an instrument flight rules flight plan.

The twin engine aircraft stalled on approach to Courchevel Airport and touched down hard, causing substantial damage to the fuselage. There were no injuries but the aircraft was damaged beyond repair.

Following an uneventful flight from Vanavara, the crew started the descent by night to Tura Airport. Weather conditions were marginal with a visibility of 3,500 metres and light snow. After being cleared to land, the crew continued the approach. At a speed of 160 km/h, the crew initiated a right turn. In a 10° nose down and a right bank of 40°, the aircraft impacted trees and crashed in a snow covered forest located 9,6 km southeast of the airport. The wreckage was found a day later near the Bazhenov River and all nine occupants were killed, among them the regional director of the Department of Transport and the vice-governor of the Evenkiya region.

While attempting to depart from the 3,500-foot long grass airstrip with a 14 knot quartering tailwind, the 5,800-hour pilot reported that at an airspeed of approximately 95 knots, "the airplane yawed left and rolled left abruptly as the aircraft came off the ground briefly." The airplane settled back onto the ground, before again climbing back into the air approximately 20 degrees left of the runway heading. Subsequently, the airplane’s landing gear struck tree tops before it impacted the ground. A passenger added that he "noticed the flaps were up during takeoff." Approximately three minutes after the accident, a weather reporting station located 5.6 nautical miles southwest of the accident site reported wind from 010 degrees at 14 knots. Examination of the engines revealed rotational scoring throughout the first and second stage turbines. No mechanical anomalies were observed.

Weather reporting facilities reported icing conditions in the area of the accident site. The pilot of a Cessna Citation flying the same RNAV approach twenty minutes prior to the accident aircraft reported picking up light to occasional moderate rime ice. The last communication between the local air traffic controller and the accident pilot indicated that the flight was two miles south of the final approach fix. The controller inquired if the pilot had the runway in sight, and the pilot reported "negative, still IMC." A witness on the ground near the accident site reported that he heard the aircraft first then saw it at a low level below the cloud base flying in a southeasterly direction. The witness stated that the right wing was lower than the left as the aircraft continued to descend. The witness then noted that the wings were moving "side to side" (up and down) a couple of times before the nose of the aircraft dropped near vertical to the terrain. This witness reported hearing the sound of the engine running steady throughout the event. The wreckage was located in a flat open field about 3,000 feet south of the final approach fix coordinates. The aircraft was destroyed by impact damage and a post crash fire.

The flight was cleared for the ILS Runway 19 approach, circle-to-land on Runway 24; a 6,013-foot-long, 150-foot wide, asphalt runway. The auto throttle and autopilot were disengaged during the approach, about 800 feet agl. However, the auto throttle reengaged just prior to touchdown, about 35 feet agl. The flightcrew did not recall reengaging the auto throttle, and were not aware of the autothrottle reengagement. According to the auto throttle computers, the reengagement was commanded through one of the Engage/Disengage paddle switches located on each power lever. The target airspeed set for the auto throttle system was 138 knots. After touchdown, as the airplane decelerated below 138 knots, the auto throttle system gradually increased the power levers in an attempt to maintain the target airspeed. Without the power levers in the idle position, the ground spoilers and thrust reversers would not deploy. While the flightcrew was pulling up on the thrust reverser levers, they may not have initially provided enough aft force on the power levers (15 to 32 lbs.) to override and disconnect the auto throttle system. The flight data recorder indicated that the autothrottle system disengaged 16 seconds after the weight-on-wheels switches were activated in ground mode. As the airplane neared the end of the runway, the pilot engaged the emergency brake, and the airplane departed the right side of the runway. The autothrottle Engage/Disengage paddle switches were not equipped with switch guards. Although the autothrottle system provided an audible tone when disengaged, it did not provide a tone when engaged. The reported wind about the time of the accident was from 290 degrees at 16 knots, gusting to 25 knots, with a peak wind from 300 degrees at 32 knots.

On November 28, 2004, about 0958 mountain standard time, a Canadair, Ltd., CL-600-2A12, N873G, registered to Hop-a-Jet, Inc., and operated by Air Castle Corporation dba Global Aviation as Glo-Air flight 73, collided with the ground during takeoff at Montrose Regional Airport (MTJ), Montrose, Colorado. The on-demand charter flight was operated under the provisions of 14 Code of Federal Regulations (CFR) Part 135 on an instrument flight rules (IFR) flight plan. Instrument meteorological conditions prevailed, and snow was falling. Of the six occupants on board, the captain, the flight attendant, and one passenger were killed, and the first officer and two passengers were seriously injured. The airplane was destroyed by impact forces and post crash fire. The flight was en route to South Bend Regional Airport (SBN), South Bend, Indiana.

On approach to Urimán, the single engine aircraft crashed in a wooded area located few km from the destination airport. Both occupants were rescued a day later. The passenger was injured and the pilot was unhurt.

During the takeoff roll, the left engine failed. Control was lost and the aircraft veered off runway and came to rest. All four occupants escaped uninjured while the aircraft was damaged beyond repair.

The commercial certificated pilot, with six passengers, was departing from a remote beach in a twin-engine airplane on an on-demand air taxi flight. The beach was oriented north/south, and was utilized by airplanes transporting guests to and from a remote wilderness lodge. Weather conditions at the beach were reported to air taxi operators via satellite phone. The pilot reported that as he was departing toward the north, the wind was from the west about 30 knots, with gusts to 50 knots. About 20 feet agl, a strong gust of wind, or a downdraft, hit the airplane. The airplane descended and the left wing collided with the beach, which spun the airplane 180 degrees. The airplane came to rest in about 2 1/2 feet of water.