Airplane Update

Wednesday, 29 January 2020

PC-Aero Elektra One Solar Specs, Engine, and Price

Admin 01:00

PC-Aero Elektra One Solar Specs, Engine, and Price – Elektra One Solar is a one-seat solar electric aircraft developed by PC-Aero. The aircraft was launched at the AERO Global Show for General Aviation which was held in Friedrichshafen, Germany in 2012. The flight test was conducted in the Alps in the municipality of Unterwössen in Germany in June 2015. The aircraft crossed the Alps across Grossglockner at an altitude of more than 3,000 m and landed after about two hours and 190 km of flights at the airfield at Zell View in July 2015.

Until now, PC-Aero is still developing the Elektra One Solar aircraft and hopes to get a type certification from Germany for the ultralight class (LTF-UL) and the FAR 103 ultralight class certification for future aircraft. Electra Two Record and Electra Two Standard are two other variants of the aircraft which are currently under development.

PC-Aero Elektra One Solar Specs

The Elektra One Solar aircraft was developed based on the fuselage of the Electra One battery powered model. This solar electric aircraft covers a longer wind range with 6 m² of solar cells on its surface offering more than 1kW of power to fly. It can fly for more than three hours without CO2 emissions and without noise.

The Elektra One Solar aircraft will be produced in different versions ranging from the wing span of 8.6 m and 15 m. Its external dimensions include a wingspan of 11m, and a wing surface of 8.2 m². It was built with lightweight carbon composite materials, while solar cells are produced by SolarWorld. It features autonomous flight control, which is also made of composite materials. The aircraft is equipped with new wings that are upgraded to reduce aerodynamic drag.

The aircraft is equipped with a mobile electric charging station, a sun hangar and a solar trailer. It is equipped with an onboard 5 cm resolution camera for 3D landscape mapping, developed by partner company Elektra UAS.

PC-Aero Elektra One Solar Engine and Performance

The Elektra One Solar aircraft is powered by 280 solar cells on the wing surface, which provide about half of the energy needed to fly. The energy from solar cells is combined with modern Li-Ion batteries of 11.5 kWh, which produce a constant power of around 16 kW to drive an electric motor and run other flight instruments. The aircraft uses the power of 2.5 kW in horizontal flight.

Elektra One Solar aircraft can fly with a cruising speed of 140 km / h and can cover a maximum distance of up to 1,000 km. The aircraft's maximum endurance exceeds eight hours. The aircraft has an empty weight of 100 kg, a battery weight of 100 kg, and a maximum take-off weight (MTOW) of 300 kg with a load capacity of 100 kg. The aspect ratio of the aircraft is 14: 7 and the best glide ratio is 30.

PC-Aero Elektra One Solar Price

The price of a Elektra One Solar aircraft is around US $ 150,000. But until now, PC-Aero has not given an official statement about the price of the aircraft, this is because the aircraft is still under development.

Monday, 27 January 2020

Light Sport Aircraft

Airbus E-Fan Specs, Engine, Cockpit, and Price

Admin 01:00

Airbus E-Fan Specs, Engine, Cockpit, and Price – E-Fan is an experimental two-seat electric aircraft designed and developed by Airbus Group in collaboration with other consortium partners. This aircraft was launched and conducted its first public flight demonstration at Bordeaux-Mérignac Airport in France in April 2014. The aircraft was developed with the aim of flying clubs and schools and can be used to train professional pilots.

Flight tests on the E-Fan 2.0 prototype are currently underway, while development of the production version is expected to begin in June at a production facility near Bordeaux Airport. BpiFrance Public Investment Bank will provide some funds for development. Currently Airbus is also developing a four-seat version of the E-Fan 4.0 aircraft.

Airbus E-Fan Specs

E-Fan airframe construction is made from all-composite materials provided by the French company Aéro Composite Saintonge (ACS). This also includes a pyrotechnic parachute rescue system. The aircraft is equipped with a video camera mounted on the fuselage to provide security, maintain contact with the pilot and monitor flight parameters. The overall dimensions of the aircraft include a length of 6.67 m and a wingspan of 9.5 m.

The E-Fan aircraft are designed to meet flight and aeroclub training requirements, considering hangar parking spaces and flight endurance criteria. In addition, the development of aircraft also aims to meet emission standards set out in the European Commission report (Flightpath 2050) on the European Vision for Aviation. This report sets targets compared to the 2000 standard, which includes reducing aircraft carbon dioxide emissions by 75%, nitrous oxide emissions by 90% and noise levels by 65%.

The E-Fan landing gear wheel consists of two electrically movable wheels that are positioned fore and aft under the fuselage. It also includes two small wheels under the wing. The rear main wheels include an electric motor with 6 kW of power which provides transport and acceleration of up to 60 km / h when taking off. This device is designed to reduce overall power consumption during operation.

Airbus E-Fan Engine and Performance

The E-Fan is powered by two electric motors with a combined power output of 60 kW. The motor is equipped with two fans to distribute and increase static thrust, reduce perceived noise, and improve safety on the ground. The power source to drive the electric motor is provided by a 250 V lithium-ion polymer battery produced by KOKAM. Lithium polymer batteries are equipped with 120 cells with a rated capacity of 4V per cell in addition to a spare battery for emergency landing purposes. The battery pack is located on the wing of the aircraft and can be recharged in one hour.

The E-Fan is also equipped with a telemetry system, which records all parameters of the drive, battery and engine and transmits them to the earth station. E-Fan aircraft can fly with a cruise speed of 160 km / h and a maximum speed of 220 km / h. The endurance of the aircraft ranges between 45 minutes and 1 hour.

Airbus E-Fan Price

The price of an Airbus E-Fan electric aircraft ranges from US $ 167,000 to $ 222,800. But until now, Airbus has not given an official statement about the price of the aircraft, this is because the aircraft is still under development

Saturday, 25 January 2020

Light Sport Aircraft

Extra 330LE Specs, Engine, Cockpit, and Price

Admin 01:00

Extra 330LE Specs, Engine, Cockpit, and Price – Extra 330LE is a two-seat electric-powered aerobatic aircraft designed and developed by Extra Aircraft based in Germany. This aircraft was launched at AERO Friedrichshafen in April 2016. The aircraft is equipped with an Siemens electric engine, making the aircraft completely silent.

