Monday, 9 December 2019

Kolb Flyer Super Sport Specs, Cockpit, and Price

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

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

Kolb Flyer SS Light Sport Aircraft

Kolb Flyer Super Sport Specs

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

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

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

Kolb Flyer Super Sport Engine and Performance

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

Kolb Flyer SS Cockpit

Kolb Flyer Super Sport Cabin and Cockpit

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

Kolb Flyer Super Sport Price

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

Saturday, 7 December 2019

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

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

Vans RV-14 light sport aircraft

Vans RV-14 Specs

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

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

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

Vans RV-14 specs

Vans RV-14 Engine and Performance

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

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

Vans RV-14 Cockpit and Avionics

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

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

Vans RV-14 interior

Vans RV-14 Cabin and Interior

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

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

Vans RV-14 Price

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

Thursday, 5 December 2019

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

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

Vans RV-12 light sport aircraft

Vans RV-12 Specs

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

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

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

Vans RV-12 engine

Vans RV-12 Engine and Performance

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

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

Vans RV-12 cockpit

Vans RV-12 Cockpit and Avionics

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

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

Vans RV-12 Cabin and Interior

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

Vans RV-12 Price

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

Tuesday, 3 December 2019

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

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

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

Vans RV-10 light sport aircraft

Vans RV-10 Specs

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

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

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

Vans RV-10 engine

Vans RV-10 Engine and Performance

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

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

Vans RV-10 interior

Vans RV-10 Cabin and Interior

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

Vans RV-10 cockpit

Vans RV-10 Cockpit and Avionics

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

Vans RV-10 Price and Orders

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

Sunday, 1 December 2019

Tecnam P2010 Specs, Interior, Cockpit, and Price

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

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

Tecnam P2010 light aircraft

Tecnam P2010 Specs

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

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

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

Tecnam P2010 Engine and Performance

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

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

Tecnam P2010 cockpit

Tecnam P2010 Cockpit and Avionics

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

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

Tecnam P2010 interior

Tecnam P2010 Cabin and Interior

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

Tecnam P2010 Price and Orders

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

Friday, 29 November 2019

Czech Sport Aircraft PS-28 Cruiser Specs, Cockpit, and Price

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Czech Sport Aircraft PS-28 Cruiser Specs, Cockpit, and Price – The PS-28 Cruiser is a two-seat low-wing lightweight sport aircraft developed by Czech Sport Aircraft. This aircraft can be used for basic and advanced flight training, air clubs, basic military pilot training, general recreational use, and air tourism. The PS-28 Cruiser aircraft obtained type certification from the European Aviation Safety Agency (EASA) in April 2012 in the category of lightweight sport aircraft and entered service in October 2012. This aircraft is available in Classic, Style and Exclusive models.

Czech Sport Aircraft PS-28 Cruiser

PS-28 Cruiser Specs

The PS-28 Cruiser has an all-metal airframe design, conventional cantilevered wings and tail. The aircraft is equipped with a fixed tricycle type landing gear with hydraulic brake support. The main undercarriage is attached directly to the bottom of the fuselage and the nose landing gear is attached to the firewall.

The aircraft tail unit consists of vertical fins, steering, horizontal stabilizers and lifts with trim tabs. This elevator is balanced with electrically controlled elevator lifts. The lift is also equipped with a balance tab for better control and balance.

The wings are equipped with electrically controlled flaps and ailerons. The right aileron is equipped with an electric trim. Each wing is held with six bolts in the center of the wing. The wing tips are made of carbon-glass composite and are equipped with spotlights.

This aircraft can accommodate 2 passengers who double as pilots. The aircraft's interior includes two seats mounted side by side. Leather seat seats will increase passenger comfort when flying.

The dimensions of the PS-28 Cruiser aircraft include a length of 6.62 m, a height of 2.31 m, and a wingspan of 8.6 m. The aircraft's wing surface area is 12.3 m². The aircraft has two luggage storage compartments located in each wing with a capacity of 10 kg each. Other luggage storage compartments are also available at the back of the seat with a capacity of 18 kg.

PS-28 Cruiser specs

PS-28 Cruiser Engine and Performance

The PS-28 Cruiser is powered by a Rotax 912 ULS2 / S2 engine that can produce an output power of 73.5 kW. The engine drives the Sensenich Fixed 3-blade propeller. The aircraft is equipped with fuel tanks with a total capacity of 114 l.

Rotax 912 engine support allows the PS-28 Cruiser to fly a maximum cruise speed of 172 km / h and a horizontal speed of 220 km / h. The aircraft has a climbing speed of 4.2 m / s and a range of 512 nm (948 km). This aircraft consumes fuel around 17.5 l / h and has a durability of 5 hours and 26 minutes.

PS-28 Cruiser requires a take-off distance of 387 m on the concrete surface and 457 m on the surface of the grass. Meanwhile, landing a plane requires a distance of 362 m on the concrete surface and 338 m of grass.

