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Tuesday, 25 February 2020

Cirrus SR22 Specs, Interior, Cockpit and Price

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Cirrus SR22 Specs, Interior, Cockpit and Price – The Cirrus SR22 is a high-performance lightweight, piston-engined passenger aircraft manufactured by Cirrus Design Corporation (CDC), United States. This aircraft was launched in 2000, this is an enhanced version of the Cirrus SR20. Cirrus SR22 aircraft are supported by a single engine and are equipped with a parachute designed by BRS and turbo normalization options. The aircraft equipped with ice protection received Federal Aviation Administration (FAA) certification in April 2009. This became the best-selling model aircraft owned by the CDC company. Currently the company has developed the latest version of the aircraft, the SR22-G3 third generation and also the SR22T version with new engine options and a modern environmental control system.

Cirrus SR22 aircraft

Cirrus SR22 Specs

The Cirrus SR22 fuselage has a low-wing monoplan design made of composite materials. This aircraft has a tricycle type landing gear wheel that cannot be pulled. On each side of the fuselage equipped with passenger doors and windows tilted backwards. The wheel cover, fairing support and inner edge of the wing are coated with 3M paint protective film to protect paint from scratches. The dimensions of the Cirrus SR22 aircraft include a length of 7.92 m, height 2.7 m, and wingspan 11.68 m.

Cirrus SR22 aircraft are designed to carry gross weights of up to 1,542 kg. The aircraft's empty weight is 1,028 kg and the useful load that can be carried by the aircraft is 605 kg. The aircraft has a fuel capacity that can be used which is 348 liters.

Cirrus SR22 aircraft has a ballistic parachute system called the Cirrus Airframe Parachute System (CAPS), and a four-point seat belt with a built-in air bag for pilots and co-pilots. CAPS was designed by BRS in collaboration with Cirrus. This is a solid-fuel rocket motor used, and uses a 17 m parachute. Pilots or passengers can use a parachute by pulling on the overhead handle.

Cirrus SR22 Engine and Performance

The Cirrus SR22 is powered by a Continental IO-550-N piston engine. The engine produces an output power of 310 hp to spin the three-bladed Hartzell propeller at constant speed. This aircraft has a climbing rate of 1270 ft / min (6.45 m / sec), and can fly to heights of 17,500 ft.

Cirrus SR22 aircraft can fly with a maximum speed of 185 KTAS (340 km / h). The stall speed is a calibrated air speed of 60 KCAS (104 km / h) with a flap. The maximum range that can be traveled by Cirrus SR22 aircraft is 1,170 nm with 55% power. The aircraft requires a 348 m Landing Groundroll and a 330 m take-off distance.

The Cirrus SR22 aircraft also has an engine option with a Tornado Alley upgrade turbo. The use of turbo can improve aircraft performance which includes an increase in operating altitude up to 25,000 ft and an increase in turbo maximum cruising speeds of up to 219 ktas, 34 kt higher than the standard version.

Cirrus SR22 cockpit

Cirrus SR22 Cockpit and Avionics

The Cirrus SR22 cockpit is fully integrated with the Garmin Cirrus Perspective avionics suite. The avionics suite includes a 12in dual screen (PFD and MFD), electronic environment control system, airway flight planning, keyboard controller, GFC 700 autopilot with GMC 705 controller, engine and fuel monitoring, dual radio communication / navigation, dual WAAS GPS, AHRS double, and FliteCharts.

The XM radio weather data link has been installed to provide important weather information including next-generation radars, METAR, TAF, AIRMET (pilot meteorological information), SIGMET (important meteorological information), TFR (radar following the terrain), high winds, freezing levels and lightning. A synthetic vision technology that provides 3D images from the outside, helps identify terrain warnings, obstacles, traffic, flight path markers, zero pitch lines, runways, airport signs, and "highways in the sky" or lane guidance.

Cirrus SR22 aircraft is equipped with a traffic information system that will display a message on a multi-function display (MFD) if there are other aircraft equipped with transponders approaching. An audible warning also sounds when another aircraft is too close. There is also an enhanced vision system (EVS) that uses an EVS-600 camera to detect and display night vision and visible light on the MFD.