The first Extra 330LE flight test using an Siemens-electric drive system was carried out at the Schwarze Heide landing field in Hünxe in June 2016, while the first full flight was completed at Schwarze Heide Airport in July 2016.

During the first flight test, the Extra 330LE aircraft reached an altitude of 3,000 m in only 4 minutes and 22 seconds at a speed of 11.5 m / s, which was officially recognized by the Fédération Aéronautique Internationale (FAI) as the world record climbing performance in November 2016. It reached the highest speed 337.50 km / h at a distance of 3 km, and was also the first aircraft to pull an LS8-neo type glider to an altitude of 600 m in 76 seconds in March 2017.

Extra 330LE Specs

The Extra 330LE aircraft is designed based on the Extra 300LP two-seat aircraft. The 330LE fuselage is built with lightweight material and is suitable for 20-minute flights, including takeoff, climbing and full throttle flights for 5 minutes. The overall dimensions of the aircraft include a length of 7.5 m, height 2.6 m, wingspan 8 m, and a total wing area of 10.84 m².

The aircraft has an electric drive system five times larger than other systems currently available on the market, allowing it to provide a means of sustainable transportation with carbon-free emissions. The company noted that the success of the first prototype aircraft flight in a two-seat tandem arrangement powered by an electric motor would make the development of electric-powered aircraft with four or more seats possible in the future.

Extra 330LE Engine and Performance

The Extra 330LE aircraft is powered by an electric SP260D motor with an output power of 260 kW (348 hp). The electric motor was developed by Siemens with support from the German Aeronautics Research Program (LuFo). The motor drives the MT-Propeller propeller directly without using a transmission, and can produce 2,500 rpm at rational speed.

The electric motor has a continuous torque of 1,000 nm and a link voltage of 580 v. The motor has a maximum cooling inlet temperature of 90 ° C and an efficiency of 95%. The aircraft's power is provided by two battery packs, each with 14 high-power Li-Ion battery modules with a capacity of 18.6 kWh.

The aircraft's motorcycle weighs 50 kg including air cushion, and has a low power-to-weight ratio, five kilowatts per kilogram, which is achieved using new simulation techniques and sophisticated lightweight construction. The overall weight of the Extra 330LE aircraft is around 1,000 kg, while the average climbing rate is 2,300 ft / m.

Extra 330LE Price

Until now, the Extra Aircraft company has not announced the price of the Extra 330LE aircraft, because the aircraft is still under development.

Thursday, 23 January 2020

Light Sport Aircraft

e-Go Aircraft Specs, Interior, Cockpit, and Price

Admin 01:00

e-Go Aircraft Specs, Interior, Cockpit, and Price – The e-Go (e-Plane) is a one-seat light sport aircraft (LSA) designed and developed by e-Go Aeroplanes (GioCAS Aeronautical), a British aircraft manufacturer. This aircraft was developed under the Single Seat Deregulated (SSDR) category in the United Kingdom. The first flight prototype SSDR e-Go aircraft took place in October 2013. The first production aircraft were delivered to customers in June 2016.

The e-Go aircraft is also available in another variant, e-Go plus. the aircraft was developed in accordance with US light sport aircraft rules, and the Fédération Aéronautique Internationale's microlight rules. Production is set to resume shipping in 2020.

e-Go Aircraft Specs

e-Go aircraft are designed by Giotto Castelli and are built using carbon fiber. The fuselage weighs around 12 kg and the main wing panel weighs around 20 kg. The main wing stays at zero angle when the plane is on the ground. The wing can be removed by moving a single lever on each side with an aileron control that connects and disconnects automatically. This includes the electrical system rather than the manual system.

The overall dimensions of the e-Go aircraft include a length of 3.79 m, a height of 1.8 m, a wingspan of 7.99 m, and a wingspan of 11.5 m². This aircraft has an empty weight of 139 kg and can carry a maximum mass of 270 kg. This requires a ground roll taking off more than 200 m, and a 150 m ground roll.

e-Go Aircraft Engine and Performance

e-Go aircraft are powered by a Rotron e-Go rotary engine which produces an output power of 30 hp at 6,500 rpm. It has a 30 liter fuel capacity with an option to increase tank capacity up to 40 liters. He uses unleaded mogas as fuel. Fuel consumption is 65 mpg at 166 km/ h.

e-Go aircraft can fly with aircraft cruising speed is 167 km/ h, speeds never exceed 222 km/ h, and kiosk speeds of 65 km/ h. The aircraft has a climbing rate of 900 ft / min (4.6 m/ s), a service ceiling of 10,000 ft (3,050 m), and a range of 610 km (330 nm).

e-Go Aircraft Cabin and Interior

The e-Go aircraft cabin can accommodate one passenger and pilot. The mass of pilots that can be accommodated ranges between 60 kg and 100 kg, and the mass of baggage up to 15 kg. Ventilation is provided by temperature controlled air ventilation and removes mist through slots in coaming. Storage space is provided for charts, snacks and luggage behind the seats. The cabin features a glider style canopy that allows entry and exit easily.

e-Go Aircraft Cockpit and Avionics

The e-Go aircraft is equipped with a complete glass cockpit integrated with Kanardia NESIS III's large screen electronic flight instrument system (EFIS). EFIS is connected to the data acquisition system and the Rotron Wankel rotary engine control unit (ECU) via the controller area network bus (CANbus). It also includes an 8.3 kHz radio, and an S transponder mode ADSB developed by Trig.

The avionics suite of e-Go aircraft includes engine monitoring, checklists and navigation systems. Also includes adjustable steering pedals and conventional controls for throttle, elevator, steering and aileron.

e-Go Aircraft Price

The price of the latest e-Go light sport aircraft is around US $ 80,000.

Tuesday, 21 January 2020

REMOS

REMOS GXiS Specs, Interior, Cockpit, and Price

Admin 01:00

REMOS GXiS Specs, Interior, Cockpit, and Price – REMOS GXiS is a new two-seat light sport aircraft manufactured by REMOS, Germany. This aircraft was introduced at the AERO Friedrichshafen which was held in Germany in April 2016. The first prototype was run on April 7, 2016 and completed the first flight test in May 2016. The aircraft was designed to obtain light sport aircraft certification (LSA) from the European Aviation Safety Agency (EASA ). It is also available in an ultralight version which is marketed in Europe. In addition the aircraft are also marketed in the North American region through an exclusive distributor, Skybound Aviation.

