Friday, 13 December 2019

Skycraft SD-1 Minisport Specs, Cockpit, and Price

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Skycraft SD-1 Minisport Specs, Cockpit, and Price – SD-1 Minisport is a one-seat ultralight aircraft manufactured by Skycraft Airplanes, US. This aircraft was designed by Igor Špaček from the Czech Republic, then assembled and manufactured by Skycraft in accordance with ASTM regulations for light sport aircraft at its factories located in Orem and Provo in Utah. The SD-1 Minisport aircraft conducted its first flight test in May 2014. It is available in rear wheel drive and tri-gear configurations.

Skycraft SD-1 Minisport aircraft

Skycraft SD-1 Minisport Specs

The airframe from SD-1 Minisport is made with wood, carbon fiber and composite materials. Wooden frame bodies integrate removable wings. Wing and tail ribs are made of extruded polystyrene. The overall dimensions of the aircraft include a length of 14.27 ft, height of 5 ft, wingspan of 19.62 ft, wing area of ​​65.66 ft², horizontal tail span 6.43 ft, and horizontal tail area of ​​10.23 ft². The base diameter of the wheels and main gears are 3.54 ft and 11.81 inches respectively. The aircraft has 285 lb of empty weight and a useful payload of 295lb. This can take a maximum pilot weight of 230 lb.

The SD-1 Minisport aircraft has a single-seat cabin with a height of 40.5 in, width 20.5 in, and legroom 43 in. It combines genuine leather interiors and can carry a maximum rear luggage load of 23 lb. The aircraft is equipped with an optional Galaxy GRS 6/375 ballistic parachute which has a minimum deployment height of 210 ft, a weight of 24.9 lb, and a drop rate of 21 fps. Parachute has a repackage time of six years.

Skycraft SD-1 Minisport interior

Skycraft SD-1 Minisport Engine and Performance

The SD-1 Minisport aircraft is powered by the Hirth F-23 engine which can produce a power output of 50 hp at 6,150 rpm. This German-made engine has a two-step configuration with a combustion capacity of 521 cc, and includes dual ignition and fuel injection. This machine drives a tri-bladed hostage propeller. The engine has a 1,000 hour repair time (TBO). This aircraft has a fuel capacity of 34l (9 gal) and uses 91 Octane automotive fuel or 100 LL with TCP additive fuel with Bluemax premem oil with 90: 1 comparison.

The SD-1 Minisport aircraft can fly at a cruising speed of 160 km / h and a maximum speed of 190 km / h. Maneuvering speed and minimum aircraft speed are 156 km / h and 80.5 km / h, respectively. The aircraft has a maximum range of 660 km, a service ceiling of 14,000 ft, and a climbing rate of 900 fpm. The distance required for take-off aircraft is 800 ft and has a durability of 4.1 hours.

Skycraft SD-1 Minisport cockpit

Skycraft SD-1 Minisport Cockpit and Avionics

The SD-1 Minisport cockpit is equipped with the Dynon SkyView instrument panel integrated with the Dynon avionics. The avionics suite includes air speed indicator, altimeter, compass, vario, and slip indicator. It also includes a collision avoidance system and Dynon COM Radio. It comes with two-channel monitoring and GPS-based frequency. It also includes a fuel and power management system, which will provide audio and visual warnings when fuel and power are low.

The cockpit is also equipped with a tachometer, heat meter, and a power management system with audio warning. This aircraft has a navigation feature and landing lights, while the instrument lights up to fly at night. The aircraft also has a personal tracking beacon which can be used to quickly notify search and rescue in the event of an emergency. The auxiliary port in the cockpit allows residents to listen to the iPod without interrupting radio communication.

Skycraft SD-1 Minisport Price

The price of the latest Skycraft SD-1 Minisport aircraft is around US $ 54,850. The operational costs required to fly this aircraft are under $ 15 per hour.

Wednesday, 11 December 2019

Privateer Amphibian Specs, Interior, Cockpit, and Price

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Privateer Amphibian Specs, Interior, Cockpit, and Price – Privateer Amphibian is a seaplane being developed by Privateer Industries for water and ground-based operations. This aircraft was designed by John Meekins and Bill Husa and the prototype aircraft were assembled and integrated by Comp Air Aviation in Titusville, Florida. The aircraft was launched from the hangar in September 2015 and made its first flight on 6 August 2018.