PS-28 Cruiser cockpit

PS-28 Cruiser Cockpit and Avionics

The aircraft has a large glass fiber cockpit that is equipped with a main Dynon D-100 flight data display and a Dynon D-120 engine monitoring system. A large cockpit glass cover will provide perfect visibility for the pilot. Flight controls such as wheel brakes are located on the pedals and throttles are located on the center console in the cockpit.

The cockpit of the PS-28 Cruiser is equipped with a modern and sophisticated avionics system, such as a magnetic compass, a backup air speed indicator, and a navigation / communication radio. Other avionics suites include the HS-34 navigation extension module, S mode transponders and class 2 intercoms, and the Garmin 695 GPS.

PS-28 Cruiser Price and Orders

The price of the latest light sport aircraft PS-28 Cruiser is around US $ 140.000. Czech Sport Aircraft received orders for two PS-28 Cruiser aircraft to be sent to France in March 2013. Eindhoven Aero Club ordered the delivery of two aircraft in January 2014. To date, Czech Sport Aircraft has sent more than 500 aircraft to various operators around the world.

Wednesday, 27 November 2019

Tecnam P2002 Sierra MkII Specs, Cockpit, and Price

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Tecnam P2002 Sierra MkII Specs, Cockpit, and Price – Tecnam P2002 Sierra MkII is a single-engine, low-wing light sport aircraft (LSA) manufactured Tecnam, based in Italy. This aircraft was first introduced in December 2016, this is the latest and second generation version of the previous aircraft. The P2002 Sierra MkII aircraft was developed by offering an enhanced cabin for greater comfort, top-level avionics, new paint colors and interior options. Most of the operators of these aircraft are individuals and flight schools.

Tecnam P2002 Sierra MkII

Tecnam P2002 Sierra MkII Specs

The Tecnam P2002 Sierra MkII fuselage is made of lightweight metal with a corrosion resistant epoxy coating. The aircraft's wings are manufactured using light alloys combined with a single spar and a full metal torque box. The front edge of the wing can be removed to be fixed and adjusted to the fuel tank. The aircraft has exterior dimensions which include a length of 6.74 m, height of 2.4 m, wingspan 8.56 m, and wingspan of 11.5 m².

Tecnam P2002 Sierra MkII is equipped with the aircraft's main landing gear built with lightweight alloy springs, which can land on non-upgraded landing lanes. This aircraft has a trailing nose wheel that is integrated with a rubber shock absorber system. The horizontal stabilizer tail design offers loose hands stability with minimum resistance.

This aircraft has an empty weight of 367 kg and a maximum take-off weight of 600 kg, and can carry a useful maximum load of up to 233 kg. The aircraft needed 262 m for take-off and 170 m for landing landing. The take-off and landing distance are 434 m and 333 m, respectively.

Tecnam P2002 Sierra MkII Engine and Performance

Tecnam P2002 Sierra MkII is powered by a Rotax 912ULS2 engine that can produce around 98 hp. The engine moves the fixed bladed pitch propeller developed by Sensenich. This aircraft has two fuel tanks located on the wings with a capacity of 55 l each. The aircraft uses mogas and avgas fuels and consumes around 17 l of fuel per hour.

Tecnam P2002 Sierra MkII aircraft can fly with a maximum cruise speed of 204km/ hour and a maximum speed of 222 km/ hour. The maximum range that can be traveled by aircraft is 642 nm. The aircraft has a service ceiling of 15,000 ft (4,572 m) and climbing speed of 4.06 m/ s.

Tecnam P2002 Sierra MkII cockpit

Tecnam P2002 Sierra MkII Cockpit and Avionics

The Tecnam P2002 Sierra MkII cockpit has a redesigned sliding canopy with more headroom to increase visibility to 360 °. This aircraft can be equipped with a variety of flight instruments including basic analog instruments for visual flight, analog six packages with Garmin GPS, Dynon SkyView with two 10 in screens, Garmin G3X with two 10.6 in screens, and the G3X night version with fully back up instrumentation backlights.

Avionics equipment includes the Garmin GMA 240 audio panel, the Garmin GTR 200 COM, the Garmin GTX 327 transponder, the Garmin XM version of the GPS, and the antenna. The aircraft has flight control equipment including hydraulic foot brake, parking brake, electric flap, dual flight control, adjustable nose wheel, electric stabilizer trim and engine control. It also includes a central quadrant with a single throttle lever, fuel control selector, and chokes.

The standard electrical system installed on the P2002 Sierra MkII aircraft includes a 7 Amp Alliant battery, 14 V alternator, ACS starter key, split starter, and switch. Also included is a circuit breaker panel, 12V socket, and warning lights.

Tecnam P2002 Sierra MkII specs

Tecnam P2002 Sierra MkII Cabin and Interior

The Tecnam P2002 Sierra MkII cabin can accommodate two passengers in an adjoining seat, with one passenger double as a pilot. The cabin is 0.95 m high, 1.11 m wide, and has a luggage compartment that can carry up to 20 kg of luggage. The cabin is equipped with leather interior and new seat rails, the operator can also choose the seat model to use.