REMOS GXiS Specs

The GXiS fuselage is built with composite materials and has a high wing configuration. The aircraft's forward-firewall section was redesigned, and all system checks on the aircraft can now be carried out automatically. The aircraft is designed to meet the requirements of modern general aviation. It features new engine features, avionics and a new cover design, as well as including an easy start-up procedure called SMARTstart.

The overall dimensions of the REMOS GXiS aircraft include a length of 6.60 m, a height of 2.28 m, a wingspan of 9.32 m, and a wingspan of 10.97 m². This aircraft has a maximum take-off weight (MTOW) of 600 kg, and requires a take-off distance of 322 m and a landing distance of 233 m. The ultralight version weighs 472.5 kg.

REMOS GXiS Engine and Performance

The REMOS GXiS aircraft is powered by a Rotax 912iS sport engine with electronic fuel injection that generates power of 74 kW (100 hp). The engine drives a three-bladed MT-Propeller propeller. The propeller is available in a version of speed and constant speed. The ultralight version is equipped with a fixed three-blades propeller developed by NEUFORM.

REMOS GXiS aircraft can be boasted with a cruise speed of 189 km / h, kiosk speed of 77 km / h, normal operating speed of 198 km / h, maneuver speed of 174 km / h, and a maximum speed of 220 km / h. The aircraft has a maximum range of 975 km (526 nm) and endurance of 6.5 hours.

REMOS GXiS Cockpit and Avionics

The REMOS GXiS cockpit can accommodate two personnel consisting of a pilot and a passenger. The 1.19m wide cockpit is equipped with the Dynon SkyView SE avionics suite. The avionics suite includes a 10-inch touch screen combined with an electronic flight instrument system (EFIS), an engine monitoring system (EMS) and a Dynon SV-D1000T / B display system.

The transponder installed in the cockpit sends an ADS-B signal to show the surrounding traffic on EFIS. The center stack includes the Garmin GTN 750, a complete navigation system and control panel for radios, audio panels, and transponders. The aircraft is equipped with the TRX-1500 collision avoidance system developed by Air Avionics, and the GXiS ballistic parachute made by BRS.

REMOS GXiS Price

The price of the latest REMOS GXiS light sport aircraft is around US $ 200,000.

Sunday, 19 January 2020

Tomark

Tomark Viper SD-4 Specs, Interior, Cockpit, and Price

Admin 01:00

Tomark Viper SD-4 Specs, Interior, Cockpit, and Price – The Viper SD-4 is a two-seat light sport aircraft designed and developed by TomarkAero. This aircraft can be used for sports, entertainment and recreational flying. This aircraft completed the SPIN test in November 2015. The SPIN test is required to obtain a certificate from the European Aviation Safety Agency (EASA) in the CS-LSA category. It received an EASA type certification in March 2016 and began production at the Tomark facility located in Prešov in Slovakia. Light sport aircraft on display at the AERO Friedrichshafen in April 2016.

Tomark Viper SD-4 Specs

Viper SD-4 aircraft were developed using CAD design and CNC precision cutting methods. The fuselage is built with an all-metal semi-monocoque and frame structure, with aluminum alloy stringer and leather. Integrated airframe with vertical stabilizers and steering. Includes an elevator equipped with a trimming tab. The aircraft engine compartment is built separately from the crew compartment. It is separated by a steel firewall and also includes a three-point harness. The overall dimensions of the aircraft include length of 6.4 m, height of 2.2 m and wingspan of 8.4 m.

The Viper SD-4 aircraft is equipped with a tricycle landing gear. This includes composition springs and hydraulic disc brakes on wheels controlled from the center panel. The front landing gear wheel is equipped with a slim cover and rubber band for bearings. This aircraft can optionally be equipped with a towing hook for use as a towing tower that can take off with weights of up to 750 kg. The aircraft's empty weight is 285 kg, while the maximum take-off weight (MTOW) is 472.5 kg.

Tomark Viper SD-4 Engine and Performance

The Viper SD-4 is powered by a four-stroke, four-cylinder Rotax 912 engine with a liquid-cooled cylinder head and an air-cooled cylinder. The engine produces an output power of 100 hp to drive the fixed-pitch and variable-bladed propeller blades. To support engine performance, the aircraft is equipped with a fuel tank with a capacity of 100 liters.

Viper SD-4 aircraft can fly at cruise speeds of 200 km / h, kiosk speeds of 75 km / h, and never exceed 240 km / h. It has a maximum range of 1,100 km (594 nm), climbing rate of 5 m / s and a service ceiling of 5,000 m (16,404 ft). The aircraft requires a distance of 180 m for take-off and 160 m for landing.

Tomark Viper SD-4 Cockpit and Avionics

The Viper SD-4 aircraft cockpit is integrated with the latest avionics technology with extensive utility options including aviation, navigation, communication, and top monitoring systems with large-sized liquid crystal (LCD) screens. These include lifts, ailerons controlled through push rods, and steering controlled through Bowden cables. Avionics further includes electric flaps, electric trims, autopilot, and ballistic recovery systems (AEPS).

Tomark Viper SD-4 Cabin and Interior

The spacious Viper SD-4 cabin can accommodate two personnel consisting of a pipolt and a passenger in an adjoining configuration. The cabin is covered by clear or colored canopies, which can be opened up and back. The cabin features three air vents on the sides of the fuselage.

Tomark Viper SD-4 Price

The price of the latest Tomark Viper SD-4 light sport aircraft is around US $ 159,900.

Friday, 17 January 2020

Magnus

Magnus eFusion Specs, Interior, Cockpit, and Price

Admin 01:00

Magnus eFusion Specs, Interior, Cockpit, and Price – eFusion is an all-electric two-seat light sport aircraft developed by Magnus Aircraft, a company based in Hungary, in collaboration with Siemens. This aircraft was launched at the AERO Friedrichshafen exhibition in Germany in April 2016. The first Magnus eFusion flight was conducted at the Matkópuszta airfield in Kecskemet, Hungary in April 2016. The aircraft was also developed for other categories including ultra-light (UL) and very light aircraft (UL) VLA). This aircraft can be used for interference recovery training with low operating costs.

