Airplane Update

Sunday, 29 December 2019

Airplane Factory Sling 4 Specs, Interior, Cockpit, and Price

Admin 01:00

Airplane Factory Sling 4 Specs, Interior, Cockpit, and Price – Sling 4 is a four-seat light sport aircraft manufactured by The Airplane Factory (TAF), a South African aircraft manufacturer. This aircraft is available in kit and version ready to fly. The Sling 4 aircraft design was first introduced in 2009. The first aircraft with the EFIS Garmin G3X system was sent to Kevin Els and Thierry Plojoux & Rae Hoenderpoep in December 2014. Dean Hall received the latest version of the aircraft in August 2015.

Sling 4 Specs

The Sling 4 is an upgraded version of the two-seat Sling 2 aircraft. The fuselage is made of aluminum alloy 6061T-6. The aircraft includes strong rivets on the main spar to provide additional strength. Composite materials are used in the construction of the cover, the wing root cover and the junction between the vertical stabilizer and the fuselage, the wheel pants, and the instrument panel and canopy structure.

The Sling 4 aircraft has bubble canopies, gull wing doors, and composite landing gear that absorbs pressure on a regular basis. The aircraft is also equipped with a complete airframe emergency parachute for added safety. The dimensions of the aircraft include an overall length of 7.1 m, height of 2.45 m, wingspan of 9.96 m, wing surface area of 12.4 m² and a body length of 6.17 m. The aircraft's take-off and landing distance are 213 m and 152 m, respectively.

Sling 4 Engine and Performance

The Sling 4 aircraft is powered by a Rotax 914 UL turbo charged engine manufactured by Bombardier-Rotax. The engine produces an output power of 84.5 kW (115 hp) at 5,800 rpm to drive the Airmaster 3-Bladed Constant Speed propeller. The aircraft is equipped with two fuel tanks that offer a maximum fuel capacity of 185 l integrated in both wings.

Sling 4 aircraft can fly with a maximum speed of 250 km / h and a cruising speed of 240 km / h. The maximum range of the aircraft is 780 nmi. The aircraft can rise to a maximum operating height of 15,000 ft at a rate of 750 fpm. The standard empty weight and maximum aircraft takeoff weight are 470 kg and 920 kg, respectively. The aircraft has a useful load carrying capacity of 450 kg.

Sling 4 Cockpit and Avionics

Sling 4 aircraft are equipped with a 44 in wide glass cockpit from MGL Avionics with complete flight data, engine monitoring and GPS. It features nine screens completely user-programmed with PC-based editing software. The cockpit also features coordinated and very responsive controls. The cockpit displays the Garmin G3 primary avionics, while the secondary avionics includes instruments and configurable items such as traditional analog calls, bar graphs, digital readings, horizons and moving maps.

The avionics suite of the Sling 4 aircraft also includes a mobile GPS map, map display, terrain warning and voice confirmation in addition to visual and external alarms. It further includes a weight and balance calculator, flight and machine recording facilities for key flight data, and flight logs which can be downloaded using an SD / MMC card.

Sling 4 Cabin and Interior

The wide Sling 4 aircraft cabin can accommodate four passengers and can carry luggage weighing up to 40 kg. The nicely appointed cabin interior offers four-seat executive comfort. The cabin is shrouded in genuine leather and luxurious carpet that stands out to add elegance and a touch of class. The cabin interior is available in five color palettes namely Cast Iron, Red Velvet, Indigo Sky, Namib Dune and Cloud Burst with stitches, piping, and panels in complementary colors.

Sling 4 Price

The price of the latest Sling 4 light sport aircraft is around US $ 190,000. Prices include engines, parachute fuselage, propeller and MGL avionics. Prices are subject to change according to the kit chosen and demand time to work.

Friday, 27 December 2019

Light Sport Aircraft

Atol 650 Specs, Cockpit, Engine, and Price

Admin 01:00

Atol 650 Specs, Cockpit, Engine, and Price – Atol 650 is an amphibious light sport aircraft (LSA) designed and developed by Atol Avion Ltd. This aircraft is capable of operating in water, land and snow. This aircraft completed its maiden flight in April 2015. The LSA underwent a water transport test for the first time in December 2014. The LSA was exhibited for the first time at the Sodankylä Airshow in June 2015 and was also displayed at the Aero 2015 exhibition in Germany.

