Saturday, 29 February 2020

Piper PA-34 Seneca V Specs, Interior, Cockpit and Price

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Piper PA-34 Seneca V Specs, Interior, Cockpit and Price – The Piper PA-34 Seneca V is a lightweight, dual piston engined business aircraft manufactured by Piper Aircraft, United States. This is the latest variant for the PA-34 Seneca series aircraft, which includes PA-34 Seneca I, PA-34 Seneca II, PA-34 Seneca III, and PA-34 Seneca IV. Piper Aircraft launched the first Seneca V series production aircraft in 1997. The industry-proven design and smooth structure of the lightweight aircraft enabled it to carry out passenger transport, surveillance, reconnaissance and patrol missions. The aircraft can also be used for basic pilot training.
Piper PA-34 Seneca V aircraft

Piper PA-34 Seneca V Specs

The Piper PA-34 Seneca V airframe has a low wing configuration design, which allows for more lift and significant drag reduction. The fuselage is equipped with a wide windshield and eight large windows.

 Dimensions of the Piper PA-34 Seneca V include a length of 8.7 m, a height of 3 m, and a wing span of 11.9 m. The maximum takeoff weight and weight that are equipped with aircraft standards are 2,155 kg and 1,561 kg, respectively. The aircraft can carry a maximum of 604 kg of standard useful load, while the fuel tank is designed to carry 462 l of usable fuel.

Piper PA-34 Seneca V Engine and Performance

The Piper PA-34 Seneca V aircraft is powered by two Continental TSIO-360-RB engines equipped with an intercooler. Each engine produces a maximum power of 220 hp to drive the three-bladed McCauley Propeller propeller at constant speed. This aircraft can fly with a maximum speed of 370 km / h and a maximum range of 1,534 km with a 45-minute reserve. The aircraft requires a take-off distance of 520 m and a landing distance of 664 m. The service ceiling of the aircraft is 7,620 m, while the climbing rate is 1,455 ft / min.
Piper PA-34 Seneca V cockpit

Piper PA-34 Seneca V Cockpit and Avionics

The Piper PA-34 Seneca V cockpit is equipped with the Garmin G1000 avionics device which integrates a sophisticated communication and navigation system. High resolution screens provide environmental data, engine data, traffic, maps and graphics to increase the situational awareness of the crew. Further avionics suites include the GFC 700 autopilot system, digital audio panels, Garmin FliteCharts, transponders, electronic flight displays (EFD), air data computers and yaw dampening systems.

 The automatic flight control system (AFCS) in the aircraft ensures the safety of personnel on board by improving handling quality. The optional Garmin Synthetic Vision Technology (SVT) gives pilots a 3D picture of terrain, airports, water reserves, obstacles and traffic.

 The Piper PA-34 Seneca V aircraft is also equipped with a GWX 68 weather radar, a traffic advisory system and a warning and terrain system (TAWS). Other optional equipment and systems include the GSR 56 Iridum transceiver, BendixKing KR-87 ADF receiver, GDL 69SXM satellite radio, L3 WX-500 Stormscope and Vision 1000 flight data monitoring devices.
Piper PA-34 Seneca V interior

Piper PA-34 Seneca V Cabin and Interior

The Piper PA-34 Seneca V aircraft can accommodate six passengers, including a pilot. The spacious cabin has a natural leather seat interior. The cabin is equipped with large doors allowing easy movement of passengers and luggage. The aircraft can also be equipped with a built-in oxygen system.

Piper PA-34 Seneca V Price and Orders

The price of the latest Piper PA-34 Seneca V is around US $ 1.25 million. The Argentine Air Force intends to complete a contract with Piper for the supply of three aircraft. The first aircraft was sent in the second half of 2018. A Seneca V aircraft was inaugurated by the Bolivian Air Force in June 2018.
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Thursday, 27 February 2020