Tecnam P2002 Sierra MkII Price

The price of the latest Tecnam P2002 Sierra MkII light sport aircraft is around US $ 150,000 to $ 160,000. This price is very dependent on the selected avionics package.

Monday, 25 November 2019

Tecnam Astore Specs, Interior, Cockpit, and Price

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Tecnam Astore Specs, Interior, Cockpit, and Price – Tecnam Astore is a luxurious two-seat light sport aircraft developed by Tecnam, an aeronautical manufacturer in Italy. This aircraft was launched at AERO Friedrichshafen in Germany in March 2013. This aircraft can be operated as private transportation and public transportation. The first production aircraft was named the P48 Astore.

Tecnam Astore made its first flight in June 2013 and has obtained FAR part 23 certification from the Federal Aviation Administration (FAA) and has also received type certification from New Zealand and Australia.

Tecnam Astore light sport aircraft

Tecnam Astore Specs

The Astore fuselage is built with all-metal material and carbon or glass fiber reinforced matrices for upper radome and fairing. It is also coated with anti-corrosion epoxy to make it resistant to bad weather and prolong aircraft life. This aircraft has wings mounted low on the fuselage. The overall dimensions of the aircraft include a length of 7 m, a height of 2.3 m, and a wingspan of 8.65 m. The wingspan of the aircraft is 12.2 m².

Tecnam Astore has a horizontal tail including stabilizer and lift with tip balancing horns. The aircraft is equipped with a landing gear tricycle which is equipped with two 7075T6 lightweight alloy springs. The nose of the aircraft is equipped with oleo-pneumatic shock absorbers that are connected to the firewall. This aircraft has an empty weight of 367 kg, a maximum takeoff weight of 600 kg, and a useful loading capacity of 233 kg.

Tecnam Astore specs

Tecnam Astore Engine and Performance

Tecnam Astore is equipped with optional engine versions including 912ULS2, N 912is and 914UL2 produced by Rotax. Standard aircraft are powered by the Rotax 912ULS2 engine which can produce up to 115 hp. This engine drives two/ three-blade Sensenich composite blades which can be adjusted on land. This aircraft has a total fuel capacity that can be used 110 l (29 gal).

Tecnam Astore aircraft can fly with a maximum speed of 222 km / hour and a maximum cruise speed of 219 km / hour. It has a maximum range of 750 nm at a climbing rate of 5.6 m / s and a service ceiling of 4,572 m (15,000 ft). The aircraft requires a takeoff distance of 218 m and a landing distance of 154 m.

Tecnam Astore cockpit

Tecnam Astore Cockpit and Avionics

The Tecnam Astore cockpit can be equipped with three optional flight instruments which include the Astore six pack, the Dynon SV1000 plus GPS 796, and the two-screen G3X display. The aircraft has a glass canopy and is equipped with a flight control system including a hydraulic foot brake, a single throttle lever, an electric flap, dual flight controls, trim stabilizers, and a choke.

The standard avionics suite installed on Tecnam Astore includes a magnetic compass, airspeed and sidelip indicators, altimeters and a static system. Avionics further includes panel panels, fuel press, clock recorder, and aviator trim with indicators. Pilots can use the Wi-Fi connection to display on iPad mini the altitude, airspeed shown, and GPS.

Tecnam Astore Cabin and Interior

The Tecnam Astore cabin is 1.15 m wide and 0.98 m high. This includes baggage compartments with a total volume of 11.6 ft³ and a maximum load carrying capacity of up to 35 kg. The cabin interior includes environmentally friendly leather seats featuring three-point seat belts and adjustable front and rear. This includes an adjustable ventilator, a heating system, and a windshield defroster. The cabin is equipped with an Apple iPad mini charger and a USB charger.

Tecnam Astore Price and Orders

The price of the latest Tecnam Astore light sport aircraft is around US $ 147,000 ($ 176,000 with Rotax 912iS). To date, Tecnam has received orders for Astore from various operators throughout the world including New Zealand, Korea, Brazil, South Africa, Spain, Kuwait and the US.

Saturday, 23 November 2019

Gulfstream G700 Specs, Interior, Cockpit, and Price

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Gulfstream G700 Specs, Interior, Cockpit, and Price – Gulfstream G700 is the latest long-sized twin-engine business jet manufactured by Gulfstream Aerospace based in the United States. This business jet was first launched at the NBAA Business Aviation Convention & Exhibition (NBAA-BACE) in Los Angeles in October 2019. This will be the longest variant currently produced by Gulfstream.

The Gulfstream G700 business jet combines ultralong range, speed and proven performance with flight-deck innovation and the latest cabin creation. The aircraft has carried out lab tests for 14,000 hours, including engine speed, load calibration, ground vibration testing, and structural element evaluations.

