Flying Magazine

APRIL 26, 2024

The small aileron “tabs” were not doing a great job in crosswind ability. Hand flying the circuit, I blasted through the shear with ease, but the big wings made it even more noticeable in rolling motions and aileron slop. Older jets without winglets or shorter wingspans are much faster in roll and lack some stability in bank.

Crosswind 105

Crosswind Weather Knot Aileron 105

Northstar VFR

JULY 21, 2024

The rudder is a movable flight control which is mounted on the trailing edge of the vertical stabilizer on the back of the airplane. Some new student pilots think the rudder and vertical stabilizer are the same thing. The vertical stabilizer is a vertical fixed part of the plane’s empennage. Why is the rudder so important?

Rudder 52

Rudder Airplanes Pilot Stability 52

Plane and Pilot

SEPTEMBER 20, 2024

Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth. I did my first aileron roll in an RV-4. The pilot died instantly.

True Airspeed 68

True Airspeed Indicated Airspeed Horizontal Stabilizer Aileron 68

Plane and Pilot

SEPTEMBER 20, 2024

Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth. I did my first aileron roll in an RV-4. The pilot died instantly.

True Airspeed 65

True Airspeed Indicated Airspeed Horizontal Stabilizer Aileron 65

Flying Magazine

MAY 15, 2024

Piper’s Cherokee Six appeals to pilots for some of the same reasons that other Cherokee models are popular, including stability, predictable handling, and reliability. Additional equipment includes electric pitch trim, rudder trim, Flightcom six-place intercom, cabin ventilation fan, auxiliary power receptacle, and aileron gap seals.

Transponder 52

Transponder Aileron Rudder Stability 52

Vintage Aviation News

DECEMBER 15, 2024

Head on view of the Northrop X-4 Bantam (NASA) The X-4 was a research aircraft developed by the Northrop Corporation to test the stability of semi-tailless wing designs at transonic speeds in excess of Mach 0.9. For better maintenance access, the small tail of the aircraft could be removed to work on or remove the engines.

Stability 52

Stability Horizontal Stabilizer Aileron Rudder 52

Flight Training Central

DECEMBER 4, 2023

Adjust pitch and power for the desired airspeed and approach angle.The approach should be stabilized on the extended runway centerline no lower than 300’ AGL. At this time, it should be gently lowered.Maintain directional control and crosswind correction with appropriate rudder aileron input.

Approach 52

Approach Ground Effect Final Approach Airplanes 52

Pilot Institute

OCTOBER 12, 2024

The turbulent air hits the horizontal stabilizer, which causes a vibration that can be felt throughout the aircraft. The lack of airflow over the ailerons results in a loss of control authority and mushy and ineffective controls. As the aircraft stabilizes at level attitude, reduce flaps to 10 degrees.

Stability 52

Stability Horizontal Stabilizer Airplanes Lift 52

Vintage Aviation News

OCTOBER 19, 2024

The modifications included replacing the single fin and rudder with a twin-tail design to improve stability. A particularly harrowing incident occurred during a test flight in March 1934 when the ailerons tore off one of the prototypes mid-flight. Despite these efforts, the problems persisted.

Weight-Shift-Control 52

Weight-Shift-Control Aviation Technology Aileron Rudder 52

Pilot Institute

MARCH 29, 2024

Trim for level flight once you’re stabilized at your target speed. To fight this overbanking tendency, add light aileron pressure in the opposite direction. Not Maintaining Heading Once you’ve practiced slow flight a few times, you’ll realize just how ineffective the ailerons are. Stay coordinated throughout the turn.

Lift 52

Lift Rudder Drag AGL 52

Pilot Institute

JULY 12, 2024

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. Keep the ailerons into the wind. Most approaches use a 3:1 glidepath.

Descent 52

Descent Weight-Shift-Control Crosswind Runway 52

Plane and Pilot

NOVEMBER 10, 2024

Sure, there are the removable wings and an unusual-for-an-RV stabilator out back for pitch control, but there’s nothing revolutionary in the concepts or execution. On the walkaround, you doubtlessly noted the full-span flaperons (flaps plus ailerons as one unit). The RV-12 is, of course, all metal.

Airplanes 84

Airplanes Knot Pitot Tube Gross Weight 84

Plane and Pilot

OCTOBER 2, 2024

By doing so, a recognizable, firm input demonstrates that using all the aileron travel wasn’t the answer—those rudder pedals are not footrests. Constant manipulation of attitude and power while chasing errant airspeed are signs that a CFI needs to step in to stabilize things.

Runway 52

Runway Wind Shear Crosswind Ceiling 52

Plane and Pilot

OCTOBER 2, 2024

By doing so, a recognizable, firm input demonstrates that using all the aileron travel wasn’t the answer—those rudder pedals are not footrests. Constant manipulation of attitude and power while chasing errant airspeed are signs that a CFI needs to step in to stabilize things.

