Vintage Aviation News

SEPTEMBER 21, 2024

The restoration team removed, refurbished (or remade) and reinstalled each component from the original vertical stabilizer, one-at-a-time, so everything stayed in alignment, negating the need for a fixture. AirCorps Aviation’s CAD department has produced a rendering of the AT-10’s horizontal stabilizer.

Horizontal Stabilizer 98

Horizontal Stabilizer Stability Rudder Tail 98

Vintage Aviation News

FEBRUARY 20, 2025

The tail section mates perfectly with the forward fuselage. The horizontal and vertical stabilizers have also been completed and attached to the tail section. Before the temporary halt in restoration, the fuselage structural framework had been completed and painted.

Stability 92

Stability Tail Aileron Rudder 92

Flying Magazine

APRIL 30, 2024

An unbuilt concept, the Douglas DC-8 Skybus aimed to position two V-12 piston engines in the forward fuselage and link them with two contra-rotating propellers in the tail. A ventral stabilizer doubled as propeller protection in the event of over-rotation or tail strikes.

Drag 133

Drag Thrust Stability Tail 133

Vintage Aviation News

JULY 3, 2024

The aircraft’s wings and horizontal stabilizer required only minor repairs. The team installed new electrical systems and hoses, rebuilt the main landing gear and tail wheel, and recovered and painted the fuselage, wings, and flight surfaces to restore the aircraft’s original appearance.

Horizontal Stabilizer 124

Horizontal Stabilizer Stability Tail Pilot 124

Plane and Pilot

NOVEMBER 6, 2024

The initial version had a “fastback” fuselage that lacked a rear window and a large, unswept vertical stabilizer. The most modern versions incorporate a rear window and swept tail. This example, built in 1960, combines the fastback of earlier models with the swept tail of later ones.

Tail 98

Tail Airplanes Stability Pilot 98

Vintage Aviation News

JANUARY 9, 2025

On this day in aviation history, January 9, 1943, a large four engine transport aircraft with three tail fins rose from the runway at Burbank Airport, California. The tail was the most distinctive part of the Connie’s design. The prototype Lockheed L-1049 Super Constellation, N67900 over Burbank.

Tail 116

Tail Stability Pilot Hangar 116

Vintage Aviation News

SEPTEMBER 26, 2024

In March 1939, a new owner, Alhambra resident Warren Knox Layne, added a tailwheel to better operate from paved runways as opposed to the original tail skid. It shows that the aircraft had border stripes following the contours of its tail surfaces and wings, with a single stripe down the length of each side of the fuselage.

Tail 111

Tail Horizontal Stabilizer Stability Airplanes 111

Plane and Pilot

OCTOBER 24, 2024

As a 1979 N-model this 172 incorporates the swept vertical stabilizer and rear cabin window, giving it the most modern look of any 172 variants. Custom-painted wheel pants and a sharp paint scheme add to the overall appearance and make it stand out from older, round-tail, fabric-covered taildraggers.

Stability 98

Stability Tail Airplanes General Aviation 98

Vintage Aviation News

NOVEMBER 26, 2024

The initial design incorporated wing panels from the North American P-51 Mustang, the tail assembly of the Douglas A-24, and the landing gear from the Vought F4U Corsair. Engineers struggled to stabilize the aircraft’s center of mass, and the V-3420 engine often failed to deliver its expected power output.

Tail 105

Tail Aileron Approach Stability 105

Learn to Fly

DECEMBER 6, 2024

The F-35 Lighting II Joint Strike Fighter features vertical tail feathers and horizontal stabilators made from carbon fiber-reinforced bismaleimide composite. Composites can make up 50 to 90% of a rotorcrafts airframe by weight, including radomes, tail cones and large structural assemblies (Figure 6).

Stability 73

Stability Tail Horizontal Stabilizer Cargo 73

Fear of Landing

JUNE 28, 2024

The Cabri G2 comprises a shrouded tail rotor, usually referred to as a “Fenestron” (a registered trade mark of Eurocopter) that was proven to provide excellent maneuverability in every flight condition, in every direction of flight up to 40 kt at least. They crashed into a field east of the runway, breaking the skids off.

Rudder 106

Rudder Tail Lift Knot 106

Plane and Pilot

OCTOBER 19, 2024

That is the story of the Bellanca Aries T-250, an efficient, T-tailed travel machine that rivaled the Beechcraft Bonanza and Piper Comanche in speed, load-carrying capacity, and elegant design. Their first design, the Anderson Greenwood AG-14, was a 90 hp, twin-tailed, two-seat pusher.