Gulfstream G700 business jet

Gulfstream G700 Specs

The Gulfstream G700 fuselage has a low wing monoplane design based on the G650 variant. The fuselage has swept wings with wings at the ends. The overall dimensions of the aircraft include a length of 33.48 m, a height of 7.75 m, and a wingspan of 31.39 m. This aircraft has an optimal take-off weight of 48,807 kg and a load capacity of 2,896 kg.

Gulfstream G700 has the highest, widest and longest cabin with the range and speed capabilities developed by Gulfstream Aerospace. it uses avionics-based systems to monitor and control engine performance, take-off and landing, and safety measures.

Gulfstream G700 Engine and Performance

Gulfstream G700 is powered by two Rolls-Royce Pearl 700 engines that can generate 18,250 lbf of thrust each. The Pearl 700 engine was developed specifically for this business jet, the engine is equipped with a four stage high efficiency low pressure turbine (LPT) and a new ultra slim-line nacelle. The engine produces a 12% higher thrust-to-weight ratio with 5% fuel efficiency.

The Gulfstream G700 business jet can fly with a maximum operating speed of Mach 0.925 (1,142 km / h) and a maximum cruise speed of Mach 0.9 (1,073 km / h). The aircraft has a cruising altitude of 51,000 ft (15,545 m) and a maximum range of 7,500 nm (13,900 km)

Gulfstream G700 interior

Gulfstream G700 Cabin and Interior

Gulfstream G700 has a long cabin with five living rooms that can accommodate up to 19 passengers. The cabin interior can be configured into a waiting room or crew compartment, dining / conference room, and master bedroom. Designed with a major emphasis on lifestyle and space, this cabin offers the lowest cabin height in its class and is suitable for arranging meetings and dinners.

The Gulfstream G700 cabin is equipped with a sophisticated circadian lighting system that integrates white and yellow LEDs. A total of 20 panoramic oval windows are installed on each side of the cabin to provide natural light to the living room and increase passenger visibility. This lighting system can reduce the impact of passenger jet-lag.

Overall, the Gulfstream G700 cabin has a length of 19.41 m, a width of 2.49 m, a height of 1.91 m, and a luggage compartment with a storage volume of 5.52 m³. The cabin features artificial intelligence (AI) and ergonomic design and is also equipped with Jet ConneX Ka-band Wi-Fi.

Gulfstream G700 cockpit

Gulfstream G700 Cockpit and Avionics

The Gulfstream G700 business jet is equipped with Honeywell Symmetry Flight Deck which is equipped with an integrated touch screen controller for system control, flight management, communication, checklists, and weather forecasts. This aircraft has a next generation flight management system (NGFMS) that is optimized for future air traffic management (ATM) which helps improve operating cost efficiency. The cockpit is equipped with active control Sidestick to reduce the workload of flight crew during long flights.

Other systems mounted on the Gulfstream G700 cockpit include an enhanced battle vision system with a double head-up display, synthetic vision with a double head-up display, and a primary flight display. A predictive landing performance system was also installed to enable safe landing.

Gulfstream G700 Price and Orders

The price of the latest Gulfstream G700 business jet is US $ 75 million. Qatar Airways is a customer launch of the G700 aircraft, as many as ten jets have been ordered for Qatar Executive charter services in October 2019. The aircraft will be delivered in 2022.

Thursday, 21 November 2019

Bye Aerospace eFlyer 2 Specs, Range, Cockpit, and Price

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Bye Aerospace eFlyer 2 Specs, Range, Cockpit, and Price – eFlyer 2 is a lightweight electric aircraft with a capacity of 2 passengers developed by Bye Aerospace, United States. This aircraft was originally named Sun Flyer 2 which was intended for pilot training missions. Sun Flyer 2 was renamed eFlyer 2 in April 2019. Bye Aerospace began flight testing with new Siemens motorcycles in July 2019 and is expected to receive Federal Aviation Administration (FAA) certification by 2020.

The prototype eFlyer 2 aircraft completed its first flight at the Centennial Airport (KAPA) located in Colorado in April 2018. During the flight test, the flight characteristics of the aircraft assessed included speed, altitude, and endurance.

Bye Aerospace eFlyer 2 electric aircraft

Bye Aerospace eFlyer 2 Specs

The fuselage eFlyer 2 has a low wing support design and is made of composite materials. Overall, the dimensions of the eFlyer 2 aircraft include a wingspan of 11.58 m, wing area of ​​12 m², cabin width of 1.16 m, and a sliding ratio of 18.5. This aircraft has an empty weight of 662 kg, while the gross weight of the aircraft is 862 kg.

The eFlyer 2 aircraft is equipped with a two-bladed composite propeller and fixed tricycle type landing gear with spring suspension. This aircraft offers a longer operating period and is integrated with the ballistic parachute recovery system. This offers lower operating costs compared to other sized aircraft, which is US $ 14 per hour.