Privateer Amphibian Aircraft

Privateer Amphibian Specs

Privateer Amphibian aircraft are designed to minimize operational impacts around densely populated wildlife areas. The fuselage is built with carbon fiber composite material to make it lightweight, strong and resistant to corrosion. The aircraft has a wet wing design and has a low wing configuration to reduce drag. It also includes a counterweight in the airfoil for elevators and ailerons to neutralize flutter and has two sponsors and twin tails.

The aircraft has a closed propeller design mounted on the rear which increases efficiency and thrust for takeoff and sailing. The shroud blades will also make the turbine quiet by dampening the acoustic profile. In addition, the aircraft is equipped with a retractable three-wheel landing gear, which allows conventional landing and taxi on the runway. Overall, the aircraft's exterior dimensions include a length of 43 ft from nose to tail, height of 12.3 ft on wheels, and wingspan of 42.9 ft.

Privateer Amphibian Specs

Privateer Amphibian Engine and Performance

The Privateer Amphibian aircraft is powered by a Walter M601 series turbine engine which can produce thrust of 724 hp. The engine moves a constant speed 5-bladed propeller. The aircraft can fly with a maximum cruising speed of 360 km / h at sea level, a service ceiling of around 25,000 ft and a climbing rate of 2,100 fpm at sea level. It has a targeted fuel range of 870 nmi (1,000 miles).

The aircraft has an empty weight of 3,600 lb, gross weight of 5,600 lb and a useful load of 2,000 lb. It has a wing loading capacity of 19.8 psf. The maximum takeoff distance at maximum weight is 1,200 ft above water and 960 ft on land.

Privateer Amphibian Cockpit

Privateer Amphibian Cockpit and Avionics

The cockpit of the Privateer Amphibian aircraft can accommodate 1 person in a single pilot operation. The cockpit is equipped with an instrument and radio panel supplied by Garmin. It has controls with an electro-mechanical design and triple redundant.

Privateer Amphibian Cabin and Interior

The spacious Privateer Amphibian cabin can accommodate one pilot and six passengers. The cabin has internal dimensions that cover a length of 13.2 ft and shoulder-width in a sitting position of 4.1 ft. The cabin can also be equipped with a three-seat bench at the rear.

Privateer Amphibian Price

The price of the latest Privateer Amphibian aircraft is around US $ 1.5 million.

Monday, 9 December 2019

Kolb Flyer Super Sport Specs, Cockpit, and Price

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Kolb Flyer Super Sport Specs, Cockpit, and Price – Kolb Flyer SS (Super Sport) is a light sport aircraft produced jointly by New Kolb Aircraft, US and Flyer Industria Aeronautica, Brazil. This aircraft was originally developed as an Ultravia Pelican designed by Jean Rene Lepage. Pelican was produced by Ultravia Aero International until the company closed in 2006. New Kolb Aircraft obtained a design and began production in 2008.

The first flight of the Kolb Flyer SS aircraft was carried out in April 2008 and launched on the market in July 2008 at Airventure 2008, Oshkosh, USA. Around 75 aircraft have been operating since July 2008. SS-S-LSA flyers (Light Sports Special Aircraft).

Kolb Flyer SS Light Sport Aircraft

Kolb Flyer Super Sport Specs

The Kolb Flyer SS design has been modified to fit the US light sports aircraft market. Initially the fuselage was made of fiber-glass material, then replaced with carbon-fiber material. This was done to reduce the weight of the aircraft while increasing its strength. Changes were also made to the size of the door, so that passengers can get in and out of the plane more easily from the plane made possible by pushing the buffer position backwards.

The Kolb Flyer SS aircraft has wet wings and artificial metal tail feathers, Fowler wings, and the aileron Frize. The metal wing is covered with aluminum sheets. The wing has two interconnected fuel tanks. Horizontal empennage is also covered with aluminum and fiberglass ends. Aileron turns up to 300 up and 170 down. The bell crank makes the ailerons move. The flap is connected through a torque tube which is connected to an electric motor. Flaps turn from -4 ° to 40 °. The control cover is placed on the cockpit center console.

