Remove Knot Remove Rudder Remove Torque
article thumbnail

The Fenestron Factor: Cabri G2 Crash in Gruyéres

Fear of Landing

In the event of an unintentional left yaw, the pilot must immediately apply right rudder, that is, firmly apply pressure on the right rudder pedal. The key is to respond swiftly and with rather more right rudder than might be expected from pilots without experience with Fenestron-equipped helicopters. The weather was clear.

Rudder 111
article thumbnail

The pros and the cons: Cirrus SR22

Air Facts

Even the normally aspirated version (which is less popular than the turbo) climbs to 11,000 feet pretty easily, where it will cruise at over 160 knots on less than 15 gallons per hour. No rudder trim. Like the lack of nose wheel steering, the lack of rudder trim has always bothered me. Its noisy.

Insiders

Sign Up for our Newsletter

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.

Trending Sources

article thumbnail

Everything You Need To Know About Ailerons

Pilot Institute

Adverse yaw is a side effect of aileron use, countered by rudder input. The rotational force thats needed to move an object about an axis is called torque. The simplest formula for torque is: Torque = F x L L is the distance between the object and the axis of rotation, also called the moment arm. What Is an Aileron?

Aileron 90
article thumbnail

Used Aircraft Guide: Piper Aerostar Offers Turbine-Like Performance

Flying Magazine

Claimed 75 percent cruise is a blistering 261 knots, and initial climb rate is 1875 fpm. At economy cruise (55 percent), the fuel burn is 32 gph and claimed speed is 225 knots. Primary flight controls are via push-pull tubes, torque tubes and bell cranks. The airplane gets a gross weight boost to 6,356 pounds ramp weight.

Knot 115
article thumbnail

Nothing Small About It

Plane and Pilot

“We routinely taxi at 1200 rpm due to the low spray…[we] can cruise at 10 knots” in displacement mode, something a Goose can’t do. Another advantage of the counter-rotating props is the elimination of torque roll. This is the tendency to dig in the left tip float during takeoff while countering engine torque.