Bye Aerospace eFlyer 2 specs

Bye Aerospace eFlyer 2 Engine and Performance

The eFlyer 2 aircraft is powered by a new Siemens SP70D single electric motor powered by six lithium-ion batteries. The aircraft is equipped with a control unit that allows optimal use of battery energy to control engine performance.

The electric propulsion system can produce a thrust of 90kW. The eFlyer 2 aircraft can fly with a maximum speed of 250 km / h and has a flight endurance range of 3.5 hours. The aircraft has a maximum climbing rate of 5.3 m / s.

Bye Aerospace eFlyer 2 cockpit

Bye Aerospace eFlyer 2 Cockpit and Avionics

The eFlyer 2 cockpit has an open design that is covered in a bubble canopy. The cockpit is equipped with an iPad to display the characteristics of the motor, battery and aircraft systems. Real-time information from the engine, flight time, location and altitude of the aircraft can be tracked by the Sidekick system provided by Redbird Flight Simulation.

The on-board avionics suite integrated in the eFlyer 2 aircraft is provided by Avidyne Corporation. With the support of a special instrument panel next generation makes the aircraft more easily flown by a single pilot.

Bye Aerospace eFlyer 2 Price and Orders

The price of the latest eFlyer 2 aircraft is around US $ 349,000. Spartan College of Aeronautics and Technology became the first operator to order 20 eFlyer 2 aircraft in 2016.

BlackBird placed orders for the first 100 commercial four-seat eFlyer 4 and ten eFlyer 2 commercial aircraft, while OSM Aviation Group also ordered 60 eFlyer 2 aircraft in May 2019. Bye Aerospace received commitments for 298 eFlyer aircraft from unknown customers in May 2019.

Tuesday, 19 November 2019

Cessna Turbo Stationair Specs, Interior, Cockpit, and Price

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Cessna Turbo Stationair Specs, Interior, Cockpit, and Price – Cessna Turbo Stationair is a piston-engine light sport aircraft (LSA) with capacity of 6 passengers manufactured by Cessna, a subsidiary of Textron. This aircraft was first launched in 1963 as the Cessna 210. Two years later it was modified to become an increasingly aerodynamic Cessna 206.

At the end of 1997, the company launched the latest variants namely the Cesnna 206H and Cessna T206H which were equipped with turbocharge engines. Both of these variants have operated in various services with defense forces from Argentina, Bolivia, Costa Rica, Djibouti, Guyana, India, Israel, Mexico, Malaysia, Paraguay, Peru, Philippines, Uruguay and Venezuela.

Cessna Turbo Stationair

Cessna Turbo Stationair Specs

Cessna Turbo Stationair can be used as light commercial airplanes, private / light sport aircraft, business aircraft, and decorative aircraft. This aircraft has dimensions which include a length of 8.6 m, height 2.8 m, wingspan 10.97 m, and a wing area of ​​16.17 m².

Cessna Turbo Stationair aircraft can be operated during the day or night. The fuselage made of aluminum alloy makes Stationair aircraft proven to be corrosion resistant, so it can be operated in a variety of weather conditions. The aircraft is equipped with a fixed tricycle type landing gear and can be modified into a ski board for amphibious support.

Cessna Turbo Stationair Engine and Performance

The Cessna Turbo Stationair is powered by a Lycoming TIO-540-AJ1A single piston engine with a turbocharged engine. The engine can produce a maximum power output of 310 hp to drive McCauley's constant speed three-bladed metal propeller with ice boots.

Cessna Turbo Stationair aircraft can fly with a maximum cruise speed of 298 km / h with a maximum range of up to 703 nm (1,302 km). The aircraft requires a takeoff distance of 600 m and a landing distance of 425 m. The aircraft service ceiling is 26,000 ft (7,925 m).

Cessna Turbo Stationair cockpit

Cessna Turbo Stationair Cockpit and Avionics

the Cessna Turbo Stationair's cockpit is integrated with the Garmin G1000 NXi avionics suite. The glass cockpit is equipped with two 26.4 cm active matrix LCDs to display all the flight, engine and main sensor data in real time.

Furthermore, the Cessna Turbo Stationair can also be optionally installed with the GFC 700 Automatic Flight Control System (AFCS) and Flight Director (FD), Wide Area Augmentation System (WAAS), Garmin SafeTaxiTM and Garmin FliteCharts as standard equipment.

Cessna Turbo Stationair interior

Cessna Turbo Stationair Cabin and Interior

The Cessna Turbo Stationair cabin is 3.7 m long, 1.08 m wide, and 1.3 m high. The cabin can accommodate up to 6 passengers side by side or can be configured into four spatial arrangements namely only pilots, one pilot and one passenger, pilot and three passengers, and pilot and five passengers. The cabin is equipped with an access door with a height of 1.04 m and a width of 0.885 m. The cargo area is accessed through the clamshell door on the exterior cargo pod.