Tail 98

Tail Airplanes Crosswind Knot 98

Vintage Aviation News

JANUARY 22, 2025

But the most radical feature of the Pigeon-Fraser was Albree’s all-moving tail design. Albree would consider this design to be his “make or break” aircraft to validate his theory for the Flying Tail design he and Roscoe P. serial numbers 116 and 117, with U.S. Timson had designed nearly ten years prior.

Tail 98

Tail Airplanes Stability Aileron 98

Pilot Institute

DECEMBER 26, 2024

The white light is located on the aircrafts tail and sometimes additionally on the wingtips, facing backward (aft). Logo Lights Logo lights are lights mounted on the horizontal stabilizer of an aircraft and point upward toward the vertical stabilizer, illuminating the airlines logo. These lights are not a legal requirement.

Airplanes 111

Airplanes Horizontal Stabilizer Runway Pilot 111

AV Web

FEBRUARY 4, 2025

As of today, the CRJs right wing, center fuselage, part of the left wing and left fuselage, significant portions of the forward cabin and cockpit, vertical stabilizer, tail cone, rudder, elevators, TCAS computer, and quick access recorder have been recovered and will be moved to a secure location for examination.

Air Traffic Control 66

Air Traffic Control Quick Access Recorder Cockpit Rudder 66

Fear of Landing

APRIL 19, 2024

At approximately 30-40 feet agl, the spinning stopped and the helicopter appeared to stabilize for a brief moment before continuing a nose-low, forward descent into the grass north of Runway 28. The operator confirmed that the tail rotor had been installed the day before the accident. As it descended it spun around 2-3 times.

Torque 87

Torque Indicated Airspeed Tail Knot 87

Plane and Pilot

SEPTEMBER 20, 2024

Missing its tail, pointing almost straight down, a Van’s RV-7A single-engine, two-seat homebuilt plummeted out of the blue and into the rocky ground. Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth.

True Airspeed 93

True Airspeed Indicated Airspeed Horizontal Stabilizer Aileron 93

Plane and Pilot

SEPTEMBER 20, 2024

Missing its tail, pointing almost straight down, a Van’s RV-7A single-engine, two-seat homebuilt plummeted out of the blue and into the rocky ground. Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth.

True Airspeed 93

True Airspeed Indicated Airspeed Horizontal Stabilizer Aileron 93

Plane and Pilot

JANUARY 20, 2025

Unlike the Cessnas all-aluminum airframe construction, the Stinson uses a steel tube fuselage with fabric covering the fuselage, wing, and tail. This particular 108 is the dash three model, identifiable by the large vertical stabilizer. It has a low 2,221 hours on the airframe with no known damage history.

Transponder 97

Transponder Stability Tail Airplanes 97

Aerotime

NOVEMBER 1, 2024

Renatas Repcinskas / Shutterstock Even if delivery schedules can be stabilized to meet airlines’ expectations in the future, it remains likely that they will still not have enough aircraft to sustain their desired growth. Only a couple of years ago, the scramble to get into the P2F market was rising unabated.

Cargo 278

Cargo Jet Airline Airlines 278

Pilot Institute

NOVEMBER 11, 2024

How an aircraft handles Dutch roll depends on its dynamic stability. The aircraft’s design influences its dynamic stability. To understand the aircraft’s response to a disturbance, you need to understand aerodynamic stability. There are two main types of stability: Static and Dynamic stability.

Stability 52

Stability Center of Gravity Aileron Lift 52

Flight Training Central

JANUARY 27, 2025

As the airplane contacts the ground, the tail will be forced down very rapidly by the back-elevator pressure and by inertia acting downward on the tail. Be patient and practice disciplined traffic pattern and stabilized approach procedures. When a porpoise is severe, the safest procedure is to EXECUTE A GO-AROUND IMMEDIATELY.

Airplanes 89

Airplanes Runway Accelerated Stall Lift 89

Vintage Aviation News

JANUARY 30, 2025

A short 18 months later, on August 13, 1937, the XPB2Y-1 took to the skies for the first time, revealing plenty of room for improvement lateral instability was a major problem for the deep-hulled boat, so the single tail fin was augmented by two smaller fins on the horizontal stabilizers. ” “I guess we surprised them!”