Cirrus Perception Specs, Sensor, Cockpit, and Price

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Cirrus Perception Specs, Sensor, Cockpit, and Price – Cirrus Perception is a special mission piston-engined aircraft developed by Cirrus Design Corporation (CDC), United States. The development of the aircraft is based on the Cirrus SR22/ SR22T aircraft. This aircraft can be used in command and control, law enforcement, military pilot training, search and rescue (SAR), VIP / captive transportation, border surveillance, mapping and photography, aerial surveys, disaster management and support missions. Cirrus Perception was introduced to the public and obtained certification from the Federal Aviation Administration (FAA) in July 2014.
Cirrus Perception special mission aircraft

Cirrus Perception Specs

The Cirrus Perception fuselage features a low-wing cantilever monoplane design and is made of composite material. The fuselage is equipped with a parachute recovery system known as the Cirrus Airframe Parachute System (CAPS). It integrates standard equipment, including front seat airbag seat belts, single movement power levers, double side yoke, dual alternators, advanced wheel fairing, high performance brakes, tubeless tires, and surface lighting lamps.

 The Cirrus Perception landing system is equipped with a non-retractable three-wheel landing gear, including a nose castering wheel and two controllable main wheels. The dimensions of the aircraft include a length of 7.92 m, height 2.7 m and a wing span of 11.68 m. The aircraft based on the SR22 fuselage has an empty weight of 1,028kg and can carry a useful maximum load of 605 kg.

Cirrus Perception Engine and Performance

The Cirrus Perception aircraft is powered by a 310 hp Continental IO-550-N engine or a 315 hp turbocharged TSIO-550-K engine. The engine drives a lightweight three-bladed composite Hartzell propeller. The aircraft can fly with a maximum cruising speed of 185 KTAS (340 km / h) and a stall speed calibrated air speed of 60 KCAS (104 km / h) with a flap. This special mission aircraft can ride at a speed of 6.45 m / s to reach a maximum height of 17,500 ft, and requires a 330 m take-off distance and a 359 m landing roll ground.

Cirrus Perception Cabin and Interior

Cirrus Perception aircraft can accommodate four passengers, including pilots and co-pilots. The cabin measures 124 cm wide and 127 m high. The aircraft cabin can be accessed through the large doors found on each side of the fuselage. The cabin has a USB power port, a standard leather interior, and UV Protected Windows.

Cirrus Perception Cockpit and Avionics

The Cirrus Perception cockpit is fully integrated with the Garmin Cirrus Perspective avionics system, which consists of a primary flight display (PFD), multi-function flight display (MFD), all-digital Bluetooth GMA 350c audio panel, keyboard controller, dual WAAS Radio GPS/ communication/ navigation, ADS-B transponders and emergency locator transmitters (ELT). The main screen measuring 10 in shows current moving maps, satellite weather data, synthetic vision, infrared enhanced vision system (EVS), terrain awareness, traffic data, fuel gauges, as well as engine and subsystem information.

 Cirrus Perception aircraft also feature the GFC700 digital autopilot which offers a direct flying experience. It is also equipped with a dual attitude and heading reference system (AHRS) system, and an electronic stability and protection (ESP) system.
Cirrus Perception sensor

Cirrus Perception Sensor

Cirrus Perception special mission aircraft are installed with the Cloud Cap TASE imaging package from UTC Aerospace Systems and FLIR Systems Star 380 HDC EO / IR systems. The TASE500 and TASE400 sensors on board offer sophisticated imagery, while the Star 380 HDC delivers ultra-far-infrared and electro-optical imaging capabilities for special mission operations.

 The open architecture of the sensor mounting system allows for the integration of sensors and imaging systems from leading sensor system integrators. Customers can choose various user stations and mission specific equipment and can erase / reconfigure the sensor circuit according to their needs.

Cirrus Perception Price

The price of the latest Cirrus Perception special mission aircraft is around US $ 950,000.
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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.
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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.
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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.
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Wednesday, 19 February 2020

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

01:00
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.
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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.
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Saturday, 15 February 2020

Pilatus PC-6 Porter Specs, Interior, Cockpit and Price

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Pilatus PC-6 Porter Specs, Interior, Cockpit and Price – Pilatus PC-6 is a light utility turboprop single-engine aircraft designed and manufactured by Pilatus Aircraft of Switzerland under the Fairchild Hiller license. This aircraft is designed to carry out various missions, including passenger and cargo transportation, paradropping, ambulances, desert and bush operations, search and rescue (SAR), surveillance, smuggling, goods trading, geographical analysis, and intelligence calls for surveillance air and border patrols . His take-off and landing capability (STOL) enables the aircraft to operate in all weather conditions and all terrain.