Cirrus SR22 interior

Cirrus SR22 Cabin and Interior

Cirrus SR22 cabin has 124 cm width and 127 cm height. The cabin can accommodate 4-5 passengers including the pilot and co-pilot. There are large doors on each side of the cabin that provide easy entry and exit of passengers into the cabin. The cabin interior includes chairs made of quality and durable materials. Special front seats are equipped with airbag seat belts. The cabin is also equipped with UV Protected Windows to prevent direct UV radiation and increase passenger visibility.

Cirrus SR22 Price and Orders

The price of the latest Cirrus SR22 aircraft is around US $ 629,900. In July 2007, PlaneSmart, a professional aircraft management company, announced plans to replace the SR22-G2 fleet with SR22-G3s. The third generation SR22-G3 aircraft was delivered to PlaneSmart in September 2007. To date, more than 5,000 aircraft have been delivered and operated by operators in various services.

Sunday, 23 February 2020

Cirrus SR20 Specs, Interior, Cockpit and Price

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Cirrus SR20 Specs, Interior, Cockpit and Price – Cirrus SR20 is a lightweight piston-engined passenger aircraft manufactured by Cirrus Design Corporation (CDC), United States. This aircraft can be used for personal, corporate and pilot training. The Cirrus SR20 aircraft was certified by the Federal Aviation Administration (FAA) in October 1998 and became the first of its kind to receive a European Aviation Agency (EASA) certificate in June 2004. At present more than 6,000 SR20 aircraft have been operating in a variety of services.

Cirrus SR20 aircraft are available in three SR20S, SR20GS and SR20GTS models. SR20S and SR20GS come in a single exterior color, a white base color. SR20GTS comes in three exterior colors, namely white, dark red, and iridium. VarianS has a total weight of 2,093 lb, while the GS and GTS versions have a weight of 2,144 lb and 2,167 lb respectively. Strip packages for SR20S and SR20GS are "Matador" and "Red Dusk" respectively while the interior is made of slate cloth for both variants. Meanwhile, the strip package for the SR20GTS variant is "Garnet" and the interior is made of slate leather.

The SR20GS and SR20GTS variants can be customized for X edition. X Edition features premium exterior and interior, including adjustable interiors. In a typical SR20 X edition, the instrument panel and center console are coated with carbon fiber and aluminum which are machined. The cabin is covered with leather with specially stitched accents and comfortable chairs made from Alcantara.

Cirrus SR20 aircraft

Cirrus SR20 Specs

The Cirrus SR20 airframe has a low-wing monoplane design. The aircraft landing system consists of a tricycle type non-retractable landing gear wheel. Overall the dimensions of the Cirrus SR20 include a length of 7.92 m, a height of 2.71 m, and a wingspan of 11.68 m. This aircraft is designed to carry a maximum gross weight of 1,386 kg and has a standard empty weight of 945 kg, a useful load of 441 kg, usable fuel capacity of 56 gal / 336 lb (212 l / 153 kg) and a full fuel load of 288 kg.

The Cirrus SR20 aircraft includes a ballistic parachute system and four-point seat belts with built-in air bags for pilots and co-pilots. The parachute system, known as the Cirrus Airframe Parachute System (CAPS), is a 17 m motorized motorized rocket parachute designed by BRS. The parachute can be activated by pulling its overhead handle in an emergency to lower the entire plane safely to land.

Cirrus SR20 Engine and Performance

The Cirrus SR20 aircraft is powered by a Continental Lycoming IO-390-C3B6 piston engine. The engine has six cylinders fueled by an adjustable exhaust system. The engine produces 215 hp of power to drive the three-bladed Hartzell propeller.

