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Delta Connection flight received sink rate alert before Toronto Pearson crash

Aerotime

Around 13 seconds before touchdown as the aircraft was descending through 153 feet above ground level (AGL) the TSB said the CRJ900s indicated airspeed increased to 154 knots whereas the ground speed did not change appreciably, consistent with a performance-increasing wind gust. The bank angle increased to a 4.7right bank.

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Delta CRJ-900 Accident In Toronto: Preliminary Report Published

One Mile at a Time

degrees Less than one second before touchdown, the plane had an indicated airspeed of 134 knots, a ground speed of 111 knots, a bank angle of 7.1 A large portion of the tail section was found on the runway, around 1,680 feet from the threshold, and 235 feet from the main wreckage.

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Unbolted in Fairfield (Update on the 2022 Bell 407 GXP Crash)

Fear of Landing

As the helicopter continued towards the airport, the airspeed began to decrease. The indicated airspeed 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 indicated airspeed of zero knots when the right yaw ceased.

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Split-S Decision

Plane and Pilot

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. Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth.

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Split-S Decision

Plane and Pilot

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. Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth.

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We Fly: Cirrus SR G7

Flying Magazine

Holding down the autopilot disconnect button allows you to maneuver past the ESP (electronic stability protection), and in this case, pitch up to a deck angle needed to induce preliminary stall buffeting. It also prevents you from retracting the flaps when airspeed is too low.

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