 Pilatus PC-6 aircraft made their first flights in 1961 and were operated by various operators throughout the world. This aircraft has 15 variants namely PC-6/350, PC-6/ A, PC-6/ A1, PC-6/ A2, PC-6/ B, PC-6/ B1, PC-6B2-H2, PC- 6/ C, PC-6/ C1, PC-6/ C2-H2, PC-6/ D-H3, AU-23A peace maker, OV-12, Chiricahua UV-20A, and PC-8 Twin Porters.
Pilatus PC-6 Porter

Pilatus PC-6 Specs

Pilatus PC-6 was built using semi-monocoque construction techniques. The fuselage is built with aluminum alloys and extruded. Metals used in construction are protected from corrosion by painting, painting before a rigid polyurethane-based external paint is applied. The dimensions of the PC-6 aircraft include a length of 11 m, height of 3.2 m, and wingspan of 15.87 m.

 The Pilatus PC-6 landing mechanism is equipped with low-pressure tires, twin disc brakes, and a high absorbency undercarriage that allows the aircraft to land on rigid, rough, short, sandy, rocky, soft or muddy airfields, and remote areas. It can also be mounted skis or floating type landing gear to support aircraft operations in snow fields, glaciers, and lakes.

 The aircraft is equipped with an infrared camera (FLIR), forward-looking, light and distance detection (LIDAR) and digital cameras when conducting search and rescue operations. Passenger seats in the cabin of the PC-6 aircraft can be replaced with two stretchers on the left and right side for ambulance missions. The PC-6 aircraft can accommodate ten passengers in a triple-bench configuration or seven passengers in a single seat during its operation as a passenger aircraft.

Pilatus PC-6 Engine and Performance

The Pilatus PC-6 is powered by Pratt & Whitney Canada PT6A-27 single turboprop engine. The engine produces an output power of 410 kW (550 hp) to drive the three-bladed Hartzell HC-B3TN-3D aluminum propeller. The propeller is equipped with anti-icing facilities and can rotate at a constant speed of 2,200 rpm. The length and diameter of the engine are 1.57 m and 0.48 m, respectively.

 Pilatus PC-6 aircraft can fly with a maximum speed of 244 km/ h and a cruising speed of 232 km/ h. The kiosk speed is 107 km/ h and can go up to 331 m/ min. The aircraft has a range of 1,612 km and a service ceiling of up to 8,197 m. The aircraft's empty weight is around 1,270 kg and the maximum take-off weight (MTOW) is 2,800 kg.
Pilatus PC-6 cockpit

Pilatus PC-6 Cockpit and Avionics

The Pilatus PC-6 cockpit is fully integrated with the advanced Garmin G950 avionics suite. This includes the main flight display (PFD) and multifunctional display (MFD) to show flight data input, making navigation easier for pilots. The cockpit is also equipped with dual control brakes, weather radar, oxygen system, eight outlet adapters, and high frequency radio. An autopilot system installed in the cockpit reduces pilot workload through its automatic function.

 The cockpit is equipped with two seats for pilots and co-pilots or passengers. The cockpit has doors on both sides that allow pilots to get on and board the plane quickly. The aircraft is also equipped with panoramic windows to provide clear visibility to pilots and co-pilots / passengers.
Pilatus PC-6 interior

Pilatus PC-6 Cabin and Interior

Pilatus PC-6 aircraft has a spacious and comfortable cabin with a volume of 3 m³. The cabin can accommodate ten passengers or 1,000 kg of goods. The cabin has two large sliding doors and a trapdoor as an option for loading and unloading of goods. The trap door takes 150 kg and can be closed or opened by pilots during surveillance and skydiving operations.

 This cabin has a camera installation, paracit, passenger seat, Pax cargo kit, rough crane bar and cabin ventilation with six outlets. It also combines two stretchers, nine binding points and three bench seats for different roles. The cabin can be easily converted to carry out various surveillance operations. Seats can be removed without design changes when additional space is needed for cargo transportation.