This aircraft has the main gear Wittman and trailing link nose gear. Operated through throttle and brake. Two main wheels are mounted in the landing gear socket. The main wheels are placed on an aluminum fork. The nose wheel can rotate 360 ​​°. This aircraft has a differential braking system which is operated from the pilot and passenger seats.

Kolb Flyer Super Sport Engine and Performance

The Kolb Flyer SS aircraft is powered by a single Rotax 912 S engine that produces an output power of 100 hp (74.6 kW). The engine has a maximum continuous power of 95 hp (70.87 kW). This aircraft allows the installation of various engines because of its long nose. The aircraft can fly with a maximum cruising speed of 216.6 km / h with a climbing rate of 1.234 fpm. Two fuel tanks (in each wing) have a capacity of 14 gallons (53 liters) each, giving the aircraft endurance for five hours.

Kolb Flyer SS Cockpit

Kolb Flyer Super Sport Cabin and Cockpit

The Kolb Flyer SS cabin has two seats side by side for the pilot and co-pilot. The seat can be electrically adjusted through the rocker switch located between the seats on the center console. Adjustable seats allow pilots more than 183 cm tall to sit comfortably. Pilots can access the baggage compartment through the cargo door. The luggage area behind the seat is a little longer than at Pelican. Additional doors at the rear allow easier movement for pilots.

Kolb Flyer Super Sport Price

The price of the latest Kolb Flyer SS (Super Sport) aircraft is around US $ 104,300.

Saturday, 7 December 2019

Vans RV-14 Specs, Interior, Cockpit, and Price

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Vans RV-14 Specs, Interior, Cockpit, and Price – The Vans RV-14 is the latest two-seat light sport aircraft designed and manufactured by Van's Aircraft headquartered in Oregon, United States. This aircraft can be used for the purpose of sports tours and basic/ advanced pilot training. The first prototype RV-14 aircraft completed its first flight test in July 2012. Another variant of this aircraft is the RV-14A.

Vans RV-14 light sport aircraft

Vans RV-14 Specs

The RV-14 aircraft are built based on the RV-10 aircraft with similar features including the tail wheel and nose of the aircraft. The fuselage is made of aluminum and uses wings with airfoil. The aircraft has components such as wing spars, pre-installed bubble canopies, pre-installed cables and avionics systems that are easy to assemble.

The overall dimensions of the RV-14 aircraft include a length of 6.43 m, a height of 2.48 m, and a wingspan of 8.23 ​​m. It has a wing area of ​​11.7 m². A large wing and flap area allows planes to land at short distances. It can also land on grass, dirt, and gravel runways.

The standard RV-14 aircraft has a conventional two-seat landing gear with rear wheels. The wheel consists of leaf springs made of steel. It has 4 × 1 fixed wheels between leaf springs at one end and the plane at the other side. Meanwhile, the RV-14A version is equipped with a fixed tricycle type landing gear tricycle.

Vans RV-14 specs

Vans RV-14 Engine and Performance

The RV-14 aircraft is powered by a Lycoming IO-390 engine which produces an output power of 210 hp. This four-cylinder engine has a fuel capacity of 50 gal. RV-14 aircraft can fly with a maximum cruise speed of 330 km / h and go at 305 km / h using 70% power. The aircraft can travel up to 1,400 nm in eight hours of flight. It has a range of 938 mi with a light weight and 925 mi with a gross weight.

The aircraft's takeoff distance is 160 m, and landing distance is 166 m. This aircraft has a climbing rate of 1,500 feet / minute and a maximum ceiling of more than 18,000 ft (5,486 m). The aircraft weighs around 1,700 lb (771 kg), while the maximum take-off weight is 2,050 lb (930 kg).

Vans RV-14 Cockpit and Avionics

The RV-14 cockpit is equipped with the Skyview avionics system supplied by Dynon Avionics. This system has a standard cable harness to handle the usual electrical basics such as lights, fuel pumps, flaps, and trims.

Wiring harness also has a convenient plug-and-play expansion capability for electronic flight instrumentation systems (EFIS). This can significantly reduce pilot workload due to the fast and positive response of the aircraft to small control inputs.