Cirrus SR20 aircraft can fly at speeds up to 155 KTAS (287 km / h) with 75% power. The kiosk speed of the aircraft is a calibrated air speed of 60 KCAS (104 km / h) with a flap. While still in the air, it can go up to a distance of 785 nm with a 55% power reserve. The aircraft requires a 260 m landing ground and 450 m takeoff distance. The aircraft can operate up to a ceiling of 17,500 ft (5,334 m) and has a climbing rate of 3.97 m / sec.
Airplane with

Cirrus SR20 cockpit

Cirrus SR20 Cockpit and Avionics

At present, the Cirrus SR20 cockpit is fully integrated with the digital avionics suite known as the Garmin Cirrus Perspective. This avionics suite includes keyboard controllers, 12 in dual screens (PFD and MFD), dual communication / navigation / WAAS GPS, engine and fuel monitoring system, flite graphics, S-tech 55 X autopilot, S-transponder mode, 406MHz ELT, GFC 700 autopilot / dual AHRS, EVS perspective and chart display.

Other avionics features on the Cirrus SR20 include weather information in flight and traffic information such as TCAS. All critical weather information including next-generation radars, METAR, TAF, AIRMET (airmen's meteorological information), SIGMET (significant meteorological information), TFR (terrain tracking radar), high winds, freezing and lightning levels are provided through XM weather links data. Stormscope WX-500 enables detection of every type of lightning including ground-based strikes and cloud-to-cloud strikes.

This aircraft is also equipped with synthetic vision technology that provides a three-dimensional appearance from the outside. Any terrain warnings, obstacles, traffic, flight path markers, zero pitch lines, runways, airport signs, and "highway guidance" or lane guidance can be easily identified through the use of synthetic vision technology.

Cirrus SR20 interior

Cirrus SR20 Cabin and Interior

Cirrus SR20 aircraft has a spacious cabin that can accommodate 4 passengers, including pilots and co-pilots. The cabin has a width of 49 in (124 cm) and a height of 50 in (127 cm). There are large doors on each side of the cabin that provide easy entry and exit of passengers into the cabin. The cabin interior includes chairs made of quality and durable materials. Special front seats are equipped with airbag seat belts. The cabin is also equipped with UV Protected Windows to prevent direct UV radiation and increase passenger visibility.

Cirrus SR20 Price and Orders

The price of the latest Cirrus SR20 aircraft is around US $ 474,900. In January 2006, four new Cirrus SR20 aircraft were sent to UND Aerospace, which were used for student training. In January 2011, Purdue University's Aviation Technology Department purchased 16 Cirrus SR20 aircraft to carry out the training program.

Friday, 21 February 2020

Pilatus PC-21 Specs, Interior, Cockpit and Price

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Pilatus PC-21 Specs, Interior, Cockpit and Price – Pilatus PC-21 is a next generation trainer aircraft with a single turboprop engine manufactured by Pilatus Aircraft of Switzerland. The trainer aircraft is designed to meet the requirements for basic, advanced and combat lead-in training for pilots and, if needed, weapons systems (WSO) officers.

The Pilatus PC-21 aircraft was launched in May 2002 and made its first flight in July 2002. The first aircraft successfully completed more than 400 flight hours. The second test plane made its first flight in June 2004 but, in January 2005, was destroyed in an accident that claimed the lives of the pilots. The first preproduction aircraft made its maiden flight in August 2005 and the second joined the flight test program in 2006. The PC-21 aircraft received certification for visual flight rules (VFR) operations in December 2004 and full certification for instrument flight rules (IFR) in December 2006 .

Pilatus PC-21 next generation trainer

Pilatus PC-21 Specs

The construction of Pilatus PC-21 aircraft is adapted to the capabilities of the latest generation of jet training. The aircraft is equipped with a sophisticated power management system with high efficiency. The aircraft has three spars and the wing design is swept with hydraulic ailerons supported by spoilers. The main edge of the wing is high impact resistant material.

Pilatus PC-21 aircraft are equipped with a fully digital glass cockpit with head-up display, face control panel (UFPC), direct throttle and stick control (HOTAS) and full sized multi-function displays that provide the same cockpit environment as the current generation of fighters , such as AV-8B, F-16, F / A-18 and Gripen.