Atol 650 amphibious light sport aircraft

Atol 650 Specs

The Atol 650 fuselage is made of modern composite wood. The dimensions of the aircraft include a length of 7.45 m, a wingspan of 9 m, a wingspan of 13.5 m², and a tail span of 2.4 m. It features a conventional landing gear that can be pulled back during flight and water operations. It also includes an auxiliary nose wheel which helps in sliding to steep beaches. The aircraft can be equipped with an Atol water taxi (AWTS) system for water maneuvers.

Atol 650 aircraft have a wing folding system with a manual control line connection. Wing aspect ratio ensures center of gravity (CG) range and ease of loading without strict loading restrictions. The wing tips are positioned at the top of the fuselage to ensure safe operation on water, while the dihedral wing further ensures good roll stability. The aircraft can be optionally equipped with skis to operate in the snow during winter.

The amphibious aircraft is also equipped with a bilge pump, a bulkhead in the rear body to prevent the uncontrolled hull water from moving, aft cleats, and mooring poles in additional buoy supporters and tails. It also integrates luggage compartment, and integrated water steering in the tail wheel, as well as paddles and fasteners. The aircraft's empty weight is 375 kg, the maximum take-off weight (MTOW) is 650 kg, and the maximum load carrying capacity is 275 kg. this aircraft weighs 100 kg lighter than other LSA that is currently available on the market.

Atol 650 Engine

Atol 650 amphibious aircraft is powered by a Rotax 912iS engine which can produce outout power of 100 bhp. The engine drives a fixed three-blades propeller with a height of 1,720 mm. This aircraft has a fuel capacity of 140 liters which provides nine hours of endurance. The aircraft can fly with a cruise speed of 170 km / h and a strike speed of 74 km / h. It has a maximum range of 1,500 km (950 mi).

Atol 650 Cockpit and Avionics

Atol 650 aircraft can accommodate pilots and passengers in side-by-side seat configurations. Each seat has a four-point seat belt and a shoulder strap. The cockpit is equipped with fabric or leather upholstery. It was covered by a rear hinged canopy that rose with an instrument panel. Canopies allow occupants to enter or exit planes on the beach with dry feet. This includes emergency canopy releases and can be locked from the outside.

The Atol 650 avionics suite includes a 7 in MGL screen, a 4.3 in MGL XTreme engine monitoring system, dual controls and dual brake pedals. The cockpit is also equipped with a fresh air nozzle, installed for iPad, electrical sockets on the instrument and top panel, electric trim, and heating and defogging systems.

Atol 650 Price

The price of the latest Atol 650 amphibious light sport aircraft (LSA) is around US $ 179,000.

Wednesday, 25 December 2019

Light Sport Aircraft

Lambert Mission M108 Specs, Engine, Cockpit, and Price

Admin 01:00

Lambert Mission M108 Specs, Engine, Cockpit, and Price – Mission M108 is a two-seats light sport aircraft manufactured by Lambert Aircraft Engineering, an aircraft manufacturing company based in Belgium. The aircraft's first flight test was conducted at the Kortrijk-Wevelgem airfield in May 2014. After completing eight months of testing and evaluation phases by the Department of Light Aircraft Association (LAA) British Civil Aviation Authority, the aircraft finally received a type certification and full permission to fly in January 2015,

Lambert Mission M108 light sport aircraft

Lambert Mission M108 Specs

The Mission M108 fuselage is built using strong tubes. The fuselage has a standard emergency parachute feature and is produced in two versions namely the nozzle and tail dragger. This aircraft has wings that can be folded in less than five minutes by one person. It can operate from a very short agricultural strip (STOL) and includes a steering wheel that can be controlled.

The dimensions of the Mission M108 aircraft include a length of 6.10 m and a height of 2.15 m for the tail dragger version, while the nosewheel version is 1.95 m in height. The wingspan of the aircraft in the folded position is 2.60 m and in the open position 9.32 m. The aircraft has a wingspan of 11.8 m², a tail span of 2.40 m, and a wheelbase of 1.75 m.