Cessna Turbo Stationair Price and Orders

The price of the latest Cessna Turbo Stationair light air sport aircraft is around US $ 714,000. At present more than 4,000 aircraft have been ordered and operate in various services throughout the world.

Sunday, 17 November 2019

Cessna Skylane Specs, Interior, Cockpit, and Price

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Cessna Skylane Specs, Interior, Cockpit, and Price – The Cessna Skylane is a piston-engine light sport aircraft (LSA) with capacity of 4 passengers manufactured by Cessna, a subsidiary of Textron Aviation. This aircraft has been produced since 1956 with a variant of 182. Until now, the Cessna has built more than 20,000 units of Skylane aircraft. Cessna launched the latest variant of the 182T Skylane in 2000.

Cessna Skylane aircraft are certified to the requirements of the US FAA Federal Aviation Regulations Part 23 through amendments 23-6, including day, night, VFR (Visual Flight Rules) and IFR (Instrument Flight Rules). Enhancements for the aircraft include stainless steel control cables and corrosion inspection of the whole body epoxy. The 182T Skylane variant was certified on February 23, 2001 and is the only variant in production to date.

Cessna Skylane light sport aircraft

Cessna Skylane Specs

The Cessna Skylane fuselage has a high wing monoplane design which is equipped with a supporting post on each wing. The fuselage is made of all-metal (mostly aluminum alloy), while the engine cover and wingtip are made of fiberglass though. This aircraft is equipped with a fixed tricycle type landing gear.

The overall dimensions of the Cessna Skylane include 8.84 m in length, 2.84 m in height, 10.97 m in wingspan, and 16.17 m² in wing area. This aircraft has a gross weight of 1,406 kg for take-off and 1,338 kg for landing. The aircraft can carry a maximum payload of up to 431 kg.

Cessna Skylane Engine and Performance

The Cessna 182T Skylane is powered by a Lycoming IO-540-AB1A5 single piston engine. The engine can produce a maximum power output of 230 hp to drive a McCauley three-bladed metal propeller constant speed.

Cessna Skylane aircraft can fly with a maximum cruise speed of 269 km / h and have a maximum range of up to 915 nm (1,695 km). The aircraft requires takeoff and landing distances of 461 m and 411 m, respectively. The aircraft service ceiling is 5,517 m.

Cessna Skylane cockpit

Cessna Skylane Cockpit and Avionics

The Cessna 182T Skylane glass cockpit is integrated with the Garmin G1000 NXi avionics. The cockpit is equipped with two active 26.4 cm matrix LCDs to display all the flight, engine and main sensor data in real time. With an improved graphical interface, stronger hardware, higher resolution display, additional functionality will increase situational awareness of pilots when flying aircraft.

In addition, the Cessna Skylane can also be optionally installed with the Garmin Automatic Flight Control System GFC 700 (AFCS) and Flight Director (FD), Wide Area Augmentation System (WAAS), Garmin SafeTaxiTM and Garmin FliteCharts as standard equipment.

Cessna Skylane interior

Cessna Skylane Cabin and Interior

The Cessna Skylane cabin can accommodate four passengers, including pilots. The cabin is 3.4 m long, 1.07 m wide, and 1.2 m high. The cabin is accessed through 2 doors found on each side. Luggage area and luggage nets are behind the rear passenger seat. The aircraft's luggage capacity is 91 kg.

Cessna Skylane Price and Orders

The price of the latest Cessna Skylane light sport aircraft is around US $ 515,000. This aircraft is most often used for personal use / light sport, small business use and as a coach. Cessna has nearly 300 Cessna Pilot Centers (CPC) worldwide.

The Cessna 182 Skylane variant is currently operating with the US Civil Air Patrol as a platform for digital search and rescue satellite imaging systems and has been operated by defense forces in Argentina, Belize, Canada, Guatemala, Lesotho, Peru, Uruguay and Venezuela.

Friday, 15 November 2019

Cessna Skyhawk Specs, Interior, Cockpit, and Price

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Cessna Skyhawk Specs, Interior, Cockpit, and Price – Cessna Skyhawk is a piston-engine light sport aircraft (LSA) with capacity of 4 passengers produced by Cessna, a subsidiary of Textron Aviation. This aircraft can be used in a variety of operations, including personal and small business use, as well as trainer aircraft. Cessna has built nearly 300 Cessna Pilot Centers (CPC) worldwide. Originally the aircraft was known as the Cessna 172 Skyhawk and first flew in 1955, the aircraft began to be produced a year after. The latest variant of this aircraft is the JT-A Turbo Skyhawk which was certified by EASA and FAA in June 2017. Currently the company is also developing an electric-powered Skyhawk aircraft.

Cessna Skyhawk light sport aircraft

Cessna Skyhawk Specs

The Cessna Skyhawk fuselage is made of aluminum alloy which is resistant to corrosion, so the aircraft can be operated in a variety of weather conditions. Overall, the dimensions of the aircraft include a length of 8.3 m, height 2.7 m, wingspan 11.00 m and a wing area of ​​16.17 sq m.