Vans RV-14 interior

Vans RV-14 Cabin and Interior

The RV-14 cabin is designed with a two-seat interior side by side. The large cabin can accommodate one passenger and one pilot. The cabin has wider head and legroom and is equipped with a large bubble canopy that can increase passenger visibility in all directions.

The aircraft has a maximum luggage capacity of 100 lb which is located behind the instrument panel. In addition, the aircraft is equipped with a exhaust system that keeps noise inside the cabin at low levels.

Vans RV-14 Price

The price of the latest Vans RV-14 light sport aircraft is around US $ 130,000. Prices depend on the kit option selected. An RV-14 aircraft ready to fly can be assembled at a cost of at least around $ 90,000. At present, the company has produced 113 aircraft and has been sent to various operators throughout the world.

Thursday, 5 December 2019

Vans RV-12 Specs, Interior, Cockpit, and Price

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Vans RV-12 Specs, Interior, Cockpit, and Price – The Vans RV-12 is a single-engine, two-seat light sport aircraft manufactured by Van's Aircraft headquartered in Oregon, United States. The first RV-12 flight took place on November 9, 2006 and began operating in April 2008. The aircraft kit is available in six separate sub-kits: empennage or tailcone kits, wing kits, aircraft kits, finish kits, avionics kits and powerplant kits. The latest variant of the RV-12 is the RV-12iS which is equipped with the latest avionics engine and suite.

Vans RV-12 light sport aircraft

Vans RV-12 Specs

RV-12 is designed in accordance with the standards of lightweight sports aircraft. The fuselage is made of all-metal materials, especially aluminum. This aircraft has a unique design and is claimed to be more efficient than the RV-9A. The aircraft is equipped with flapers and full-span stabilizers that are small enough to allow the aircraft to fit in the trailer. The aircraft can be navigated in various directions via a controlled nozzle. Diemnsi overall aircraft includes a length of 6.12 m, a wing width of 8.15 m, and a height of 2.53 m.

RV-12 aircraft have removable wings, gear kits or wheel fairings, stabilizers, strobe, landing and position lights, canopies, and computer punch machines. The wing can be easily removed in a few seconds by two people by simply pulling a pair of pins located behind the seat. The removable lightweight wing allows the RV-12 to be parked at home or hangar. The aircraft is equipped with a ignition system to prevent engine start if the wing is not installed properly.

The RV-12 landing mechanism is a fixed tricycle-type landing gear. The wheels are built with steel leaf springs and are equipped with hydraulic disc brakes. It was also equipped with three 5 × 5 wheels which were located one under the nose and two under the fuselage.

Vans RV-12 engine

Vans RV-12 Engine and Performance

The RV-12 is powered by a single Rotax 912ULS engine that can produce an output power of 74 kW to drive a two-bladed Sensenich composite propeller. The engine is equipped with four-stroke and four-cylinder air conditioners, which offer electronic dual ignition, electric starter, air intake and exhaust system. The engine weighs around 56.6 kg and its displacement is 82.6 inches (2 m³). This engine offers an external 12V DC alternator.

RV-12 aircraft can fly with a maximum speed of 223 km / h and a cruise speed of 210 km / h. While the stall speed is 75 km / hour. The service range and ceiling are 893 km and 4,206 m, respectively. The RV-12 aircraft requires a 213 m takeoff distance and 160 m landing distance. This aircraft weighs around 340 kg and the maximum take-off weight is 600 kg.

Vans RV-12 cockpit

Vans RV-12 Cockpit and Avionics

The RV-12 cockpit can accommodate 2 seats for pilots and passengers in side-by-side configurations. The Dynon D180 cockpit is integrated with avionics suite including the Garmin SL-40 communication radio, Flightcom intercom, Artex 406 emergency locater transmitter, Garmin GTX-327 transponder and Garmin 496 global positioning system.

The Dynon AP74 and Dynon D100 passenger side electronic flight instrumentation systems are also installed as standard. The switches and fuses incorporated in the glass panel control the entire RV-12 circuit. The glass fiber panel which is equipped with a cockpit avionics system is provided by Garmin Avionics.