Pilatus PC-6 Price

The price of the newest Pilatus PC-6 Porter aircraft is around US $ 1.9 million. Until 2017, Pilatus Aircraft has built 595 PC-6 aircraft and all have been sent to various operators.
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Friday, 14 February 2020

Beechcraft Bonanza G36 Specs, Interior, Cockpit and Price

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Beechcraft Bonanza G36 Specs, Interior, Cockpit and Price – Beechcraft Bonanza G36 is a single engine aircraft manufactured by Hawker Beechcraft Corporation (HBC), a subsidiary of Textron Aviation. This aircraft was first produced under the name Beechcraft Bonanza A36 in 1947. In 2004, Raytheon enhanced the Bonanza A36 aircraft with an integrated glass cockpit along with the Garmin G1000 avionics suite. After upgrading, the name of the aircraft was changed to Beechcraft Bonanza G36 in April 2005. This aircraft was certified in November 2005. The inaugural flight of the Bonanza G36 was carried out in December 1945 and began operating in 1947.
Beechcraft Bonanza G36

Beechcraft Bonanza G36 Specs

The dimensions of the Beechcraft Bonanza G36 include a length of 8.39 m, a height of 2.62 m, and a wingspan of 10.21 m. The aircraft is equipped with TKS Flight Into Known Icing (FIKI) protection system to protect the fuselage, wings, tail surface, propeller, and windshield when operating in cold conditions. Besides that the aircraft is also combined with a tank full of ice protection liquid to provide continuous protection for up to two and a half hours.

 The Bonanza G36 aircraft operator is currently equipped with an advanced vision system (EVS), namely the EVS-100 and EVS-600. This system increases pilot visibility by eight to ten times during fog, fog, smoke and rainfall conditions. EVS gives pilots infrared images that turn darkness into daylight.

 The aircraft also includes a standby alternator and secondary backup battery to provide the electricity needed to the engine when the primary battery fails to function. The secondary backup battery can provide 30 minutes of electric power to the alternator and primary battery when power is lost. The Bonanza G36 is equipped with retractable and sturdy landing wheels for aero-dynamic efficiency and high operational air speed.

Beechcraft Bonanza G36 Engine and Performance

Beechcraft Bonanza G36 is powered by a single engine Teledyne Continental IO-550-B. The IO-550-B is a six-cylinder air-cooled engine fueled with an overhead valve design. The engine produces an output power of 300 hp to drive a three-bladed Hartzell constant speed propeller. Bonanza G36 aircraft can fly with a maximum cruise speed of 326 km / h. The aircraft can ride at a rate of 6.25 m / s. The range and ceiling of the aircraft service are 1,722 km and 5,639 m, respectively. The aircraft's take-off and landing distance are 583 m and 442 m, respectively.
Beechcraft Bonanza G36 cockpit

Beechcraft Bonanza G36 Cockpit and Avionics

The Beechcraft Bonanza G36 cockpit is fully integrated with the Garmin G1000 avionics suite. The cockpit is equipped with two high-resolution 10.3 in LCD screens consisting of a primary flight display (PFD) and multifunctional display (MFD). The screen provides flight data, communication and identification data, engine performance, and graphical navigation. The aircraft is equipped with a GFC 700 autopilot system to reduce pilot workload.

 Other avionics installed on the aircraft include a global positioning system (GPS) sensor, GTX 33 Mode-S transponder, engine control unit, dual navigation radio and communication, Jeppesen electronic graphics, traffic advisory system (TAS) and Class-awareness and warning systems terrain (TAWS). TAWS notifies pilots of potential conflicts with obstacles and terrain.
Beechcraft Bonanza G36 interior

Beechcraft Bonanza G36 Cabin and Interior

The Beechcraft Bonanza G36 cabin has a length of 3.84 m, width 1.07, and height of 1.27 m. The cabin has a 1.1 m x 0.8 m double door for passenger entry, a 0.93 m x 0.91 m one-piece front door for the passenger exit and two middle windows for the double emergency exit.