Magnus eFusion all-electric light sport aircraft

Magnus eFusion Specs

The eFusion aircraft was developed based on a Fusion engine powered by a piston engine. This aircraft has a low-wing monoplane design that is equipped with symmetrical wings, a titanium firewall, and a central part made of chrome molybdenum alloy. The fuselage is mounted with a non-retractable three-wheeled landing gear. Overall aircraft dimensions include a length of 6.7 m, a height of 2.4 m, a wingspan of 8.3 m including winglets, and a wingspan of 10.59 m².

The aircraft is also equipped with a built-in parachute system (ballistic recovery system) that connects to the aircraft at three points and protects the entire aircraft in the event of an emergency. This serves to reduce the risk of accidents and improve flight safety. The aircraft has an empty weight of 410 kg and a maximum take-off weight (MTOW) of 600 kg. This requires a take-off distance between 120 m and 130 m, and a landing distance between 150 m and 200 m.

Magnus eFusion Engine and Performance

Magnus eFusion is powered by the Siemens 60 kW all-electric system to drive the propeller. This offers a low level of engine noise and minimal operating costs. This aircraft is fully battery powered and has an endurance of around one hour.

EFusion aircraft can fly with cruise speeds ranging from 185 km / h and 240 km / h. Kiosk and aircraft maneuver speeds are 64.8 km / h and 192.6 km / h, respectively. This aircraft has a maximum range of up to 1,100 km and a service ceiling of 12,000 ft.

Magnus eFusion Cabin and Interior

The Magnus eFusion cabin can accommodate two personnel consisting of a pilot and a passenger in a side by side seating configuration. The cabin is 1.17 m wide and features a glass canopy that will increase passenger visibility to 180 degrees.

Magnus eFusion Cockpit and Avionics

The Magnus eFusion cockpit is integrated with the avionics circuit that includes a video surveillance system with an onboard operator work station or a wireless video surveillance system with a ground station control version. It also includes daytime visible electro-optical (EO) sensors with object tracking systems and camera sensors and combined thermal EO sensors seen day and night. The aircraft can be optionally installed on autopilot, dual controls, attitude indicators, night visual flight rules (NVFR) packages, landing lights, heated pitots and leather seat covers.

Magnus eFusion Price

The estimated price of the Magnus eFusion all-electric light sport aircraft is around US $ 200,000.

Wednesday, 15 January 2020

Rans

Rans S-20LS Raven Specs, Interior, Cockpit, and Price

Admin 01:00

Rans S-20LS Raven Specs, Interior, Cockpit, and Price – The Rans S-20LS Raven is a two-seat light sport aircraft manufactured by RANS Designs, US. This aircraft was approved by the Federal Aviation Administration (FAA) under the Special Light Sport Aircraft (SLSA) category in March 2016. This also means the aircraft may be able to obtain type certification with minimal changes from the European Aviation Safety Agency (EASA).

Rans S-20LS Raven Specs

Construction The S-20LS Rans fuselage is constructed using a 4130 chrome-moly welded steel tube. The wing of the aircraft is a combination of aluminum tubes and stamped wing ribs, the leading ends of aluminum sheets and aluminum wing struts. All covered with cloth. The overall dimensions of the aircraft include a length of 6.4 m, 2 m height, 9.2 m wingspan and 14.1 m² wing area. The aircraft has an empty weight of 336 kg and a gross weight of 599 kg, and can carry up to 263 kg of useful load. The aircraft's wing loading capacity is 4 kg.

The aircraft is equipped with internal corrosion protection, classic steering, and ball bearing control pulleys. It is also equipped with double sided hydraulic foot brakes, parking brakes and braided stainless steel brake lines, and throttles mounted on a single panel. The landing gear includes 6 in. Hydraulic wheels and brakes, telescopic tunable steerable nose wheels, fully rotatable tail wheels, and buoy attachments.

Rans S-20LS Raven Engine and performance

The Rans S-20LS Raven aircraft is powered by a Rotax 912ULS engine which produces an output power of 100 hp. The engine drives a three-bladed drive warp propeller hub that can be adjusted to w-HP-L with a carbon fiber spinner. The fuel system includes a 26 gal fuel system and a gasolator fuel tank.

The Rans S-20LS Raven can fly at cruising speeds of 180 km / h and never exceed 209 km / h. It has a maximum range of 937km and an endurance of 5.2 hours. The aircraft service ceiling is 4,420 m (14,500 ft) and the climbing level is 900 fpm. The aircraft requires a distance of 91 m for takeoff and 104 m for landing.

Rans S-20LS Raven Cabin and Interior

The Rans S-20LS Raven cabin measuring 46 in. Can accommodate two passengers in an adjoining seating configuration. The cabin interior includes plush upholstered seats with map pocket and in-flight adjustments with three different reclining arrangements. The seat includes three lap points and shoulder belts. The cabin is equipped with a 21.2 ft luggage compartment with a maximum load capacity of 80 lb.

The cabin can be accessed through a 50 in curved door with a gas lifting cylinder to make it easy to enter and load luggage. These are equipped with cabin heat, and cabin air vent mounted on the dashboard. In addition, some additional equipment in the cabin includes a fire extinguisher mounted on the floor and a wind shield / avionics cooling fan.

Rans S-20LS Raven Cockpit and Avionics

The Rans S-20LS Raven cockpit is equipped with avionics circuit that includes dual control sticks, air speed indicator, vertical speed indicator, altimeter, engine gauge including RPM, oil pressure / oil pressure, volt meter and hour meter, and pedestal compass. It also integrates a Garmin GTR 200 radio with an intercom, a Garmin Aera 550 GPS, and a Garmin GTX 327 transponder. In addition, other instrument options that can be mounted on an aircraft include traditional analog, or Dynon or Garmin electronic flight instrument systems.

