Thursday, 9 January 2020

ATEC 322 Faeta Specs, Interior, Cockpit, and Price

01:00
ATEC 322 Faeta Specs, Interior, Cockpit, and Price – ATEC 322 Faeta is a two-seater light sport aircraft (LSA) designed and developed by ATEC, Czech Republic. This aircraft can be used by flight training schools, couples, pilots and retired pilots. The aircraft underwent flight tests in October 2015 and is ready for shipping in the S-LSA category to US distributors.
ATEC 322 Faeta light sport aircraft

ATEC 322 Faeta Specs

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

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

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

ATEC 322 Faeta Engine and Performance

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

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

ATEC 322 Faeta Cockpit and Avionics

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

 Avionics further includes position recorders, three-axis autopilot, and various GPS, radio, and emergency locator transmitters (ELT). It also includes a USB connector, MP3 and movie player. The pedal can be adjusted in three positions, according to the height of the pilot.
ATEC 322 Faeta interior

ATEC 322 Faeta Cabin and Interior

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

ATEC 322 Faeta Price

The price of the ATEC 322 Faeta light sport aircraft is around US $ 150,000.
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Tuesday, 7 January 2020

Evektor Harmony Specs, Interior, Cockpit, and Price

01:00
Evektor Harmony Specs, Interior, Cockpit, and Price – The Evektor Harmony is a two-seat light sport aircraft manufactured by Evektor-Aerotechnik, a company from the Czech Republic. This aircraft can be used for cross-country tour and training purposes. The aircraft obtained the USA FAA approval certificate in 2011 and the first aircraft were sent to the US that same year. The aircraft subsequently received a special airworthiness certificate from the Directorate General of Civil Aviation in Chile in May 2014.
Evektor Harmony light sport aircraft

Evektor Harmony Specs

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

Evektor Harmony Engine and Performance

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

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

Evektor Harmony Cabin and Interior

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

Evektor Harmony Cockpit and Avionics

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

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

Evektor Harmony Price

The price of the newest Evektor Harmony light sport aircraft is around US $ 125,000.
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Sunday, 5 January 2020

ONE Light Sport Aircraft Specs, Cockpit, and Price

01:00
ONE Light Sport Aircraft Specs, Cockpit, and Price – ONE is a safe, affordable and efficient light sport aircraft (LSA) designed and developed by ONE Pro, Slovenia. This aircraft can be used by flight training schools, couples, pilots and retired pilots. It underwent horizontal and static tests respectively in November 2012 and January 2013, and was exhibited at the AERO trade show held in Europe in April 2015. The sport-family configuration of the aircraft is currently in the process of being certified for CS-VLA (3-4 seat) with the European Aviation Security Agency (EASA). It was also certified for the US LSA configuration in 2016.
ONE Light Sport Aircraft

ONE Light Sport Aircraft Specs

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

ONE Light Sport Aircraft Engine and Performance

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

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

ONE Light Sport Aircraft Cabin and Interior

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

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

ONE Light Sport Aircraft Cockpit and Avionics

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

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

ONE Light Sport Aircraft Price

The price of the latest ONE light sport aircraft is around US $ 110,000.
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Friday, 3 January 2020

Lisa AKOYA Specs, Interior, Cockpit, and Price

01:00
Lisa AKOYA Specs, Interior, Cockpit, and Price – Lisa AKOYA is a two-seat amphibious light sport aircraft designed and developed by Lisa Airplanes, France. This aircraft can operate on land, water and snow, designed in accordance with the American community for international standards of testing and materials (ASTM) F37 for lightweight sport aircraft. The aircraft specifications have been certified by the European air safety agency for very light aircraft (CS-VLA).

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

Lisa AKOYA Specs

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

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

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

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

Lisa AKOYA Engine and Performance

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

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

Lisa AKOYA Cabin and Interior

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

Lisa AKOYA Cockpit and Avonics

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

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

Lisa AKOYA Price

The price of Lisa AKOYA amphibious light sport aircraft is around US $ 350,000. Since the aircraft was shown at AirVenture in July 2015, Lisa Airplanes's company claims to have had about 100 orders.
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Wednesday, 1 January 2020

Glasair Merlin Specs, Interior, Cockpit, and Price

17:16
Glasair Merlin Specs, Interior, Cockpit, and Price – Glasair Merlin is a high-wing light sport aircraft developed by Glasair Aviation, USA. This aircraft is designed to meet LSA certification requirements based on the American Society for Testing and Materials (ASTM) standards. The aircraft was introduced in April 2014 and completed its first flight at Arlington Airport in April 2015. The flight test lasted for more than 57 minutes. This aircraft was exhibited at AirVenture Oshkosh in August 2015. Glasair Aviation plans to produce the first certified light sport aircraft in its factories in Arlington and China.
Glasair Merlin light sport aircraft

Glasair Merlin Specs

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

Glasair Merlin Specs Engine and Performance

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

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

Glasair Merlin Cabin and Interior

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

Glasair Merlin Specs Cockpit and Avionics

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

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

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

Glasair Merlin Price

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