 The Beechcraft Bonanza G36 cabin can accommodate pilots and five passengers with more leg room for all passengers. The cabin interior includes four leather seats, an XM satellite entertainment system and a large luggage area that is fully accessible to passengers in flight. To improve passenger and pilot visibility, the cabin is equipped with a large one-piece round windshield and six very large side passenger windows.

Beechcraft Bonanza G36 Price and Orders

The price of the latest Beechcraft Bonanza G36 is around US $ 914,000. Lider Signatures SA (Lider) based in Brazil ordered three Beechcraft Bonanza G36 in October 2008 as part of a $ 200 million contract awarded to HBC. Lider has been an authorized dealer and service center for HBC since 1996. The contract also involved the supply of the following aircraft: three Hawker 4000, two Hawker 900XP, three Hawker 750, five Hawker 450XP, one Beechcraft King Air B200GT, four Beechcraft King Air C90GTi, two Beechcraft Baron G58 and three Beechcraft Bonanza G36.
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Thursday, 13 February 2020

Beechcraft Baron G58 Specs, Interior, Cockpit and Price

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Beechcraft Baron G58 Specs, Interior, Cockpit and Price – Beechcraft Baron G58 is a twin-piston engine manufactured by Hawker Beechcraft Corporation (HBC), a subsidiary of Textron Aviation. The first flight was made in June 1969 and began operating in 1970. This aircraft was first produced under the name Beechcraft Baron G55. However, in 2004 Raytheon upgraded the aircraft with an integrated glass cockpit along with the Garmin G1000 avionics suite. The aircraft's name was changed to Beechcraft Baron G58 in April 2005, and certified in December 2005. On June 21, 2010, the aircraft received certification from the Civil Aviation Administration of China (CAAC). In July 2010, the Beechcraft Baron G58 became the first HBC aircraft approved for operation at London City Airport.
Beechcraft Baron G58

Beechcraft Baron G58 Specs

The Beechcraft Baron G58 aircraft is equipped with an ice and rain protection system, which includes an automatic pneumatic shoe ice eraser, a standard electro-thermal propeller de-ice system, and a standard propeller warning propeller and fuel vents. The aircraft also includes a standby alternator and secondary backup battery to provide the electricity needed to the engine when the primary battery function fails. Some aircraft buses have increased the reliability and redundancy of the G58.

 The landing mechanism of the Beechcraft Baron G58 aircraft is equipped with a retractable landing gear that is controlled by throttle. The landing gear is equipped with an electromechanical extension and retraction system. The dimensions of the Beechcraft Baron G58 include a length of 9.09 m, a height of 2.97 m, and a wingspan of 11.53 m. It has luggage space that can hold up to 190.5 kg of luggage.

Beechcraft Baron G58 Engine and Performance

Beechcraft Baron G58 is powered by two Teledyne Continental IO-550-C piston engines. The IO-550-C engine is an air-cooled, six-cylinder, fuel-injection engine equipped with an overhead tilt valve design. Each engine can produce a maximum output power of 300 hp to drive a three-bladed McCauley constant speed propeller at a crankshaft speed of 2,700 rpm. Dry weight and the average engine are 188 kg and 210 kg respectively. Meanwhile the dimensions of the machine include a length of 1.1 m, height 0.5 m and width 0.85 m.

 Beechcraft Baron G58 aircraft can fly with a maximum speed of 385 km / h and a cruise speed of 361 km / h. It has a kiosk speed of 137 km / h, a maximum range of 2,741 km, and a service ceiling of 6,306 m. The aircraft can rise at the level of 8.43 m / s during take-off, and descend at 1.98 m / s during landing. The maximum take-off weight (MTOW) is 2,495 kg.
Beechcraft Baron G58 cockpit

Beechcraft Baron G58 Cockpit and Avionics

The Beechcraft Baron G58 cockpit is fully integrated with the Garmin 1000 avionics suite. The Garmin G1000 avionics suite includes a primary flight display (PFD), multi-function display (MFD), digital attitude heading reference system (AHRS) and air data computer (ADC) to provide attitude and air data information to the system. The cockpit has two 10.3 in high resolution liquid crystal (LCD) screens for displaying flight data, engine performance and graphical navigation. The GFC 700 autopilot system is installed in the cockpit to reduce pilot workload.