The Rans S-20LS Raven aircraft is also equipped with a gascolator, electric fuel pump, electric passenger elevator lift trim, canopy cover, carbon fiber cover, carbon fiber wing tips, and AVEO Vega TLR landing lights. The pilot control stick is mounted with an electric elevator trim with indicators on the panel.

Rans S-20LS Raven Price

The price of the Rans S-20LS Raven light sport aircraft is around US $ 119,000.

Monday, 13 January 2020

Vickers Wave

Vickers Wave Specs, Interior, Cockpit, and Price

Admin 01:00

Vickers Wave Specs, Interior, Cockpit, and Price – Vickers Wave is a amphibious light sport aircraft (LSA) designed and developed by Vickers Aircraft Company of Hamilton, New Zealand. The aircraft is designed to meet ASTM's international LSA standards, the aircraft only underwent flight testing 180 hours before being certified by the New Zealand Civil Aviation Authority (CAA). The aircraft was first introduced at the Sport Aviation Expo in Sebring, Florida in 2014. Since its introduction, Vickers Wave aircraft have received expressions of interest from several airlines in the US, Europe and Malaysia.

Vickers Wave amphibious light sport aircraft

Vickers Wave Specs

The Vickers Wave fuselage consists of an aluminum primary structure with carbon fiber hull that is resistant to corrosion. The entire fuselage, floating elements and fuselage skin of the aircraft are also made of carbon fiber supplied by Core Builders Composites. The aircraft can be operated from water and runways on land. The wings of the aircraft can be folded automatically and can be equipped with transportation trailers, and an electric davit hook recovery system for transportation on a cruise ship.

The Vickers Wave aircraft are equipped with Cross-Over fixed landing gear and an emergency aircraft recovery parachute system. It also includes an emergency locator transmitter (ELT), a vertical electric power management system, and an electrically powered water booster for engine-off, on-water maneuvers. Overall, the dimensions of the aircraft include a length of 7.5 m, a height of 2.29 m, a wingspan of 9.4 m and a wingspan of 13.87 m².

Vickers Wave Engine and Performance

The Vickers Wave seaplane is powered by the Intercooled Turbo ROTAX 915is engine which produces an output power of 141 hp. The engine moves the 72-in Catto three-bladed propeller. The aircraft uses Auto-Gas or Av-Gas fuel and has a full fuel capacity of 190 l.

Vickers Wave aircraft can fly with a maximum cruise speed of 222 km / h and a maximum range of 2037 km (1100 nm). The aircraft requires a distance of 182 m to take off and land. The aircraft has a maximum take-off weight (MTOW) of 839 kg and can carry a useful load of 295 kg.

Vickers Wave Cockpit and Avionics

The Vickers Wave cockpit is equipped with the Dynon SkyView SV-D1000 avionics device which integrates a high-resolution touch screen display. The screen has a high level of brightness and can be seen clearly even in direct sunlight. The SkyView avionics suite includes the COM-C25 CON radio, the SkyView 2S stereo intercom, the SV-XPNDR-261 transponder, and the S mode transponder.

The instrument panel also integrates standard equipment including flight control sticks, center consoles, iPad mini with electronic flight books, checklists, and backup electronic flight instrument systems (EFIS). Other avionics include SkyView automatic pilots and angle of attack (AOA) indicators.

Vickers Wave cabin and Interior

The Vickers Wave cabin has a length of 1.4 m, width 1.34 m, and height 1.20. The cabin can accommodate two personnel consisting of a pilot and a passenger. It has luggage space with a storage volume of 25 ft³ (0.71 m³). The cabin interior incorporates a heater and climate control fan, and has a double sliding door for safe and uncovered entry or exit, a high-visibility front windshield, drinking area, and seats with armrests and inertia windings, 4-point seat belts with airbags .

Vickers Wave price

The price of the Vickers Wave amphibious light sport aircraft is around US $ 180,000.

Saturday, 11 January 2020

MVP Aero

MVP Aero Model 3 Specs, Interior, Cockpit, and Price

Admin 01:00

MVP Aero Model 3 Specs, Interior, Cockpit, and Price – MVP Aero Model 3 is a two-seat amphibious light sport aircraft (LSA) designed and developed by MVP Aero Inc. of Delaware, US. This plane can be ground, air, water and snow. The first prototype of the Model 3 seaplane was first introduced at EAA AirVenture Oshkosh in 2014. This aircraft is being developed for the category of special light sport aircraft (S-LSA), and experimental light sport aircraft (E-LSA). MVP Aero began production of Model 3 aircraft in the US in collaboration with its strategic partner Glasair Aviation and Fibercraft.

MVP Aero Model 3 amphibious light sport aircraft

MVP Aero Model 3 Specs

The Model 3 aircraft was designed by Mike Van Staagen and produced by MVP Aero. The fuselage is built using carbon and glass composites. Fabric-coated wing construction provides light weight and strength. Overall, the dimensions of the aircraft include a length of 7.24 m in the extended wing position and 8.1 m when the wings are folded. The wingspan is 10.97 m in the open position and 2.44 m in width when the wings are folded.

The aircraft is equipped with re-positioned gears with standard airframe emergency parachutes and two specially designed high lift airfoils. The aircraft has manually folded wings and is able to land on land or water. This can be transformed into a versatile floating platform.

MVP Aero Model 3 Engine and Performance

The MVP Aero Model 3 is powered by a Rotax 914 engine that produces around 115 h of power. It has a fuel capacity of 26 gal along with additional tank facilities. The aircraft can fly with a maximum cruise speed of 193 km / h at sea level and stall speed of 76 km / h with full flaps. It has a maximum climbing rate of 1,000 fpm at sea level. It carries a useful load of 450 lb and has a wing loading capacity of 54 kg / m².

MVP Aero Model 3 Cockpit and Avionics

MVP Aero Model 3 has a glass canopy that fully covers the cockpit seat. The canopy moves up and back on the four-rod link, which is positioned above the machine pole. Pilots and passengers can move from the cockpit to the tail on the catwalk. The Model 3 aircraft cockpit is equipped with an instrument panel that has a standalone pod to provide protection from water droplets from swimwear and flip-flops. It also includes four hinged folding panels on the front deck.