Lambert Mission M108 Engine and Performance

The Lambert Mission M108 is powered by a single Rotax 912iS engine that produces an output power of 73 kW (100 hp) at 5,800 rpm. It has an engine displacement of 1,352 cm³. The aircraft's fuel capacity is 78 liters for the standard version and 110 liters for the remote version. Fuel consumption range is 12-15 liters/ h.

Mission M108 aircraft can fly with a maximum cruise speed of 170 km/ h, kiosk speeds of 72 km/ h, and speeds never exceed 222 km/ h. The maximum range of the aircraft is 460 nm (850 km) with a climbing rate of 4.75 m/ s. The aircraft requires takeoff and takeoff distances between 80 m and 130 m.

Lambert Mission M108 Cockpit and Avionics

The Lambert Mission M108 aircraft has a standard glass cockpit that offers good visibility. The cockpit is equipped with the Garmin G3X flight display system with 7 "dual display configuration and avionics standards including audio panel and intercom, PS Engineering PMA4000, GPS / nav / com, GPS / com or GPS, Garmin GTN650, GTN635 or GTN625, S transponder mode, and GTX23ES Avionics further includes easy flying, full dual control with individual control sticks, hydraulic brakes, and manual flaps for take-off and short landing.

Optional equipment that can be installed on the Mission M108 aircraft includes the standby air speed indicator and altimeter, LX BU57, standby magnetic compass, SIRS NV2A, backup attitude indicator, RC Allen RCA2600-2 radio, Garmin GTR225A or GNC255A VHF radio, remote measuring equipment DME), and the Garmin G3X autopilot is integrated with the GMC305 mode controller. The aircraft can also be equipped with the Garrecht TRX-1500 or the Garmin GTS800 traffic avoidance system, L-3 Avionics WX-500 Stormscope, and the Garmin Flight Stream 210 wireless interface.

Lambert Mission M108 Cabin and Interior

The Mission M108 aircraft can accommodate two passengers with adjustable seats. The cabin has a width of 1.08 m, and includes a large luggage space with a capacity of up to 40 kg. It is equipped with two hinge doors to the top for access to the cabin. The aircraft has an empty weight ranging from 330 kg and 350 kg, and a maximum take-off weight of 600 kg.

Lambert Mission M108 Price

The price of the latest Lambert Mission M108 light sport aircraft is around US $ 50,000 to 60,000.

Monday, 23 December 2019

Searey

Searey Elite Specs, Cockpit, Range, and Price

Admin 01:00

Searey Elite Specs, Cockpit, Range, and Price – Searey Elite is a amphibian light sport aircraft designed and manufactured by Progressive Aerodyne Inc SeaRey. This aircraft was launched in Tavares, Florida in January 2014. This is a development version of its predecessor Searey aircraft that first flew in November 1992. Searey Elite aircraft received airworthiness certification from the Federal Aviation Administration (FAA) in December 2013. Currently being produced at the Progressive Aerodyne facility in Tavares, Florida.

Searey Elite amphibian light sport aircraft

Searey Elite Specs

Searey Elite aircraft have sophisticated hulls made of carbon fiber. It was also equipped with a Lexan windshield optical shield, and high wings with a tail dragger. The wings of the plane are swept back on the leading edge with straight ends to form tapered wings. This aircraft has a landing gear that can be pulled to allow a smooth landing on a grass runway that has not even been repaired. The aircraft's tail wheels ensure safer takeoff and landing on crossings.

The dimensions of the Searey Elite aircraft include a length of 6.8 m, height of 2 m, and wingspan of 9.4 m. The wing area and range of the main wheels are 14.7 m² and 2.34 m, respectively. aircrafts have an empty weight of 449 kg and a maximum gross weight of 649 kg, and can carry a load of 200 kg. Airplane takeoff rollers on land are 81.7 m and landing roll on the surface is 99 m. Takeoff/ landing rollers on water measuring 107 m.

Searey Elite Engine and Performance

The Searey Elite is powered by a Rotax 914 ULS engine that produces power of 115 hp (86 kW). The engine is mounted above the wing, which is supported above the fuselage by a vertical pole. The engine drives a composite three-bladed propeller and has a 2,000 hour overhaul (TBO). The aircraft is also equipped with an electric main fuel pump, a backup fuel pump and a 12 V battery.