 Other avionics installed on the Baron G58 aircraft include a global positioning system (GPS) sensor, transponder, engine control unit, GWX-68 color weather radar, Stormscope WX-500, distance measuring equipment (DME), traffic advisory system (TAS), and Class-B warning system and warning system (TAWS) to inform pilots of potential conflicts with obstacles and terrain. The aircraft is also equipped with a Wide Area Augmentation System (WAAS), terrain warning database, GTX 33ES Mode-S transponder, GDU 104x Multifunction Multifunction Display, and GRC10 and GRT10 wireless remote control systems.
Beechcraft Baron G58 interior

Beechcraft Baron G58 Cabin and Interior

Beechcraft Baron G58 has a spacious and comfortable cabin. The cabin has a length of 3.84 m, width 1.07 and a height of 1.27 m. Cabin entrance and exit consists of double doors 1.1 m x 0.8 m for passenger entry, one-piece front door 0.93 m x 0.91 m for passenger exit, and two middle windows for some emergency exits. The cabin can accommodate pilots and five passengers with ample leg room for all passengers.

 The Beechcraft Baron G58 oval-shaped cabin is also equipped with an XM satellite entertainment system and nose trunk area to place luggage, which is fully accessible to passengers during the flight. To improve passenger and pilot visibility, the cabin is equipped with a large one-piece round windshield and six very large side passenger windows.

Beechcraft Baron G58 Price and Orders

The price of the latest Beechcraft Baron G58 is around US $ 1.48 million. As of 2007, around 38 G58 aircraft had been sent to different customers throughout the world. On May 20, 2008, Artur Przygoda from Poland awarded a contract to Hawker Beechcraft Corporation to supply the European Aviation Safety Authority (EASA) Baron G58 aircraft. Deliveries were made in May 2009.
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Tuesday, 11 February 2020

Beechcraft King Air 350ER Specs, Interior, Cockpit, and Price

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Beechcraft King Air 350ER Specs, Interior, Cockpit, and Price – King Air 350ER is a multipurpose dual-engine turboprop aircraft manufactured by Hawker Beechcraft Corporation (HBC), a subsidiary of Textron Aviation. This aircraft was developed to carry out various special missions for the military and law enforcement. Aircraft can be deployed for search and rescue (SAR), intelligence, reconnaissance, target acquisition, military transportation / utilities, air patrols, fisheries inspection, training, pollution monitoring, seaway / cruise line surveillance, law enforcement, air ambulance missions and operations other specialty.
Beechcraft King Air 350ER

Beechcraft King Air 350ER Specs

The King Air 350ER aircraft was developed based on the King Air 350i, which combines advanced technology and unique and flexible mission packages. This makes the aircraft very reliable and can last for more than 12 hours with extended range.

 The dimensions of the King Air 350ER aircraft cover an overall length of 14.22 m, a height of 4.37 m and a wing span of 17.65 m. It has a maximum ramp weight of 7,530 kg, a take-off / landing weight of 7,484 kg and a maximum zero fuel weight of 7,110 kg. The aircraft can carry a maximum payload of up to 1,361 kg and a useful payload of up to 2,903 kg. The maximum fuel weight that can be carried by the aircraft is 2.355 kg.

Beechcraft King Air 350ER Engine and Performance

Beechcraft King Air 350ER is powered by two Pratt & Whitney PT6A-60A turboprop engines, each of which produces an output power of 1,050 hp. The engine moves a reversible four-bladed pitch pitch propeller with a diameter of 266.7 cm supplied by Hartzell. This aircraft can fly with a maximum cruise speed of 578 km / h with a maximum range of up to 4,361 km. The flight service ceiling is 10.66 m.
Beechcraft King Air 350ER cockpit