MVP Aero Model 3 Cabin and Interior

The MVP Aero Model 3 cabin has a 1.17 m cabin width that can accommodate one pilot and one passenger. The aircraft seat can be removed and placed on the nose of the aircraft when relaxing or fishing. It has a flat floor from the bow to the rear of the trunk, which is adequate for two people to lie on. passengers can also sleep with a hammock that can be stretched between the engine pole and tail.

MVP Aero Model 3 Price

The price of the MVP Aero Model 3 amphibious light sport aircraft is around US $ 189,000.

Thursday, 9 January 2020

Light Sport Aircraft

ATEC 322 Faeta Specs, Interior, Cockpit, and Price

Admin 01:00

ATEC 322 Faeta Specs, Interior, Cockpit, and Price – ATEC 322 Faeta is a two-seater light sport aircraft (LSA) designed and developed by ATEC, Czech Republic. This aircraft can be used by flight training schools, couples, pilots and retired pilots. The aircraft underwent flight tests in October 2015 and is ready for shipping in the S-LSA category to US distributors.

ATEC 322 Faeta Specs

ATEC 322 Faeta was built based on the design and form of ATEC 122 Zephyr. The aircraft's wings are made of carbon fiber sandwich shells, the wing spars are made of hard beech-coated saturated with synthetic resin and the tail unit is made of all-composite material. The wing backs down with an angle of 5.5 °. Flaps, hinges, slots, Pitot tube enclosures, and wing tips were developed using a computer-aided design to get minimum airdrag.

The ATEC 322 Faeta tail unit has a T-shaped construction with a tapered horizontal tailplane, fix stabilizer, and elevator. The aircraft engine compartment is separated from the cabin by a firewall. This aircraft has a small window above the baggage compartment on both sides of the fuselage. It was also equipped with a modern USH 600 rescue system. Overall dimensions of the aircraft include a length of 6.2 m, 2 m high, 9.6 m wingspan, 2.4 m tail span and 2 m wheelbase.

The ATEC 322 Faeta aircraft has a fixed three-wheel landing gear and a steerable nose wheel. The main wheels are equipped with a pair of composite leaf springs and hydraulic brakes. The front legs of the landing gear are constructed with composites and rubber springs that can withstand loads up to 1,285 lb.

ATEC 322 Faeta Engine and Performance

The ATEC 322 Faeta aircraft is powered by a Rotax 912iS sport engine that produces an output power of 100 hp. The engine moves a two-bladed or three-bladed propeller that can be fixed, adjusted to the ground or can be adjusted in flight with manual or electric controls. The engine mount is welded with high quality chrome moly thin-walled steel tubes (CrMo). It has a fuel tank with a maximum capacity of 26.4 US gal (2 x 50 l).

The ATEC 322 Faeta aircraft can fly with a cruise speed of 211 km / h and a maximum speed of 235 km / h. The minimum speeds and aircraft kiosk speeds are 79 km / h and 60 km / h, respectively. It has a maximum flight range of 2,000 km (1,080 nm) and a climbing rate of 7.5 m / s. The aircraft has an empty weight of 300 kg, and a maximum takeoff weight (MToW) of 582 kg with a payload capacity of up to 172 kg.

ATEC 322 Faeta Cockpit and Avionics

The cockpit of ATEC 322 Faeta aircraft is equipped with a canopy that can be opened backwards. The avionics suite of aircraft includes basic analog instruments, including a glass cockpit, electronic systems for flight and engine monitoring, and navigation with a 9 in screen. It also includes dependent automatic surveillance - broadcast (ADS-B) - already using the Garmin transponder.

Avionics further includes position recorders, three-axis autopilot, and various GPS, radio, and emergency locator transmitters (ELT). It also includes a USB connector, MP3 and movie player. The pedal can be adjusted in three positions, according to the height of the pilot.

ATEC 322 Faeta Cabin and Interior

The ATEC 322 Faeta cabin can accommodate up to two passengers with side-by-side seating configurations. The cabin has two ergonomic chairs with a high-tech nanofiber fabric armrest in a variety of optional colors. The seat holder can be adjusted up or down and forwards or backwards. The cabin is also equipped with air ventilation and heating to improve air circulation for passenger comfort.

ATEC 322 Faeta Price

The price of the ATEC 322 Faeta light sport aircraft is around US $ 150,000.

Tuesday, 7 January 2020

Light Sport Aircraft

Evektor Harmony Specs, Interior, Cockpit, and Price

Admin 01:00

Evektor Harmony Specs, Interior, Cockpit, and Price – The Evektor Harmony is a two-seat light sport aircraft manufactured by Evektor-Aerotechnik, a company from the Czech Republic. This aircraft can be used for cross-country tour and training purposes. The aircraft obtained the USA FAA approval certificate in 2011 and the first aircraft were sent to the US that same year. The aircraft subsequently received a special airworthiness certificate from the Directorate General of Civil Aviation in Chile in May 2014.

Evektor Harmony Specs

The Evektor Harmony fuselage is made of all-metal, anodised and corrosion resistant. The aircraft structure joints are glued with mastic for long term service. This aircraft has a new tapered wing design, enlarged steering wheel, aerofil, and three-wheel landing gear. The aircraft is integrated with two internal wing tanks with a capacity of 60 l each. The dimensions of the aircraft include a length of 6.11 m, height of 2.48 m, and wing width of 9.25 m. The takeoff and landing distance of the aircraft is 190 m and 180 m, respectively. The aircraft has an empty weight of 311 kg, a maximum takeoff weight (MTOW) of 600 kg and a useful load capacity of up to 289 kg.

Evektor Harmony Engine and Performance

The Evektor Harmony aircraft is powered by a Rotax 912ULS engine which produces an output power of 100 hp. The propulsion propeller engine AES 1700/3 / R has three blades. The aircraft is also offered with two other engine options which include a 115 hp Rotax 914 turbo engine or a 100 hp Rotax 912iS / S2 engine with fuel injection system. The Rotax 914 turbo engine is intended for high altitude performance in mountainous or hot areas, while the Rotax 912ULS engine offers standard performance and weight reduction.