Searey Elite can fly with a maximum cruise speed of 169 km/ h and a normal cruise speed of 158 km/ h with 75% power. It has a service ceiling of 5,486 m and can rise at a rate of 5.6 m/ s at sea level. The aircraft has a maximum range of 610 km with 30 minutes of fuel reserves.

Searey Elite Cabin and Interior

Searey Elite aircraft have a spacious cabin with two side-by-side configurations. The cabin has a width of 1.1 m and a height of 0.89 m. The cabin is equipped with a luggage compartment that offers a payload volume of 13 ft³. Baggage compartment has the capacity to carry 23 kg of cargo. The cabin can be accessed through individual double sliding canopies that can be opened or closed during flights.

Searey Elite Cockpit and Avionics

Searey Elite aircraft have an ergonomic cockpit with 112 cm wide elbow room. The cockpit is equipped with comfortable and soft seats. The electronic flight instrument system (EFIS) of the avionics suite includes warning for gear, warning angle of attack, and low fuel warning with audio and visual output. The aircraft is also equipped with a Garmin GTX 327 transponder, Garmin 696 GPS system, electric trim lifts, electric hull pumps, and drain plugs. The instrument panel and cockpit can be adjusted according to customer requirements.

Searey Elite Price

The price of the latest Searey Elite amphibian light sport aircraft is around US $ 169,000.

Saturday, 21 December 2019

TL Ultralight

TL-3000 Sirius Specs, Interior, Cockpit, and Price

Admin 01:00

TL-3000 Sirius Specs, Interior, Cockpit, and Price – The TL-3000 Sirius is a two-seat light sport aircraft manufactured by TL Ultralight based in the Czech Republic. This aircraft is designed to be suitable for flight schools and is available in the European ultra-light category and the US light sport aircraft (LSA). The first flight test flight was completed in May 2008 and production began in 2010. In April 2016, TL Ultralight launched the TL-3000 Sirius aircraft variant equipped with an aerial camera mounted under the fuselage.

TL-3000 Sirius Specs

The TL-3000 Sirius aircraft has a high wing design and is constructed with a composite reinforced epoxy structure. These include rectangular wings with a trapezoid-shaped outside. The landing gear wheel has a nose wheel that can be controlled and a main wheel with brakes. It comes equipped with fixed horizontal and vertical stabilizers, effective flaps, and strong elevator, steering and aileron surfaces.

The GRP fiberglass used on the landing gear reduces the impact and makes the aircraft hold back if the landing is hard. This aircraft has a low vibration and a very low noise level of 58 dBA. Dimensions of the TL-3000 Sirius aircraft include a length of 6.97 m, a height of 2.30 m, and a wingspan of 9.4 m. The aircraft has a wing area of 11.26 m², a horizontal tail area of 2.68 m², a vertical tail area of 1.45 m², and a horizontal tail width of 2 m.

TL-3000 Sirius Engine and Performance

The TL-3000 Sirius can be powered by Rotax 912ULS (80 hp), 912iS (100 hp) or 914 Turbo (115 hp) four-cylinder and four-stroke engines. The engine drives a PowerMax 3 blades constant speed blades. The aircraft fuel tank capacity is 90 l, while the fuel consumption of the aircraft is 16.2 l / hr. This aircraft has flight resistance for 6 to 7 hours.

TL-3000 Sirius aircraft can fly with cruise speeds between 180 km / h and 220 km / h, while speeds never exceeded are 253 km / h and a minimum speed of 59 km / h. The maximum range of the aircraft is 2,000 km / h and the climbing rate is 5 m / s. This aircraft has an empty weight of 297 kg and a maximum take-off weight (MTOW) of 472.5 kg. It can carry a minimum crew weight of 60 kg, a maximum crew weight of 180 kg and a maximum luggage weight of up to 25 kg.

TL-3000 Sirius Cockpit and Avionics

The TL-3000 Sirius aircraft cockpit features the Garmin G3X Touch with a high-resolution touch screen display. The instrument panel display has a bright color that can be easily seen even in direct sunlight. The spacious glass cockpit offers ample space for pilots and passengers. The avionics suite includes 3D viewing of the outside area, mapping options and surrounding traffic information. It also includes double yoke controls for ailerons and elevators, and electric flaps. This aircraft combines the characteristics of high-performance and obedient flight, and agile and maneuver control features.