Beechcraft King Air 350ER Cockpit and Avionics

The King Air 350ER cockpit incorporates Rockwell Collins Pro Line Fusion's sophisticated avionics range. The cockpit is equipped with electro-optical / infrared (EO / IR) imaging and radome radar search systems for detection, tracking and surveillance operations. The aircraft is also equipped with a lightweight, high-performance, multi-functional Lynx-2 synthetic aperture radar unit developed by General Atomics Aeronautical Systems. The radar operates in synthetic aperture radar (SAR) mode and ground movement target mode (GMTI), offering a range of 80 km. This provides high resolution search and rescue imagery in all weather conditions.
Beechcraft King Air 350ER interior

Beechcraft King Air 350ER Cabin and Interior

Beechcraft King Air 350ER has a spacious cabin that offers superior comfort and convenience. The cabin is 5.94 m long, 1.45 m high, and 1.37 m wide. It can accommodate two crew members and up to eleven passengers. It can optionally be equipped with two additional folding chairs. The cabin can be reconfigured according to the mission that will be run.

Beechcraft King Air 350ER Price and Orders

The price of the latest Beechcraft King Air 350ER is around US $ 7.8 million. Hawker Beechcraft received a contract from the Iraqi Air Force to send five King Air 350ER aircraft for intelligence, surveillance and reconnaissance missions, in March 2007.

 The US Air Force gave Hawker Beechcraft a $ 171 million order for 23 King Air 350ER aircraft in November 2008. The first aircraft was delivered in April 2009. The USAF gave a further order of $ 45 million for six additional aircraft to support the Liberty Project in October 2009 Meanwhile in November 2009, Hawker Beechcraft also sent the first of four modified King Air 350ER aircraft to the Ministry of Defense (Department of Defense).

 The Mexican Navy Secretaría de Marina (SEMAR) signed a contract with Beechcraft for the delivery of four aircraft in early 2014. In July 2014, the first aircraft were sent to SEMAR, as part of the ongoing Mexican Navy fixed wing modernization program. The second plane was sent in August 2014, while the rest were sent in early 2015.
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Saturday, 8 February 2020

KB SAT SR-10 Jet Trainer Specs, Engine, and Price

16:06
KB SAT SR-10 Jet Trainer Specs, Engine, and Price – KB SAT SR-10 is a medium sized single-engine jet trainer designed and developed by Modern Aviation Technologies (KB SAT) to meet Russian Air Force pilot training requirements. This aircraft can be used for primary and secondary pilot training, as well as to improve military and commercial pilot piloting skills. This is being developed for the Russian Air Force and for export.

 The first test flight of the SR-10 prototype aircraft was carried out at an airport near Vorotynsk in the Kaluga region in December 2015. During the first flight test program, the aircraft's qualitative performance including certain flight characteristics, stability and control, system operation and equipment were assessed. This aircraft is being further tested at the Gromov Flight Research Center in Moscow.
KB SAT SR-10 Jet Trainer

KB SAT SR-10 Specs

the SR-10 jet trainer has an integrated aerodynamic design that allows it to do safe aerobatics. The aircraft comes with moderate wings of inverted strokes which provide greater maneuverability. The main wing is mounted at the center of the fuselage and is swept forward at an angle of 10°. The overall dimensions of the SR-10 aircraft include a length of 9.59 m, a height of 3.55 m, and a wing width of 8.40 m. This aircraft has a maximum take-off weight of 2,700 kg, a normal take-off weight of 2,400 kg, and a normal landing weight of 2,000 kg.

 The SR-10 fuselage is built from modern composite materials. The aircraft uses gliders to reduce weight and increase resources in the fuselage. The company claims that this aircraft has very low operating costs compared to other jet trainers. The aircraft is equipped with a retractable tri-cycle landing gear consisting of a single wheel attached to the nose and two main wheels under the fuselage.
KB SAT SR-10 engine

KB SAT SR-10 Engine and Performance

The SR-10 jet trainer prototype is powered by a single Ivchenko AI-25TL turbofan engine that produces power of 16.87 kN (3,790 lb). Meanwhile, the production aircraft are powered by a 1.95 m AL-55 turbofan engine developed by Saturn's NPO, which produces a takeoff thrust of 3,880 lb.

 the SR-10 jet trainer can fly with a cruising speed of 520 km/ h, a maximum air speed of 900 km/ h, and a maximum maneuver speed of 700 km/ h. The aircraft has a maximum range of 1,500 km and a service ceiling of 6,000 m with a climbing rate of 60 m/ s. The minimum rotation radius is 290 m and the maximum rational bank speed is 7 r/ s.
KB SAT SR-10 cockpit

KB SAT SR-10 Cabin and Cockpit

SR-10 jet trainer is equipped with dual cabins which provide comfort for the flight crew. The cabin accommodates two crew members, namely a pilot and an instructor, with dual control in tandem configuration. The pilot has unobstructed views through a large canopy. It was equipped with a Class 0-0 ejection seat in the cabin to ensure safety for the crew at all altitudes and piloting speeds.