Vans RV-12 Cabin and Interior

The RV-12 aircraft has a spacious and comfortable cabin in an advanced cabin configuration. The cabin has a width of 1.09 m and is equipped with a specially built canopy providing clear visibility to the pilot. Two chairs are located in front of the main pillar, not above. The cabin is equipped with a 22 kg luggage compartment located behind the seats. The RV-12 consists of interior panel kits in various colors with matching seat cushions.

Vans RV-12 Price

The price of the latest Vans RV-12 light sport aircraft is around US $ 135,000 for the base model and $ 145,000 for the premium version with two-screen glass panels, automatic pilots, and luxury interiors.

Tuesday, 3 December 2019

Vans RV-10 Specs, Interior, Cockpit, and Price

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Vans RV-10 Specs, Interior, Cockpit, and Price – Vans RV-10 is a single engine four-seat lightweight aircraft manufactured by Van's Aircraft headquartered in Oregon, United States. The aircraft made its first flight in May 2003 and began operations in September 2003. The aircraft can be used in a variety of missions including private and corporate transportation.

The RV-10 aircraft offers low operating costs, superior performance and minimal maintenance. The aircraft can reduce pilot workload because it responds quickly to small control inputs. The aircraft is equipped with gull winged doors that give the impression of luxury and futuristic.

Vans RV-10 light sport aircraft

Vans RV-10 Specs

The RV-10 aircraft has a low-wing monoplane design which was originally designed as a touring aircraft. Airplane design mainly focuses on greater stability and payload. The fuselage is made with aluminum, while the gull winged doors are made with composite materials. RV-10 has aerobatic features and a lighter management ability. The overall dimensions of the aircraft include a length of 7.44 m, height of 2.64 m, wing width of 9.68 m, and wing area of ​​13.7 m².

The RV-10 landing gear has a fixed, non-retractable tricycle that allows the aircraft to land on small airports, grass, gravel or sidewalks with very short runways. The landing gear is built with strong tubular steel. The nozzle mounting tube is connected to the engine mount and the aircraft can maneuver with differential braking. Brakes are mounted to the steering wheel toes.

The RV-10 aircraft has two brightly colored light emitting diode (LED) displays, multi-function or high-speed processing systems and two gull winged doors. The LED will offer high visibility displaying red and green range values. Green is indicated when the aircraft is within range. When an airplane is out of range, the numbers will appear red.

Vans RV-10 engine

Vans RV-10 Engine and Performance

RV-10 is powered by a single six-cylinder Lycoming IO-540D4A5 engine. The machine can produce power of 235 hp up to 260 hp. The engine moves Hartzell's fixed bladed two speed blades to speeds of 2,700 rpm. The aircraft is equipped with a fuel tank with a capacity of 60 US gallons.

RV-10 aircraft can fly with a maximum speed of 332 km/ h and a cruising speed of 323 km/ h. The range and ceiling of aircraft services are 1,600 km and 6,100 m, respectively. The aircraft can ride at speeds of 7.4 m/ s. This aircraft has an empty weight of around 689 kg and the maximum take-off weight is 1,181 kg. The loaded weight is 1,225 kg.

Vans RV-10 interior

Vans RV-10 Cabin and Interior

The spacious RV-10 cabin can accommodate 4 passengers. The cabin can be accessed through doors mounted on each side of the fuselage. The cabin has ample leg room so as to provide more comfort for passengers. The cabin interior is designed with oregon aero seats and seat cushions to give the airplane a luxurious feel. The aircraft baggage compartment can hold 45.3 kg and is accessed through the baggage door on the left. The back seat can be removed in a few minutes to provide additional luggage space.

Vans RV-10 cockpit

Vans RV-10 Cockpit and Avionics

The RV-10 cockpit is equipped with a fiber glass panel with a center console provided by Accuracy Avionics, Inc. The avionics suite installed in the cockpit includes the primary flight display (PFD), multi-function display (MFD), dual battery system, flap control, power breaker, lighted switch, and electronic flight instrumentation system (EFIS).

Vans RV-10 Price and Orders

The price of the latest Vans RV-10 aircraft is around US $ 127,485. Until now Van's Aircraft has produced 933 RV-10 units and has been operated by various operators throughout the world.