TL-3000 Sirius Cabin and Interior

The TL-3000 Sirius aircraft accommodates two passengers in side-by-side seating positions. The interior of the cabin is furnished with two body-contoured deluxe soft seats. The 1.13 m wide cab has an upward opening door, which is held with hydraulic supports. The cabin includes a large luggage compartment with a cargo volume of more than 14 ft³.

TL-3000 Sirius Price and Orders

The price of the latest TL-3000 Sirius light sport aircraft is around US $ 120,000. At present, more than 100 TL-3000 Sirius aircraft have been sent to various operators in various countries in Europe and the United States.

Thursday, 19 December 2019

Sonex

Sonex Waiex-B Specs, Engine, Cockpit, and Price

Admin 01:00

Sonex Waiex-B Specs, Engine, Cockpit, and Price – The Sonex Waiex-B is a light sport aircraft manufactured by Sonex Aircraft, a company that manufactures aircraft kits from the United States. The turbo-powered Waiex-B aircraft design was first introduced at the Sun 'n Fun show in Lakeland, Florida in April 2016. The aircraft is available in tail dragger and tricycle configuration for the aircraft manufacturing market itself.

Sonex Waiex-B Specs

The Sonex Waiex-B fuselage was built with aluminum material. The aircraft design creates expanded space by aligning the sides of the fuselage forward. Offers comfort including extra width on the shoulders, hips, knees and legs. It also features a new seating geometry that is suitable for taller individuals.

The aircraft includes spar wing assemblies, engine angle components, and Y-tails. It was upgraded to include AeroBrake hydraulic brakes and a new universal cover feature designed to fit many popular engine options. The dimensions of the Sonex Waiex-B aircraft as a whole cover a length of 18 ft, a wing span of 22 ft and a wingspan of 98 ft². The height of the standard gear tail is 51 in, while the tail gear height is 69 in. The main tooth width is 71 in and the tail width is 88 in.

Sonex Waiex-B Engine and Performance

The Sonex Waiex-B aircraft is powered by a 2,180 cc AeroVee turbo engine that can produce a power output of 80 hp. It can be equipped with four engine installation options including AeroVee / AeroVee Turbo, Jabiru / CAMit 3300, UL-350 series and Rotax 912 series. This aircraft has a fuel capacity of 20 US gallons.

Sonex Waiex-B aircraft can fly with a cruise speed of 210 km/ h and a kiosk speed of 64 km/ h, while the maneuver speed is 201 km/ h. The aircraft has a maximum range of 550 miles, a service ceiling of 16,000 ft and climbing speeds between 500 fpm and 900 fpm. The empty weight and gross weight of the aircraft are 620 lb and 1,100 lb, respectively. It has a useful carrying capacity of 480 lb and requires a landing distance of 500 ft and a landing distance of 400 ft.

Sonex Waiex-B Cockpit and Avionics

The Sonex Waiex-B aircraft features an increase in cockpit space. The cockpit is 40 in at shoulder width and 38 in at hip. It has a height of 37 in from under the seat to the canopy. Height from floor to chair 9 in, seat height to instrument panel 13 in, and seat height to 17 in. The bottom length of the seat is 23 in. And the length of the steering pedal to the front of the seat is 18.5 in. This aircraft has a glass canopy and can carry luggage with a maximum weight of up to 18.2 kg.

The Sonex Waiex-B aircraft is equipped with the Avionics 8.5 in MGL Avionics iEFIS Explorer dual-screen avionics suite. It also includes a Dynon SkyView dual screen fast panel with integrated flight control system modules. It has a Y-stick center that offers dual controls, and an electric cover that reduces cockpit clutter. Avionics includes a dual throttle quadrant, AeroConversions trim system, ABS cockpit side panels, and cable and pushrod fairing.

Sonex Waiex-B Price

The price of the latest Sonex Waiex-B light sport aircraft is around US $ 37,814 with a standard kit. Prices may change according to the chosen engine and landing gear type.

