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While the report draws no conclusions as to the cause of the crash, investigators set out a detailed timeline which focuses heavily on the Mitsubishi CRJ900s descent. TSB At a height of 50 feet the rate of descent had increased to 1114 feet per minute (fpm) from 672 fpm around 14 seconds before. to the right, the TSB said.
degrees Less than one second before touchdown, the plane had an indicatedairspeed of 134 knots, a ground speed of 111 knots, a bank angle of 7.1 degrees to the right, and a rate of descent of 1,110 feet per minute The plane touched down at a bank angle of 7.5 These details should be revealed in subsequent reports.
As the helicopter continued towards the airport, the airspeed began to decrease. The indicatedairspeed had fallen below 65 knots and was still decreasing. As the airspeed decayed, the right yaw increased. The helicopter was at treetop height with an indicatedairspeed of zero knots when the right yaw ceased.
Missing its tail, pointing almost straight down, a Van’s RV-7A single-engine, two-seat homebuilt plummeted out of the blue and into the rocky ground. This wasn’t the first Van’s homebuilt to experience an in-flight tail separation. Airspeed reached 248 kias, well over the never exceed VNE of 200 kias. The pilot died instantly.
Missing its tail, pointing almost straight down, a Van’s RV-7A single-engine, two-seat homebuilt plummeted out of the blue and into the rocky ground. This wasn’t the first Van’s homebuilt to experience an in-flight tail separation. Airspeed reached 248 kias, well over the never exceed VNE of 200 kias. The pilot died instantly.
Flying in clouds of cold and warm fronts can lead to very small supercooled water droplets which build up as rime ice on the parts of the aircraft exposed to the wind: probes, antennas, and the leading edges of the wings and tail. The ATR’s airspeed was 191 knots. The ATR’s airspeed was 184 knots.
The Rifle ASOS recorded a gust of 43 mph from the south: a 100-degree shift in direction, putting it right on his tail. Under normal circumstances Shmulik would have had sufficient altitude to delay the landing by several minutes: his glider’s minimum descent rate in still air was just 100 fpm.
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