Sunday, 1 December 2019

Tecnam P2010 Specs, Interior, Cockpit, and Price

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Tecnam P2010 Specs, Interior, Cockpit, and Price – The Tecnam P2010 is a single-engine, four-seat lightweight aircraft manufactured by Tecnam, an Italian manufacturer of light sport aircraft. This aircraft was first launched at the 2011 Aero Friedrichshafen event held in Germany. This can be used in a variety of operations including personal and business transportation.

The first Tecnam P2010 flight took place in April 2012 at the Tecnam Capua production facility in Italy. This aircraft was certified by the European Aviation Safety Agency (EASA) in September 2014 and the United States Federal Aviation Administration (FAA) certification in December 2015.

Tecnam P2010 light aircraft

Tecnam P2010 Specs

The Tecnam P2010 fuselage has an aerodynamic structure made of all carbon fiber materials. The aircraft has a high wing structure made of metal and is based on NACA63A aerofoil. The use of carbon fiber in the fuselage will provide fuel efficiency, while the metal wing provides strength and stability. Overall aircraft dimensions include a length of 7.9 m, height 2.7 m, and a wingspan of 10.3 m. It has a wing area of ​​14.6 m2 and a diameter of 1.88 m.

The aircraft's wings are designed with partial tapering which makes it close to the optimal lift distribution (ellipse). The aircraft is equipped with an all moving horizontal type tail (stabilator) which allows for excellent control and longitudinal stability. The aircraft's main control is the conventional type which is operated by a control wheel and steering wheel. Flight controls also include hydraulic brakes, caster nose wheels and parking brakes.

Tecnam P2010 is equipped with a fixed tricycle type landing gear designed to minimize drag. The aircraft propulsion system is a fixed two-blades propeller and can also be installed with a three-variable blades, depending on the engine option used.

Tecnam P2010 Engine and Performance

The Tecnam P2010 is powered by a single Lycoming IO-360-M1A engine that can produce an output power of 180 hp or Lycoming IO390-C3B6 with an output power of 215 hp and 2,700 rpm rotation. The engine has four cylinders and a double magneto ignition system. Two integral fuel tanks installed in the wing box at the rear of the main spar with a total fuel capacity of 210 l.

Tecnam P2010 aircraft can fly with a maximum cruise speed of 136 km / h and have a maximum range of up to 1,222 km. The maximum aircraft takeoff weight is 1,160 kg, landing weight is 1,157kg, and empty weight is 710 kg. The aircraft has a service ceiling of 4,572 m and a climbing rate of 5.3 m / s at sea level. The landing distance is 200 m.

Tecnam P2010 cockpit

Tecnam P2010 Cockpit and Avionics

Tecnam P2010's cockpit is equipped with the Garmin G500 avionics. The cockpit is equipped with a 6.5 in. Liquid crystal display and multifunctional display capability to display all flight information to the pilot. It is also equipped with a magnetic compass, GMA 340 audio panel, avionic circuit breaker panel, and GTX 328 transponder. The latest version of the Tecnam P2010 is equipped with the latest generation Garmin G1000 Nxi IFR twin screen display, the new Flat-Panel Suite with integrated GFC700 autopilot.

The cockpit also features indicators for HIS air velocity attitude, vertical speed, outside air temperature (OAT), actual air velocity (TAS), ground speed, wind direction, heated pilot system, and ELT Remote Switch / Annunciator. In addition, the aircraft is equipped with audible stall warnings, stabilizer trim position indicators, and handheld microphones. It also has five types of antennas, which include Beacon Markers, transponders, VHF / GPS, NAV antennas, and emergency locator transmitters.

Tecnam P2010 interior

Tecnam P2010 Cabin and Interior

The Tecnam P2010 cabin can accommodate 4 passengers including the pilot in a two-row seating arrangement side by side. The cabin is designed to provide comfort for pilots and passengers. The cabin has a modular design that is designed to use analog or digital instrumentation packages. Overall, the cabin has a length of 3.13 m, width 1.14 m, and luggage compartment with a volume of 2.5 m³.

Tecnam P2010 Price and Orders

The price of the latest Tecnam P2010 aircraft is around US $ 350,000. The company has received more than 40 orders since it was introduced in April 2011.