Tuesday, 17 December 2019

Sonaca

Sonaca 200 Specs, Interior, Cockpit, and Price

Admin 01:00

Sonaca 200 Specs, Interior, Cockpit, and Price – The Sonaca 200 is a two-seat light sport aircraft designed by Sonaca Aircraft based in Belgium for pilot training and relaxed flight. This aircraft was first introduced at the Aero Friedrichshafen event in April 2016. It became the first aircraft to be assembled in Belgium and designed for the general aviation market, especially in the European region. The Sonaca 200 aircraft has obtained the European Aviation Safety Agency (EASA) type certificate in June 2018. In addition to obtaining type certification, the aircraft has also obtained a Design Organization Approval (DOA) and Production Organizations Approvals (POA) certification.

Sonaca 200 Specs

The Sonaca 200 fuselage is built with an aluminum structure that resists half-stress corrosion. The fuselage, wings and tail of the aircraft are built using aluminum alloy. The aircraft wing is equipped with an electric perforated cover and a balanced pushrod aileron. Excellent spotlights, navigation and landing are mounted on both wings to increase visibility in adverse conditions. These winglets have an elliptical shape that is optimized to reduce aerodynamic drag. The overall dimensions of the aircraft include a length of 7 m and a wing width of 9.15 m.

The Sonaca 200 aircraft integrates a conventional tail with balanced horn and elevator stabilizers for flutter prevention. The aircraft is equipped with steerable nose wheels and can be controlled as long as the cab on any surface can avoid the initial wear of the brakes. The main landing gear has glass fiber with strong shock absorption, and is designed for use on unprepared runways and grass. This aircraft has a sharp engine cover design to maximize propeller efficiency. The aircraft's structure is repaired with rivets, which include inspection panels that can be easily removed for maintenance.

Sonaca 200 Engine and Performance

The Sonaca 200 is powered by a four-cylinder, four-stroke Rotax 914F engine liquid / air-cooled with an opposite cylinder. The engine can produce an output power of 115 hp. The engine drives a Duc Hélices 3-blades fixed pitch propeller. The engine provides short takeoff performance, high climb rates at high altitudes, as well as safe cruising speeds for long trips. It offers 2,000 hours of overhaul (TBO).

The aircraft is equipped with two fuel tanks on the aircraft wings with a total capacity of 140 l. The type of fuel used can be avgas or mogas. The Sonaca 200 can fly with a maximum cruise speed of 115 knots and a stall speed of 45 knots. It has a range of 750 nm and a climbing rate of 750 ft per minute (fpm). The aircraft's empty weight is 480 kg and the maximum take-off weight (MTOW) is 750 kg. It can take a useful payload of 320 kg and requires a 350 m take-off distance and a 300 m landing distance.

Sonaca 200 Cockpit and Avionics

The cockpit of the Sonaca 200 aircraft is fully equipped with VFR for night flights even in bad weather conditions. The cockpit dashboard displays modern instrumentation such as a digital engine monitoring system, artificial horizons and navigation aids. Avionics also includes standard analog instrumentation and foot brakes. In addition, the Garmin G500 TXI glass cockpit instrument is also available with an all digital instrument panel, this is equipped with a certified Garmin GTN 650 GPS system.

Sonaca 200 Cabin and Interior

The large cabin of the Sonaca 200 aircraft can accommodate two passengers. The cabin interior includes leather upholstered seats and hand-stitched dashboard. The luggage compartment is located behind the seat and can hold up to 35 kg in weight. The cabin is covered with a large bubble canopy mounted on two sliding tracks to increase passenger visibility. Equipped with acoustic foam for low noise levels when flying. The cabin also includes a wide area of footwear and footpaths, which allows easy access on board.

Sonaca 200 Price and Orders

The price of a light sport aircraft Sonaca 200 standard analog cockpit version is US $ 202,000, while the glass cockpit version is $ 237,000. Sonaca Aircraft company received 14 pre-orders for Sonaca 200 aircraft from European customers, including eight from the Belgian New CAG Air Academy, and two each from Aeroclub Tissandier of France, London UK Flight Training, and FFL Flugschule am Flughafen Essen / Mülheim from Germany .