The dimensions of the Pilatus PC-21 aircraft include a length of 11.22 m, a height of 3.74 m, and a wing width of 9.11 m. The aircraft's empty weight is 2,330 kg and its maximum take-off weight (MTOW) is 4,250 kg. The aircraft has five hard points to carry weapons, namely four hard points on the underside of the wing and one on the centerline pole.

Pilatus PC-21 specs

Pilatus PC-21 Engine and Performance

The Pilatus PC-21 is powered by Pratt & Whitney PT6A-68B single turboprop engine. The engine produces an output power of 1,200 kW (1,600 shp) to drive the five-bladed Hartzell E8991 KX graphite propeller. The engine is equipped with a digital power management system that delivers full power at speeds of more than 360 km / h and provides jet-like responses to trainer aircraft.

Pilatus PC-21 can fly with a maximum speed of 685 km / h and rise to a height of 7,620 m. The low altitude speed and climbing rate of this aircraft are more characteristic and similar to jet aircraft. The maximum cruise speed on low altitude flights is 590 km / h. The aircraft has a range of 1,297 km and a service ceiling of 11,582 m. The aircraft's takeoff distance is 725 m and its landing distance is 900 m.

Pilatus PC-21 cockpit

Pilatus PC-21 Cockpit and Avionics

The Pilatus PC-21 trainer aircraft is equipped with a glass cockpit with tandem seat configurations for pilots and co-pilots. The pressurized cockpit has an automatic cockpit conditioning system, an anti-g system, an on-board oxygen-producing system (OBOGS), and a zero-zero Martin Baker Mark 16L ejection seat. Mecaplex's two-part acrylic canopy gives pilots a broad view and is resistant to bird attacks.

Each Pilatus PC-21 cockpit is equipped with three 6 in × 8 in active matrix liquid crystal displays (AMLCD). The central liquid crystal display is the main flight display (PFD). Bezel-mounted display buttons and control panel buttons on the front (UFCP) are used to select navigation, mission, system and tactical data displayed on two external multi-function displays. Two 761 mm Meggitt secondary backup displays next to the UFCP show the main flight display, systems and important engine data. All cockpit displays and lighting systems are compatible with NVIS class B night vision.

The front and rear cockpits can be completely separated, allowing instructor access to training modes and sensor data not available for trainees pilots. The front cockpit is equipped with a Flight Visions SparrowHawk head-up display with the FVD-4000 HUD symbol generator, while the rear cockpit is equipped with a full-color HUD repeater screen that displays scenes from the HUD camera overlaid with HUD symbology information. The CMC Electronics FV-4000 mission computer is equipped with a 500MHz G4 Power PC processor, each with 512MB of memory for real-time data processing with a high refresh rate.

Pilatus PC-21 aircraft are integrated with a suite of open avionics systems that allow adaptation, system enhancement, and modification to suit the student pilot training phase. The navigation suite includes an integrated laser inertia navigation sensor, a global positioning system and a Kalman filter. This system has an ARINC 1553B data bus interface and military standards.

Pilatus PC-21 Price and Orders

The price of the latest Pilatus PC-21 trainer aircraft is around US $ 12 million. In November 2006, the Republic of Singapore Air Force (RSAF) awarded a contract to Lockheed Martin Simulation, Training and Support to operate the RSAF Basic Wings Course and Pilate supplying 19 PC-21 trainer aircraft. The first six aircraft were delivered in April 2008 and RSAF began flight training in July 2008.

In January 2007, Pilatus Aircraft received orders from the Swiss Air Force for six PC-21 aircraft. The six were delivered in 2008. The company was also awarded an additional contract of $ 31.87 million by the Swiss Air Force in December 2010 for two PC-21 trainer aircraft. The contract also covers logistics and engineering services and the supply of debreifing systems. Deliveries were made in 2012.

Under a $ 494 million contract signed in December 2009, the United Arab Emirates Air and Air Defense (UAE) bought 25 PC-21 trainer aircraft. The contract also includes the provision of an integrated ground-based training system and a comprehensive logistics support package. Delivery of 25 PC-21s equipped with the Pilatus training system to the UAE began in the first quarter of 2011. In May 2012 Saudi Arabia signed a contract with the BAE system to provide the supply of 55 Pilatus PC-21 aircraft and 22 BAE Systems Hawk Advanced Jet Trainer aircraft, which were used to train pilots to fly Eurofighter Typhoon fighter jets.

