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Split-S Decision

Plane and Pilot

Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth. Airspeed reached 248 kias, well over the never exceed VNE of 200 kias. The vertical descent rate reached the data-recording limit of 9,999 feet per minute.

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Split-S Decision

Plane and Pilot

Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth. Airspeed reached 248 kias, well over the never exceed VNE of 200 kias. The vertical descent rate reached the data-recording limit of 9,999 feet per minute.

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Basic attitude instrument flying – the foundation for IFR flight

Flight Training Central

Just as an excessive climb or descent will cause you to overshoot altitude, an excessive rate of turn results in overshooting the target heading. For heading corrections of five degrees or less, keep the wings level and use rudder pressure to change the heading. If airspeed is too high or low, the pitch attitude must be changed.

Descent 52
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How to Fly Perfect Lazy Eights

Pilot Institute

It’s just S-turns with climbs and descents, right? We counteract adverse yaw by applying rudder in the direction of the turn. The amount of rudder required depends on roll rate and airspeed. Airspeed and attitude change constantly, and we must change rudder input along with them.

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Invisible Trap Kills Glider Pilot – How To Avoid Microbursts

Chess In the Air

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. Even a more typical descent rate of 200 fpm would have allowed Shmulik to hold for about 5-7 minutes before he would have had to proceed with the landing.

Pilot 52
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What NTSB Reports Say About Impossible Turns and Angle of Attack

Air Facts

To get the extra lift required for the turns, I had to dive to get extra airspeed so that the plane could turn at that same AOA. Optimum” glide was not the issue here, and a visual AOA indicator would have had no value. That produced a strange traffic pattern with roller coasters at the corners.)