Sunday, 15 December 2019

Light Sport Aircraft

Evektor SportStar RTC Specs, Interior, Cockpit, and Price

Admin 01:00

Evektor SportStar RTC Specs, Interior, Cockpit, and Price – SportStar RTC is a two-seat light sport aircraft manufactured by Evektor-Aerotechnik based in the Czech Republic. This aircraft can be used in a variety of operations including private, corporate transportation, as well as basic and advanced pilot training at flight schools. The aircraft received type certification from the European Aviation Safety Agency (EASA) in May 2012. Evektor appointed Cosmik Aviation as the new dealer for SportStar RTC aircraft in the UK in April 2013.

Evektor SportStar RTC light sport aircraft

Evektor SportStar RTC Specs

The SportStar RTC aircraft was designed based on the Harmony Evektor training aircraft, which was introduced in 2005. It features anodised metal fuselage and corrosion resistance to provide higher durability. The aircraft features a tricycle-type landing gear with steering pedals and steerable nose wheels. The overall dimensions of the aircraft include a length of 5.98 m, height of 2.48 m, and wingspan of 8.65 m. All joints of the plane are fixed and bound. The aircraft's empty weight is 310 kg and its maximum take-off weight is 600 kg.

Evektor SportStar RTC Engine and Performance

The Evektor SportStar RTC is powered by a Rotax 912 ULS engine that can produce a power output of 100 hp. The engine drives the Woodcomp Klassic 1700/3/R propeller with three blades. The machine has a 2,000 hour overhaul (TBO). The aircraft is equipped with a fuel tank with a maximum capacity of 120 liters. The average fuel consumption of the aircraft is 15 liters per hour. The aircraft can fly with a maximum cruise speed of 200 km / h and a range of 1,300 km (700 nm). It has a service ceiling of 4,720 m.

Evektor SportStar RTC Cockpit and Avionics

The SportStar RTC cockpit is equipped with a Garmin G3X Touch or Dynon SkyView 10. instrument panel. It features 200 NAV / COMM channels with VOR / localiser and glideslope receivers, as well as reverse search frequencies supported by airport IDs that can automatically decode station code identifiers. Morse. This also includes a 2-place intercom. The aircraft is also equipped with 8.33 kHz channel spacing, which is required to fulfill the new Sky Europe Single mandate.

The avionics suite on the SportStar RTC aircraft includes turn and bank indicators, RCA 26AK-made horizons, RCA directional gyro 15AK-1, SIRS compass, digital flight clock, and dual control sticks. It features dual hydraulic brakes, standard flight instruments such as air speed indicators, altimeters and variometers. Other control systems on the aircraft include electric trim with dual control switches and trim position indicators, kiosk speed warning systems, and longitudinal, lateral, throttle controls with friction locks. It also includes a combined start switch, push-button circuitry bracket, and avionics master switch.

Evektor SportStar RTC Cabin and Interior

The cabin of the SportStar RTC aircraft has a shoulder room of 1.18 m. It also features a 360 ° view glass cockpit to enhance passenger visibility and provide perfect situational awareness. It has a luggage compartment with a volume of 10.1 ft³. The aircraft can accommodate luggage with a maximum weight of 25 kg. The cabin is equipped with a seat for pilots and co-pilots, with standard seats with low backrest, and side ventilation windows. It also comes with blinds that Koger can pull.

Evektor SportStar RTC Price and Orders

The price of the latest SportStar RTC light sport Evektor aircraft is around US $ 120,000. Evektor received large requests from customers from four flight shows conducted in Europe, including Tannkosh air shows in Germany, ULM Salon Blois in France, LAA Rally in England and MAKS air shows in Russia. The first SportStar RTC aircraft was sent to Aero4You, based in France in August 2013. The second aircraft will be sent to the Aeroclub Schweighofen flight training organization in Germany.

Friday, 13 December 2019

Skycraft

Skycraft SD-1 Minisport Specs, Cockpit, and Price

Admin 01:00

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 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 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 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

Privateer Amphibian Specs, Interior, Cockpit, and Price

Admin 01:00

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 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 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 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

Light Sport Aircraft

Kolb Flyer Super Sport Specs, Cockpit, and Price

Admin 01:00

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 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 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

Van's Aircraft

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

Admin 01:00

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 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 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 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

Van's Aircraft

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

Admin 01:00

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 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 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 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

Van's Aircraft

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

Admin 01:00

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 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 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 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 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

Tecnam P2010 Specs, Interior, Cockpit, and Price

Admin 01:00

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 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 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 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.