AV Web

JANUARY 1, 2025

Cruise speeds for most powerful piston versions of the aircraft are in the 160-knot category, with range figures of around 1,100 nautical miles. First, the structural design of the aircraft offers an optimized center of gravity that results in better flight stability and handling.

Center of Gravity 105

Center of Gravity Payload Knot Stability 105

Vintage Aviation News

FEBRUARY 19, 2025

(Wright State University) The original configuration of the Bell Model 68 was an open cockpit all-metal monoplane with fixed landing gear that was powered by two Armstrong Siddeley Viper turbojet engines with thrust deflectors located at the aircraft’s center of gravity.

Thrust 94

Thrust Center of Gravity Descent Cockpit 94

Pilot Institute

MARCH 26, 2024

This tendency is due to their high center of gravity and heavy engine over the nose wheel. As with any landing, it’s vital to have a stabilized approach. If you’re not stabilized at 200 feet AGL, go around. If the nose wheel digs in at high speeds, it can result in a loss of control.

NOTAMs 52

NOTAMs Runway Approach Descent 52

Pilot Institute

FEBRUARY 20, 2025

What Is Aircraft Stability? Stability is the aircrafts tendency to maintain its attitude or orientation. This means that they have to be effective enough to counter the aircrafts inherent lateral stability. Lateral stability depends on the aircrafts design. This shifts the ailerons Center of Gravity (C.G.)

Aileron 90

Aileron Weight-Shift-Control Rudder Longitudinal Axis 90

Plane and Pilot

OCTOBER 3, 2024

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. Early on a speed restriction of 130 knots was applied as a flutter issue. This was resolved on the kit version and led to cruising at 50% power and 120 knots, which proved to be the Gweduck’s sweet spot.

Airplanes 77

Airplanes Rudder Knot Aileron 77

AV Web

APRIL 15, 2025

After takeoff, the airplane impacted the ground about 600 yards from the end of the runway… Although estimated takeoff weight was below maximum, the airplane was loaded with an aft CG (hint), which would have reduced the longitudinal stability during the climb out. Other than that, what?

Pilot 52

Pilot Airplanes Runway Descent 52