This aircraft has a fixed tricycle type landing gear that is strong and can absorb shocks. The wheels are equipped with hydraulically driven disc brakes for handling and stable driving stability on the ground. The aircraft also has a high-intensity discharge lamp (HID) to support operation at night.

Cessna Skyhawk Engine and Performance

The Cessna Skyhawk is powered by a Lycoming IO-360-L2A single piston engine that can produce thrust of 180 hp. This engine drives a fixed-pitch two-bladed McCauley metal propeller.

Cessa Skyhawk can fly with a maximum cruising speed of 230 km/ h to a maximum range of 640 nm (1,185 km). This aircraft requires takeoff distance and landing distance, 497 m and 407 m, respectively. the aircraft service ceiling is 14,000 ft (4,267 m).

Cessna Skyhawk cockpit

Cessna Skyhawk Cockpit and Avionics

The Cessna Skyhawk cockpit is integrated with the G1000 NXi avionics suite supplied by Garmin. The cockpit is equipped with two active 26.4 cm matrix LCDs that display all flight data including synthetic terrain, flight hazards, flight path markers, highways, engines and main sensors in real time.

Avionik G1000 also presents weather XM WX satellite with XM satellite radio that can be activated by subscription. It integrates with transponders and dual navigation / communication / WAAS / GPS equipment. The Skyhawk variant also comes with a Garmin GFC 700 flight control system that is fully integrated with airspeed, high speed protection, pitch restraints, and paired VNAV. This system provides precise lateral and vertical guidance and capabilities.

Cessna Skyhawk interior

Cessna Skyhawk Cabin and Interior

The Cessna Skyhawk cabin is 3.6 m long, 1.00 m wide and 1.2 m high. The cabin can be configured for four passengers, one or two pilots, and two-seat bench seats. Two doors are provided on each side of the cabin to facilitate passenger entry and exit. The cabin is equipped with 54 kg luggage which is behind the rear seat and is accessed through a special door.

The lighting system in the cab can be adjusted as needed. Specifically in the pilot cabin equipped with colored sun protection features to reduce cockpit glare and eye fatigue when flying a plane.

Cessna Skyhawk Price and Orders

The price of the latest Cessna Skyhawk light sport aircraft is around US $ 310,000. At present, Cessna has received orders for more than 43,000 Skyhawk aircraft and all of them have been sent to various operators throughout the world. In August 2009, the company sent five new Cessna Skyhawks to Northwestern Michigan College to train students.

Wednesday, 13 November 2019

Eviation Alice Commuter Specs, Interior, Cockpit, and Price

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Eviation Alice Commuter Specs, Interior, Cockpit, and Price – Eviation Alice Commuter is a regional electric-powered airplane with zero emissions which is being developed by Eviation Aircraft, Israel. This aircraft is designed to carry up to nine passengers and two crews in accordance with FAA Federal Aviation Regulations Part 23, this aircraft is a fully electric commercial business aircraft that is fully qualified.

The Eviation Alice prototype was introduced at the 53rd International Paris Air Show in 2019. The aircraft is currently in the development and testing phase and its first flight is expected to take place in 2020. It is estimated that the aircraft certification program will be completed in 2021, before its commercial launch in next.

Eviation Alice Commuter

Eviation Alice Commuter Specs

The Eviation Alice airframe was built using lightweight carbon fiber composite materials supplied by Carboman Group's subsidiary, Multiplast. Composite materials will offer a lightweight airframe while maintaining its strength. This aircraft has a fixed wing design, low wing configuration, and v-tail rear structure.

Takeoff and landing operations are supported by regular tricycle type retractable landing gear. The landing gear wheel was supplied by Magnaghi Aeronautica. Overall the Eviation Alice aircraft has a length of 12.2 m, wingspan reaches 16.12 m and the maximum take-off weight is 6,350 kg.

The Eviation Alice uses a distributed propulsion system consisting of a five-bladed main propeller, which is reinforced by a pair of additional propeller thrusters mounted at the wingtips. The propeller is specially developed by the Hartzell Propeller company. The main propeller propellers are able to take off and land in the event of an emergency wingtip.

The blades are made of carbon fiber material, with the leading edge of cobalt nickel. The wingtip propellers help reduce the induced drag, while the motor helps with the self-balancing evaporating operation.

Eviation Alice Commuter Engine and Performance

The Eviation Alice aircraft is powered by three electric motors which generate thrust of 260 kW each. The power source to drive the engine comes from a 900 kWh lithium-ion battery whose charge can be 100% recharged in two to three hours. Electric drive motors are supplied by Siemens and MagniX.

Eviation Alice has a maximum allowable speed of 630 km / h and a maximum cruise speed of 482 km / h at an altitude of 10,000 ft. The aircraft can go up to 30,000 ft and is capable of flying up to a range of 1,046 km on a single charge and offers 45 minutes of backup power in the event of an emergency.