Runway 52

Runway Wind Shear Crosswind Ceiling 52

Plane and Pilot

NOVEMBER 10, 2024

Sure, there are the removable wings and an unusual-for-an-RV stabilator out back for pitch control, but there’s nothing revolutionary in the concepts or execution. On the walkaround, you doubtlessly noted the full-span flaperons (flaps plus ailerons as one unit). The RV-12 is, of course, all metal.

Airplanes 76

Airplanes Knot Pitot Tube Gross Weight 76

Pilot Institute

MAY 4, 2024

This gives you a safe buffer on the stall speed and plenty of time to stabilize. Use the rudder to keep the aircraft in line with the runway and apply aileron into the wind. You will need more aileron input as you slow down as the controls become less effective. With a short field landing, we aim to be at 1.3

Weight-Shift-Control 52

Weight-Shift-Control Runway Approach Crosswind 52

Pilot Institute

OCTOBER 16, 2024

Brief that you will use the right rudder to align the aircraft straight with the runway and the left aileron to counteract drift. This allows you to configure appropriately and ensures a stabilized approach. Explain what aircraft input you will require to land the aircraft in the crosswind. Landing on the windward wheel.

Airplanes 52

Airplanes Descent Approach Runway 52

Pilot Institute

NOVEMBER 1, 2024

It most commonly forms on the leading edges of your aircraft, including the wings, tail, and horizontal stabilizer, as well as on the propeller blades and pitot tubes. It can also cause control surfaces like ailerons and flaps to function improperly, making the aircraft harder to maneuver.

Pitot Tube 52

Pitot Tube Drag Lift Airfoil 52

Vintage Aviation News

NOVEMBER 22, 2024

137, showcasing the ventrally mounted vertical stabilizer. Unlike traditional aircraft, the Puffin’s vertical stabilizer and rudder were mounted below the fuselage rather than atop it, providing an unconventional, inverted look. Both the upper and lower wings included ailerons, maximizing maneuverability.

Stability 98

Stability Tail Aileron Rudder 98

Vintage Aviation News

NOVEMBER 19, 2024

Both the vertical and horizontal stabilizers were made of wood and fabric, while the construction of the wing involved wooden spars and ribs, with metal leading edges inboard of the engine nacelles, plywood leading edges on the outer panels, and doped fabric on the trailing section.

Aileron 122

Aileron Tail Horizontal Stabilizer Cockpit 122

Plane and Pilot

SEPTEMBER 8, 2024

This early design, also called the “Standard Seven,” featured a vestigial vertical stabilizer, ground adjustable propeller, and tight cowling that featured fairings for each rocker arm. It sported a supercharged 450 hp Pratt & Whitney Wasp Junior and an enlarged vertical stabilizer and rudder to match.

Rudder 61

Rudder Stability Airplanes Aileron 61

Airspeed Junkie

SEPTEMBER 20, 2024

These engines are arranged in four pods beneath the wings, a design that not only provides the necessary thrust but also helps delay stall onset, contributing to the aircraft’s stability and performance. The aircraft uses a system of six spoilerons on each wing for roll control, compensating for the lack of traditional ailerons.

Payload 98

Payload Weight-Shift-Control Thrust Aileron 98

Plane and Pilot

OCTOBER 3, 2024

The wing’s dead-smooth surface plus the tight-fitting aileron and flap brackets plus aileron gap seals give the build a professional factory look (left). From the pilot’s seat it cruises near effortlessly and handles nimbly on land or water with a great combination of stability and modest control pressures.

Airplanes 59

Airplanes Rudder Knot Aileron 59

Plane and Pilot

DECEMBER 16, 2024

Planespotters note the F2’s separate ailerons and flaps, conventional tail. But you can see the change to separate ailerons and flaps is just one part of preparing the F2 to grow into a four-place airplanebuying aerodynamic benefits now to spend later on a heavier, more powerful model. Out back, theres an entirely new tail.

Rudder 83

Rudder Airplanes Aileron Crosswind 83

Vintage Aviation News

OCTOBER 6, 2024

These wings help maintain stability even at a high angle of attack, especially allowing for better yaw control. Additionally, automatic slats are mounted on the wings’ leading edges with manoeuvring flaps and wingtip ailerons on the trailing edge.

Aileron 52

Aileron Jet Stability Thrust 52

Plane and Pilot

NOVEMBER 13, 2024

The ailerons feature a small flow-control trailing-edge flap to enhance roll control. The broad stabilator carries an electrically adjustable balance tab. Clearing the final approach path, we extended full flaps and stabilized at 70 knots. Electric flaps ride out on external tracks to a maximum of 30 degrees.

Knot 72

Knot Rudder Airplanes Gross Weight 72

Vintage Aviation News

OCTOBER 13, 2024

The aircraft performed well at a high speed with stable cruise and descent however, during the second flight, some issues surfaced with the longitudinal stability during the climb. Ernst Heinkel (right) with Siegfried Günter. These tanks held up to 910 liters (240 US gallons) of fuel each.

Cockpit 52

Cockpit Aileron Ceiling Descent 52