Remove Indicated Airspeed Remove Knot Remove Rudder
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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. But a review of the avionics data shows it was entered at the correct airspeed (placarded as between 104 and 165 knots), and the roll rate was constant.

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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. But a review of the avionics data shows it was entered at the correct airspeed (placarded as between 104 and 165 knots), and the roll rate was constant.

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Navy primary flight training—the instructor had it coming

Air Facts

It was a beefed up, militarized version of the Beechcraft Bonanza with a narrowed fuselage and conventional tail, seating two pilots in tandem cockpits with controls and indicators configured similarly to tactical aircraft of the period. The Navy’s primary trainer was the T-34B.

Cockpit 98
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How to Fly Perfect Lazy Eights

Pilot Institute

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. We apply right rudder to counteract the left-turning tendencies.

Rudder 52
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Invisible Trap Kills Glider Pilot – How To Avoid Microbursts

Chess In the Air

This is consistent with Rick’s report, which referenced 9 knots of wind. Without knowing the horizontal wind direction and speed at this point it is impossible to say what his indicated airspeed was. A sudden gust of 50 knots would have caused a stall unless he had been flying at about 100 knots indicated.

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. Tedious numerical interpolation is not required when adjusting airspeed for weight, contrary to the claims of some AOA advocates. That produced a strange traffic pattern with roller coasters at the corners.)