Wednesday, 19 February 2020

Pilatus PC-9M Specs, Interior, Cockpit and Price

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Pilatus PC-9M Specs, Interior, Cockpit and Price – The Pilatus PC-9M is a single turboprop engine advanced trainer aircraft manufactured by Pilatus Aircraft of Switzerland. This aircraft was produced primarily to meet the requirements of the Swiss Air Force (SAF), Australian Air Force (RAAF), Saudi Royal Air Force (RSAF) and Royal Thai Air Force (RTAF).

Development of PC-9 began in 1982 to replace the aging PC-7 fleet. The first flight PC-9 was completed on May 7, 1984. The aircraft was first certified in September 1985 and began operating in 2004. The latest variant being developed from the PC-9M is Pilatus PC-9Mk2.

Pilatus PC-9M advanced trainer

Pilatus PC-9M Specs

Pilatus PC-9M is an advanced version of PC-9. This aircraft has a wide dorsal fin to improve longitudinal stability, stall strips, new engines, and propeller control. At the bottom of the wing the aircraft is equipped with six hard points (three on each wing). These hard points can be mounted with two Rocket Podets, FN LAU 7 folding air fin rockets and two FN heavy machine guns (HMG). Each weapon can fire 250 rounds of ammunition.

Dimensions of Pilatus PC-9M include length 10.14 m, height 3.26 m, and wingspan 10.125 m. The aircraft's empty weight is around 1,781 kg and the maximum take-off weight (MTOW) is 3,200 kg. The aircraft is equipped with a retractable tricycle type landing gear.

Pilatus PC-9M specs

Pilatus PC-9M Engine and Performance

The Pilatus PC-9M is powered by a Pratt & Whitney Canada PT6A-62 single turboprop engine. The engine produces an output power of 857 kW to drive a four-bladed Hartzell aluminum propeller made of at a constant speed of 2,000 rpm. The engine has an epicyclic speed reduction gearbox to reduce propeller noise by optimizing output speed. This engine is also equipped with a one-stage axial and centrifugal multi-stage compressor, backflow burner and one-stage compressor turbine. The length and diameter of the engine are 1.79 m and 0.48 m, respectively.

Pilatus PC-9M aircraft can fly with a maximum speed of 593 km/ h and a cruising speed of 552 km/ h. The kiosk speed is 143 km/ h and can go up to 19.7 m/ s. The aircraft has a range of 1,593 km and a service ceiling of 11,580 m. The maximum endurance of the aircraft is 4 hours 30 minutes.

Pilatus PC-9M cockpit

Pilatus PC-9M Cockpit and Avionics

Pilatus PC-9M features a double glass cockpit with tandem seating configurations for pilots and co-pilots. The cockpit is equipped with a glass canopy to increase visibility. The Pilatus PC-9M cockpit is enhanced by the main flight display (PFD) and multi-function display (MFD), both of which provide clear visibility and display flight information. Engine monitoring, aircraft configuration, air pressure, and environmental control are available in the cockpit.

The Pilatus PC-9M avionics suite includes Visual Flight Rules (VFR) and Instrument Flight Rules (IFR) for navigation, communication and identification. Avionics suites installed in the cockpit include an electronic flight instrumentation system (EFIS), Head Up Display (HUD), On-board Oxygen Manufacturing System (OBOGS) and anti-G systems.

Pilatus PC-9M Price and Orders

The price of the latest Pilatus PC-9M advanced trainer aircraft is around US $ 7 million. In 1997, Croatia signed a contract with RAAF to supply three used Pilatus PC-9M aircraft. Slovenia ordered nine planes in December 1997. Oman bought 12 planes in January 1999. Ireland ordered eight planes in January 2003. Bulgaria bought 12 planes in 2004. Mexico was the last customer to receive two planes in September 2006.