Evektor Harmony aircraft can fly with a cruise speed of 204 km / h, a maximum speed of 222 km / h and a stall speed of 83 km / h. The aircraft consumes fuel at an average of 15 l per hour and can fly up to a range of 1,300 km (700 nmi). The aircraft has a 15,500 ft service ceiling with an incline of 5.2 m / s.

Evektor Harmony Cabin and Interior

The Evektor Harmony Cabin has a width of 1.18 m which can accommodate two personnel consisting of a pilot and a passenger. The cabin has a luggage room with a volume of 10.1 ft³ which can accommodate a maximum weight of 25 kg. The cabin is equipped with a ventilation system with NACA inlet and canopy side ball holes. It integrates a standard chair with a low backrest, and luxurious interior lined. It also features a padded seat belt shoulder strap, side map pockets, and armrests. It also includes an open and closed canopy warning system, and an additional 12 V outlet.

Evektor Harmony Cockpit and Avionics

The spacious Evektor Harmony cockpit offers 46.5 in shoulder width and additional leg room. The cockpit is integrated with Dynon SkyView 10 in electronic flight instrument system (EFIS) and 7 in engine monitoring system (EMS), integrated Dynon radio plus transponders and night flight flight rules (VFR) equipment packages. The cockpit is equipped with a new design instrument panel, adjustable pedals, push-button circuit breakers, nose wheel steering, and a combination starter and choke lever. It is covered by a colored canopy which offers UV protection.

The Evektor Harmony avionics suite includes air speed indicators, altimeters, magnetic compasses, vertical speed indicators, bank indicators, dual hydraulic brakes with four pumps, dual control sticks, and mechanical flaps. The aircraft is also equipped with longitudinal, lateral, flap and nose wheel control via push / pull rods, and throttle control with friction locks.

Evektor Harmony Price

The price of the newest Evektor Harmony light sport aircraft is around US $ 125,000.

Sunday, 5 January 2020

ONE Pro

ONE Light Sport Aircraft Specs, Cockpit, and Price

Admin 01:00

ONE Light Sport Aircraft Specs, Cockpit, and Price – ONE is a safe, affordable and efficient light sport aircraft (LSA) designed and developed by ONE Pro, Slovenia. This aircraft can be used by flight training schools, couples, pilots and retired pilots. It underwent horizontal and static tests respectively in November 2012 and January 2013, and was exhibited at the AERO trade show held in Europe in April 2015. The sport-family configuration of the aircraft is currently in the process of being certified for CS-VLA (3-4 seat) with the European Aviation Security Agency (EASA). It was also certified for the US LSA configuration in 2016.

ONE Light Sport Aircraft Specs

The ONE aircraft has a smart design provided by Max Piucci. Overall aircraft dimensions include length of 6.97 m, height of 2.2 m and wingspan of 9.65 m. This aircraft has two spars, which overlap and bolt together to the fuselage. It is available with two and 2 + 1 seating configurations, and includes an airplane parachute and a 3D passenger roll safety cage compartment. Airplane doors are designed to be opened in case of a roll-over. The aircraft's three-wheel landing gear is equipped with an aerodynamic cover that integrates with the front legs.

ONE Light Sport Aircraft Engine and Performance

The ONE aircraft is powered by a Rotax 912ULS2 engine that can produce an output power of 100 hp. It has a fuel capacity of 135 l / 97 kg and is equipped with an intelligent engine management system. The aircraft can fly with a maximum cruising speed of 256 km / hour and stall speed with flaps of 65 km / hour. The aircraft's take-off and landing distance is 120 m and 350 m. The aircraft has a flying range of 1,600 km (864 nm), a maximum operating altitude of 4,500 m and a climbing rate of 5 m / s.

The empty weight and gross weight of ONE aircraft are 340 kg and 600kg, respectively. The aircraft has a useful carrying capacity of up to 260 kg. The standard blank weight in the 2 + 1 configuration is 350 kg, while the gross weight and carrying capacity of useful loads are 750 kg and 395 kg, respectively.

ONE Light Sport Aircraft Cabin and Interior

The cabin of the ONE aircraft is 2.25 m long, 1.23 m wide and 1.17 m high. The spacious and soundproof cabin is equipped with an ergonomically designed seat that can be adjusted and an ISOFIX connection for a child seat. The interior of the aircraft was designed with Max Piucci and MBVision. Adequate luggage space is provided.

The FEM-designed and tested cab has car-style collision resistance. The cabin also features a full Kevlar interior that provides protection from object penetration. This includes switches grouped with clearly recognizable positions, glove compartments for storing POHs, additional cameras or charts, and iPad installation.

ONE Light Sport Aircraft Cockpit and Avionics

The ONE aircraft cockpit has the SkyView Dynon avionics suite integrated with the Garmin radio communication system. This includes an instrument panel similar to a car dashboard, where the panel pulls back in the event of a collision. Avionics includes standard center-sticks and side-sticks.

This aircraft is integrated with an easy entrance and emergency exit. The aircraft is equipped with a 4 mm certified windshield which provides protection against birds and other objects. Three hinges are provided on each moving surface, and four on the wings.

ONE Light Sport Aircraft Price

The price of the latest ONE light sport aircraft is around US $ 110,000.

Friday, 3 January 2020

Lisa Airplanes

Lisa AKOYA Specs, Interior, Cockpit, and Price

Admin 01:00

Lisa AKOYA Specs, Interior, Cockpit, and Price – Lisa AKOYA is a two-seat amphibious light sport aircraft designed and developed by Lisa Airplanes, France. This aircraft can operate on land, water and snow, designed in accordance with the American community for international standards of testing and materials (ASTM) F37 for lightweight sport aircraft. The aircraft specifications have been certified by the European air safety agency for very light aircraft (CS-VLA).

The first flight of the Lisa AKOYA aircraft took place in August 2007. The aircraft was exhibited for the first time at the AirVenture convention in July 2012 and entered service at the end of 2016. The main components of the aircraft were produced in France, Italy, Germany and Austria, while assembly and tests, and quality control were carried out in the Lisa Airplanes' last meeting hall.

Lisa AKOYA amphibious light sport aircraft

Lisa AKOYA Specs

The Lisa AKOYA fuselage is built using carbon fiber reinforced polymer composites such as high performance titanium and aluminum. Lighter airframe materials allow the aircraft to integrate more equipment, while ensuring high payload capacity. This aircraft has a corrosion resistant mechanical parts and external aircraft cover paint.