Horizontal Stabilizer 111

Horizontal Stabilizer Final Approach Tail Runway 111

Pilot's Life Blog

MARCH 15, 2024

All of these primary control surfaces serve as a horizontal stabilizer for the plane. Vital Components of a Plane in the Tail Assembly The primary function of the empennage or tail assembly of an airplane is to keep the aircraft stable despite the rotational energy of relative wind. What are the basic parts of this section?

Horizontal Stabilizer 52

Horizontal Stabilizer Aileron Air Traffic Control Lift 52

Plane and Pilot

DECEMBER 8, 2024

This version was equipped with modified flight controls based on lessons learned from the initial prototype, had a larger vertical stabilizer, and several other minor improvements. The large vertical tail completes the picture. Undeterred, Harlow and his merry band of students constructed a second prototype, the PJC-2.

Airplanes 98

Airplanes Ceiling Stability Tail 98

Pilot's Life Blog

FEBRUARY 11, 2025

Managing these elements requires continuous adjustments by the pilot to maintain stability and control. The elevator, situated on the horizontal tail surface, adjusts pitch, raising or lowering the nose for ascent or descent. The rudder, attached to the vertical tail fin, manages yaw, enabling the nose to move left or right.

Torque 52

Torque Lift Airplanes Stability 52

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

Vintage Aviation News

FEBRUARY 15, 2025

(Nigel Hitchman) The story of the Breguet Deux-Ponts begins even before WWII, when Breguet Aviation began design work on the concept for a large four engine transport with two decks for passengers called the Breguet 760, which was based on the wings and tail assembly of the Breguet 730 flying boat.

Tail 59

Tail Cargo Stability Payload 59

Professional Pilot

AUGUST 8, 2024

The Flight Safety Foundation’s approach and landing accident reduction tool kit goes on to point out that an approach is stable only if all the criteria in company standard operating procedures (SOPs) are met before or when reaching the applicable minimum stabilization in height.

Approach 105

Approach Descent Visual Meteorological Conditions (VMC) Runway 105

Vintage Aviation News

JUNE 28, 2024

Detail design began in 1941 but was delayed by including an “unsatisfactory” tailhook design and poor directional stability with only one engine operational, but the biggest delays came from the Navy asking Grumman to give priority to the development and production of the Hellcat. Navy Midway -class carriers.

Payload 116

Payload Stability Tail Pilot 116

Vintage Aviation News

FEBRUARY 12, 2025

The airship initially recovered, dumping ballast and stabilizing at 700 feet above the sea and returning to its cruising altitude of 1,600 feet, but the ship was sent into another plunge, falling a rate of 14 feet per second tail-down.

Lift 59

Lift Tail Stability Wind Shear 59

Pilot Institute

NOVEMBER 23, 2024

A flat spin happens when the center of gravity shifts too far aft (toward the tail), and the aircraft’s rotation becomes more horizontal. The problem is that the airflow from the propeller goes over the horizontal stabilizer, which produces a downward force (and causes the nose to pitch up).

Center of Gravity 98

Center of Gravity Weight-Shift-Control Aileron Rudder 98

Flight Training Central

MAY 6, 2024

Then in 1956 Cessna moved the tail-wheel on the 170 to the nose and the resulting high wing 172, with well over 40,000 copies, became the best-selling civilian aircraft in history. By incorporating more dihedral, the longitudinal stability can be increased to match that exhibited by the high wingers. Why the success of high wings?

Lift 97

Lift Drag Airplanes Ground Effect 97

Vintage Aviation News

NOVEMBER 13, 2024

With expander-tube brakes, it is difficult to brake sufficiently to pick up the tail. image via AirCorps Aviation) The transverse tube (highlighted by the red box) is where the horizontal stabilizer’s rear main spar tube passes through the fuselage.

Firewall 105

Firewall Gross Weight Horizontal Stabilizer Stability 105

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

Vintage Aviation News

JANUARY 14, 2025

However, since Convair was also developing the XF-92 delta wing prototype for a future Air Force interceptor, the design team at Convair, led by Ernest Stout, proposed a new delta wing aircraft with retractable hydro-skis for takeoffs and landings, a watertight hull, and a single delta tail.

Cockpit 98

Cockpit Flight Deck Drag Stability 98

Vintage Aviation News

OCTOBER 11, 2024

However, this wasn’t the only unique thing about Cierva Twin; it was outstanding in its class for the following reasons – Coaxial Rotor System – This design eliminated the need for a tail rotor, reducing mechanical complexity and increasing lift efficiency. This allowed for more stability and control, especially in hover.

Tail 52

Tail Drag Ceiling Cargo 52