Monday, 17 February 2020

Pilatus PC-7 MkII Specs, Interior, Cockpit and Price

01:00
Pilatus PC-7 MkII Specs, Interior, Cockpit and Price – Pilatus PC-7 MkII is a turboprop-engined basic trainer aircraft manufactured by Pilatus Aircraft of Switzerland. This aircraft is intended for ab initio training (from the start) and basic flight training for beginner pilots. It provides reliable and cost-effective training solutions for the world air force. This aircraft has been operated by the South African Air Force (SAAF), Indian Air Force (IAF), Botswana Defense Force (BDF), Royal Malaysian Air Force and Royal Brunei Air Force. More than 160 PC-7 MkII aircraft have been sold since it was introduced in 1994.

Pilatus PC-7 MkII basic trainer

Pilatus PC-7 MkII Specs

The PC-7 MkII aircraft was developed based on the advanced PC-9M trainer aircraft. It uses the fuselage and avionics of PC-9M. The aircraft has a modular design that allows system integration with minor modifications. Conventional systems used in aircraft ensure easy operation and maintenance. The dimensions of the PC-7 MkII aircraft cover a length of 10.8 m, a height of 3.26 m, and a wing span of 10.19 m and have a wingspan of 16.28 m². The aircraft's empty weight is 1,710 kg, while the maximum take-off weight (MTOW) is 2,250 kg.

Pilatus PC-7 MkII Engine and Performance

Pilatus PC-7 MkII is powered by Pratt & Whitney PT6A-25C single turboprop engine. The engine produces a maximum output power of a maximum power of 700 shp to drive the four-bladed Hartzell aluminum propeller. This engine offers lower operating costs than the PT6A-25A engine on a standard PC-7 aircraft. It was also equipped with a digital electronic engine control system.

PC-7 MkII aircraft can fly with a cruise speed of 448 km / h at sea level and a maximum operating speed of 556 km / h. The aircraft can ride at speeds of 14.79 m / s. The maximum range and maximum height of the aircraft are 1,500 km and 33,000 ft, respectively. The aircraft's takeoff and landing distances above the 15m obstacle to sea level are 457 m and 687 m, respectively. The maximum limit for certified g-loads from aircraft is + 7 g / -3.5g.

Pilatus PC-7 MkII specs

Pilatus PC-7 MkII Cockpit and Avionics

The PC-7 MkII aircraft is equipped with a glass cockpit that accommodates two crew members with a tandem configuration. The cockpit is equipped with ejection seats and glass canopies that offer unobstructed visibility for both crews. Ergonomically placed instruments, displays and controls make it easy to operate the aircraft at all stages of flight. The tandem layout also allows the instructor to monitor, assist, or override the student pilot's actions.

The PC-7 MkII avionics suite integrates the main flight display, multifunctional display, electronic flight instrumentation system, distance measuring equipment and automatic direction finder (ADF). This aircraft is also equipped with a communication suite, anti-g system, and oxygen-producing system installed (OBOGS).

Pilatus PC-7 MkII Price and Orders

The price of the latest Pilatus PC-7 MkII basic trainer aircraft is around US $ 3.9 million. SAAF became the first customer for the PC-7 MkII when it ordered 60 aircraft in 1993. Shipments ended with the delivery of the final aircraft in 2006. The PC-7 MkII aircraft in the SAAF service was designated the Pilatus Astra, due to the self-built avionics suite.

SAAF signed a contract with Pilatus Aircraft in October 2008 to improve the avionics of 35 Astra aircraft under the Ithambo Project. The first two Astra PC-7 MkII aircraft equipped with standard factory-made avionics were sent to SAAF in July 2010. The upgraded Astra aircraft was renamed PC-7 MkII, because it has standard avionics used throughout the world.

In May 2012, Pilatus Aircraft was awarded a $ 523 million contract by the Indian Air Force to send 75 PC-7 MkII trainer aircraft. The contract also includes options for additional aircraft plus an integrated ground-based training system and a logistical support package. The IAF received the first batch of PC-7 MkII aircraft in February 2013 and the remainder was shipped the following year.