The Lisa AKOYA aircraft is equipped with hydrofoils Seafoils (shark fins) which will facilitate operation during takeoff and landing on water. Hydrofoils will also provide better tolerance for aircraft in rough sea conditions. The less float design, the hull and the steps improve the aerodynamics and flight performance of the aircraft.

Detachable anchors and hooks allow towing and lifting for storage or to stabilize aircraft on land. This aircraft also includes a 12 V power supply for charging electronic devices. Under-fuselage is equipped with a conventional retractable landing gear.

The aircraft is equipped with folding wings that allow the aircraft to park in smaller spaces and are easily transported by trailer. The overall dimensions of the Lisa AKOYA aircraft include a length of 7 m, a height of 2.3 m and a wing width of 10.9 m. Whereas when the wings are folded, the length is 7.9 m and the width is 3.90 m.

Lisa AKOYA Engine and Performance

The Lisa AKOYA is powered by a Rotax 912ULS flat four-cylinder piston engine. The engine can produce an output power of 73.5 kW (98.6 hp) for driving a three-bladed propeller. The aircraft consumes 5.6 L of fuel without 94-octane octane or 100 LL of gasoline for every 100 km.

Lisa AKOYA aircraft can fly with a maximum speed of 250 km/ hour. The flight range is 670 nmi (1,250 km) and has a climbing rate of 7 m / s. The maximum takeoff weight (MTOW) of the aircraft is 650 kg (1,430lb) with a useful carrying capacity of up to 250 kg (550lb). This aircraft requires takeoff and landing distance of 200 m.

Lisa AKOYA Cabin and Interior

The Lisa AKOYA aircraft can accommodate two passengers in an adjoining seat configuration. The cabin offers some luggage space for storing luggage and recreational equipment. The aircraft has a unique interior design and can be adjusted to the user's taste. It features upholstery that can be adjusted in color. The color variations available include sea blue, light green, red-purple, white, and golden yellow.

Lisa AKOYA Cockpit and Avonics

The Lisa AKOYA glass cockpit is equipped with an altimeter, Mode-S transponder, air speed indicator and VHF radio with intercom. It has a length of 170 m and elbow width 130 m. It integrates with the glove compartment and side pocket within reach.

The aircraft has dual flight controls and is equipped with an electric canopy with a release system that opens and closes quickly for entry and exit. Electrical actuation from landers and surface selector gives pilots visual and audible warning to prepare for landing.

Lisa AKOYA Price

The price of Lisa AKOYA amphibious light sport aircraft is around US $ 350,000. Since the aircraft was shown at AirVenture in July 2015, Lisa Airplanes's company claims to have had about 100 orders.

Wednesday, 1 January 2020

Light Sport Aircraft

Glasair Merlin Specs, Interior, Cockpit, and Price

Admin 17:16

Glasair Merlin Specs, Interior, Cockpit, and Price – Glasair Merlin is a high-wing light sport aircraft developed by Glasair Aviation, USA. This aircraft is designed to meet LSA certification requirements based on the American Society for Testing and Materials (ASTM) standards. The aircraft was introduced in April 2014 and completed its first flight at Arlington Airport in April 2015. The flight test lasted for more than 57 minutes. This aircraft was exhibited at AirVenture Oshkosh in August 2015. Glasair Aviation plans to produce the first certified light sport aircraft in its factories in Arlington and China.

Glasair Merlin Specs

The Glasair Merlin airframe is made of an all-composite construction that integrates a high-wing layout and three-wheel landing gear. The aircraft is equipped with an optional BRS parachute system that offers additional pilot safety. This includes the configuration of the central control stick under the panel. The overall dimensions of the aircraft include a length of 6.60 m, height of 2.64 m, wingspan of 9.67 m and wingspan of 12.26 m².

Glasair Merlin Specs Engine and Performance

The Glasair Merlin aircraft is powered by a Rotax 912iS piston engine which produces around 100 hp (75 kW). The engine moves the two bladed propeller. This aircraft has a fuel capacity of 24 gal and offers a maximum speed of 222 km / h at sea level.

Glasair Merlin aircraft can fly at cruise speeds between 100 knots and 105 knots at 75% power. The aircraft kiosk speed is 80.5 km / h without flap and 73 km / h with full flap. The aircraft has an empty weight of 358 kg, a maximum takeoff weight (MTOW) of 599 kg and a useful load carrying capacity of 240 kg.

Glasair Merlin Cabin and Interior

The Glasair Merlin aircraft can accommodate two personnel consisting of a pilot and a passenger in a side by side seating configuration. The aircraft cabin has a width of 46.5 in and there is luggage space with a capacity of up to 22.6 kg. It features a skylight that brings natural light into the cabin and a fainter color to reduce brightness if the cockpit is too bright or hot.

Glasair Merlin Specs Cockpit and Avionics

The Glasair Merlin cockpit is equipped with a Dynon SkyView glass-panel avionics suite including a 10 in SV-D1000T touch screen, 10 in SV-D1000 screen, and SV-D700. The screen offers a high resolution screen and a sophisticated graphics processor to deliver visible and clear output. The cockpit includes a special autopilot control, and a dedicated button for setting the altimeter. It also comes with altitude and heading / track bugs, and a spare battery.

Other avionics include primary air data and attitude heading reference systems (ADAHRS) and additional ADAHRS, remote magnetometer, engine monitoring module, and GPS antenna / receiver. The avionics platform also includes system software, external data interfaces, mobile maps, GPS navigation software badgers, and automatic pilot systems. It also features radio communications, intercoms and graphics referenced by GEO.

Glasair Merlin is also equipped with onboard autopilot servo, SV32, SV42, and SV52 to automatically keep the aircraft slim when under autopilot control, thereby eliminating the need for pilots to move trim manually.

Glasair Merlin Price

The price of the latest Glasair Merlin light sport aircraft is around US $ 149,000. The price includes one Dynon SkyView touch screen, in addition there is also a choice of a second SkyView touch screen on autopilot for an additional $ 10,000 and a parachute, which will also add $ 10,000 to the purchase price.