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The anatomy of a commercial flight – all you ever wanted to know: Part one  

Aerotime

This is the result of the flight crew performing a full and free movement check to ensure that all flight control surfaces (ailerons, rudder, elevators) are working correctly and the aircraft is fit to fly before taking to the air. After reaching 100 knots, the aircraft will continue to accelerate to what is referred to as its V1 speed.

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35 years ago: How a United Airlines crew landed an ‘unflyable’ DC-10

Aerotime

The primary flight controls on the DC-10 (ailerons, rudder, elevators, spoilers) were all operated by hydraulic pressure and the first officer was quick to realize that his controls were unresponsive to his inputs. Upon his return, he reported that both right-hand and left-hand rear stabilizers had sustained damage.

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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.

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Cessna Skyhawk C172: Features, Performance, and Flight Experience

Airspeed Junkie

With a maximum takeoff weight of 2,400 pounds and a maximum gross weight that ensures stability, this aircraft is robust enough to handle a variety of flying conditions. For instance, Knots 2U offers a Cessna 172 Cowl / Body Fairing Kit that improves aerodynamics and can increase cruise speed by 3-4 mph.

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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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How to Improve Your Landings

Pilot Institute

The easiest way to achieve this is by flying a stabilized approach. So, what is a stabilized approach? A stabilized approach requires the pilot to establish and maintain a constant angle glidepath towards an aiming point. Flying at 60 knots? Most approaches use a 3:1 glidepath. Two key aspects make good approaches.

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