KB SAT SR-10 Price

The price of the KB SAT SR-10 jet trainer is around US $ 8.32 million. The Russian Ministry of Defense has allocated 2.5 bn RUR ($ 34 million) for the SR-10 development project.
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Saturday, 1 February 2020

Gulfstream G700 Vs Bombardier Global 7500, Which Business Jet is Better?

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Gulfstream G700 Vs Bombardier Global 7500, Which Business Jet is Better? – Gulfstream G700 and Bombardier Global 7500 are the mainstay business jets specifically developed by each manufacturer to meet the demands of operators in the long distance aviation sector. Both planes have a range that can connect pairs of cities such as Los Angeles to Sydney or Beijing to Cape Town.

 The Gulfstream G700 aircraft was developed based on the success of 500+ G650 sales that revolutionized business aviation with its speed and range. Whereas Bombardier Global 7500 is one of the most anticipated business jets ever, with the longest range and longest cabin produced by the manufacturer.
Gulfstream G700 Vs Bombardier Global 7500

Dimensions of the Gulfstream G700 Vs Bombardier Global 7500

Dimensions of the Gulfstream G700 include a length of 33.48 m, a height of 7.75 m, a wingspan of 31.39 m and a loading capacity of 2,896 kg. Meanwhile, the Bombardier Global Dimension 7500 covers a length of 33.71 m, a height of 8.14 m, a wingspan of 31.79 m and a maximum load that can be transported is 2,585 kg.

Cabin of Gulfstream G700 Vs Bombardier Global 7500

Both of these business jets were built specifically with a very large cabin volume. The Gulfstream G700 cabin is 19.41 m long, 2.49 m wide and 1.91 m high. The cabin has five separate zones. Meanwhile, the Bombardier Global 7500 cabin is 18.17 m long, 2.49 m wide and 1.91 m high with four separate zones. Although the G700's cabin is longer, taller and wider than the Global 7500 cabin, both planes can carry 19 passengers.

Engine and Performance of Gulfstream G700 Vs Bombardier Global 7500

The Gulfstream G700 is powered by two Rolls-Royce Pearl 700 engines, each of which can produce 18,250 lb of thrust. Meanwhile, the Bombardier Global 7500 is powered by two GE Passport turbofan engines, each of which provides a thrust of 16,500 lb. Although there are differences in power produced by the engine on each plane. However, both planes were able to fly with the same maximum speed of Mach 0.925 (1.142 km/ h) and the cruising speed of Mach 0.9 (1.073 km/ h).

Range of Gulfstream G700 Vs Bombardier Global 7500

The maximum range of the Gulfstream G700 aircraft is 7,500 nm, while the Global 7500 has a maximum range of 7,700 nm. There was only a difference of 200 nm range between the two planes, with Global 7500 winning this round. But of course this has been anticipated by Gulfstream by developing a remote version, the G700ER.

 Please note that even though the maximum range of Bombardier Global 7500 recorded is 7,700 nm. However, in early October 2019, the aircraft flew non-stop between Detroit and Sydney with a range of more than 8,200 nm. This is the longest flight ever recorded by a specially created business jet.

Price of Gulfstream G700 Vs Global Bombardier 7500

The Gulfstream G700 is priced at US $ 75 million, while Bombardier Global 7500 is priced at US $ 72.8 million. The G700 is only 3% more expensive than the Global 7500.

 In the end, the two planes have identical max speeds, high speeds, and long distance speeds. Bombardier Global 7500 has a cheaper price and flies even further. On the other hand, the Gulfstream G700 has a larger cabin.
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