Eviation Alice cockpit

Eviation Alice Commuter Cockpit and Avionics

Eviation Alice's cockpit equipped with a large windshield offers better lighting. The cockpit can accommodate two crew members consisting of a pilot and co-pilot. This aircraft integrates Honeywell avionics and fly-by-wire flight systems. The aircraft is also equipped with a thermal management system to maintain the temperature of the electric engine unit and an autonomous landing system.

Eviation Alice interior

Eviation Alice Commuter Cabin and Interior

The pressurized cab of the Eviation Alice aircraft offers spacious and comfortable seating for 9 passengers, with direct access to the aisle for everyone. The aircraft will have low operating costs given its all-composite structure and electrical energy source, which also produces zero emissions and low noise levels.

Eviation Alice Commuter Price and Orders

The price of the Eviation Alice Commuter electric aircraft is around US $ 4 million. Although the aircraft is currently under development, US regional airline Cape Air has ordered Eviation Alice with deliveries scheduled to begin in 2022.

Monday, 11 November 2019

Saab 2000 Specs, Interior, Cockpit, and Price

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Saab 2000 Specs, Interior, Cockpit, and Price – Saab 2000 is a regional turboprop engine developed by Saab Aircraft, Sweden. The Saab 2000 aircraft made its first flight in March 1992 and entered service with the launch customer Crossair (now Switzerland) in 1994. The Saab 2000 aircraft is an extended version of the Saab 340.

The Saab 2000 aircraft is being developed as an early warning and air control variant (AEWC). This variant is equipped with Saab Systems Erieye PS-890 which sided with the spine which looked like a surveillance radar. Another variant is the Saab 2000FI, a flight inspection mission aircraft developed for the Japanese Civil Aviation Bureau.

Saab 2000 Jetliner

Saab 2000 Specs

The design of the Saab 2000 airframe is based on the Saab 340. The aircraft is integrated with low wings and a conventional tail. The aircraft propulsion system is a six-bladed type Dowty R381 propeller system. The propeller is equipped with electric de-icing. Overall, Saab 2000 has a length of 27.28 m, a fuselage diameter of 2.31 m, a height of 7.73 m, and a wingspan of 24.76 m.

The Saab 2000 aircraft has two integral fuel tanks mounted on the wing. The tank can hold fuel with a total capacity of 5,300 l. The fuel system is equipped with a gravity overwing refueling station on each wing and one pressure refueling station on the right wing.

Saab 2000 Engine and Performance

The Saab 2000 aircraft are powered by two Rolls-Royce Allison AE 2100A turboprop engines. Each engine is capable of producing a maximum power of 3,096 kW and is equipped with Lucas Aerospace Full Authority Digital Engine Control (FADEC). The aircraft is equipped with an additional Sundstrand power unit providing power for engine start and for the air conditioning system.

Saab 2000 aircraft can fly with a maximum cruise speed of 685 km / h and have a maximum range of 2,868 km. High speed performance allows airline operators to exchange fleet schedules with jets on 500 nm routes. The aircraft can carry 50 passengers to destinations of more than 1,000 nm in three hours flight time.


Saab 2000 interior

Saab 2000 Cabin and Interior

The Saab 2000 cabin is 16.7 m long and 2.16 m wide. The cabin is configured in one aisle with three-parallel seating arrangements to accommodate 50 to 58 passengers. The cabin is equipped with an active Ultra Electronics noise control system. The aircraft is equipped with a Pacific Scientific fire detection system, a Kidde Graviner fire extinguisher system, AC Hamilton Standard Recircair and an environmental control system that uses air from the engine. The pressurized and air-conditioned cabin will make passengers feel comfortable when on the plane.

Saab 2000 cockpit

Saab 2000 Cockpit and Avionics

The Saab 2000 cockpit is equipped with the Rockwell Collins Pro Line 4 avionics suite with an integrated avionics processor (IAP), engine indication and crew warning system (EICAS) and traffic warning systems and impact avoidance systems (TCAS). Flight control systems include the Post and Attitude Reference System (AHRS) and the Digital Air Data System (DADS).

The Saab 2000 navigation suite includes an inertia reference system, Rockwell Collins WR-840 solid-state weather radar with an optional turbulence detection radar. The cockpit has Swedlow panel windshield which is electrically heated.

Saab 2000 Price and Orders

The price of the Saab 2000 aircraft is around US $ 15 million. There are 60 Saab 2000 aircraft operating throughout the world in France, Ireland, Italy, Japan, Lithuania, Marshall Islands, Sweden, Switzerland and the United States. However, aircraft production had stopped in 1999.

Saab Aircraft, headquartered in Washington DC, leases around 289 Saab 340 and Saab 2000 aircraft to 25 airlines. Airlines that rented Saab 2000 included AirJet of France, Lithuanian Airlines, AeroLitoral of Mexico, Transwest Air of Canada, Blue 1 (formerly Air Botnia) from Finland and OLT GmbH from Germany.