Saturday, 14 March 2020

Boeing 737-900 Next-Generation Specs, Interior, Cockpit, and Price

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Boeing 737-900 Next-Generation Specs, Interior, Cockpit, and Price – The Boeing 737-900 is the largest aircraft variant of the Boeing 737 Next-Generation (NG) family. This aircraft was launched in 1997 and made its first flight on 3 August 2000. The Boeing 737-900 began operating in May 2001.

In July 2005, Boeing launched the 737-900ER with an increased range and passenger capacity. The Boeing 737-900 ER is a development version of Boeing Next-Generation which operates in Indonesian airports. Lion Air Indonesia is a launch customer with 175 aircraft orders.

Boeing 737-900 Next-Generation

Boeing 737-900 Next-Generation Specs

The Boeing 737-900 fuselage was built using safe aluminum material. The aircraft wing has a fail-safe design with an aluminum alloy structure with corrosion resistant leather. Nosecone fairing, wings and fuselage, fin tips, fairing of flap actuators and other non-pressure components are constructed of glass fiber and carbon reinforced plastic (GFRP and CFRP). The back of the engine nacelles is built from graphite, Kevlar and glass fiber composites. Overall, the dimensions of the Boeing 737-900 include 42.1 m in length, 12.5 m in height, and 35.8 m in wingspan.

The landing system of the Boeing 737-900 is a three-wheeled hydraulic retractable landing gear type wheel. The gears are equipped with oleo-pneumatic shock absorbers designed by Boeing. The main wheel pulls in with the wheels forming a well seal; the well has no door. The main wheels are equipped with Honeywell or Goodrich wheel brakes. Twin nose wheel pulled forward.

Boeing 737-900 Next-Generation Engine and Performance

The Boeing 737-900 is powered by two CFM56-7B27 turbofan engines supplied by CFM International. Each engine can produce a thrust of 121.4 kN. The machine is supplied by CFM International. Each engine is mounted on a pod engine under the wing. The aircraft is equipped with an additional Honeywell 131-9B power unit, which provides 90 kVA and air start capability.

Noise on the ground is reduced to 12dB by installing a new diffuser duct and dampers on the cooling vents on additional power units. A new quiet operating fan has been installed in the environmental control system and in the electronic cooling system.

Boeing 737-900 can fly with a maximum speed of 876 km / h and a cruising speed of 823 km / h. The fuel capacity that can be carried by the aircraft is 29,660 L. The aircraft has an empty weight of 44,676 kg and a maximum take-off weight of 85,139 kg. The aircraft can cover a range of up to 6.045 km.

Boeing 737-900 interior

Boeing 737-900 Next-Generation Cabin and Interior

The Boeing 737-900 cabin can accommodate 178 passengers in a two class configuration, usually arranged with four first class passengers following and six tourist class passengers following. The cabin has a maximum capacity of 220 seats. Air-conditioned cab with an air cycle environmental control system. Airstairs is optional for the front cabin, which allows the aircraft to operate in an airport measuring conveyor.

Boeing 737-900 cockpit

Boeing 737-900 Next-Generation Cockpit and Avionics

The Boeing 737-900 cockpit accommodates pilot and co-pilot. The cockpit is equipped with a Common Display System (CDS) from Honeywell Air Transport Systems which combines six flat panel liquid crystal displays. The CDS software can be programmed to enable the presentation of data in the replication format of the main Boeing 777 electronic flight system and navigation and navigation display.

Boeing 737-900's cockpit has also been equipped with Head Up Display (HUD). This equipment is usually used on military aircraft. Its function is to facilitate the pilot in determining the tilt of the aircraft both vertically and horizontally. In addition, this aircraft can be equipped with an optional global positioning system, satellite communications, and dual flight management systems.

Boeing 737-900 Next-Generation Price and Orders

The price of the latest Boeing 737-900 Next-Generation aircraft is around US $ 112.6 million. Alaska Airlines is an initial customer with orders for ten aircraft with additional optional. Total orders are for 244 aircraft which also include: SpiceJet from India, Sky Airlines from Turkey, Continental, GECAS. Meanwhile, orders for Boeing 737-900ER aircraft include Lion Air in June 2010, Israeli national carrier EL AL in March 2011, Delta Air Lines and Korean Air in August 2011, as well as various other airlines around the world.

Thursday, 12 March 2020

Boeing 737-800 Next-Generation Specs, Interior, Cockpit, and Price

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Boeing 737-800 Next-Generation Specs, Interior, Cockpit, and Price – The Boeing 737-800 is a medium sized twin engine aircraft that belongs to the Boeing 737 Next-Generation (NG) family. This aircraft is the basis for Boeing Business Jet 2 (BBJ2). The 737-800ERX variant was chosen as the fuselage for the new US Navy Multi-Mission Maritime (MMA) aircraft, designated by P-8A, in June 2004. It became one of the best-selling types of jet aircraft of all time.

The first flight for the Boeing 737-800 took place in February 1997. The aircraft entered service with Hapag-Lloyd launch customers in 1998. This aircraft can fly farther and accommodate more passengers than the previous version. The Boeing 737-800 was built to compete primarily with the Airbus A320.

Boeing 737-800 Next-Generation

Boeing 737-800 Next-Generation Specs

The Boeing 737-800 fuselage was built using safe aluminum material. The aircraft wing has a fail-safe design with an aluminum alloy structure with corrosion resistant leather. Nosecone fairing, wings and fuselage, fin tips, fairing of flap actuators and other non-pressure components are constructed of glass fiber and carbon reinforced plastic (GFRP and CFRP). The back of the engine nacelles is built from graphite, Kevlar and glass fiber composites. Overall, the dimensions of the Boeing 737-800 include 39.5 m in length, 12.5 m in height, and 35.8 m in wingspan.

The Boeing 737-800 aircraft landing system is a landing gear that can be hydraulically pulled on a tricycle type. The gears are equipped with oleo-pneumatic shock absorbers designed by Boeing. The main wheel pulls in with the wheels forming a well seal; the well has no door. The main wheels are equipped with Honeywell or Goodrich wheel brakes. Twin nose wheel pulled forward.

Boeing 737-800 Next-Generation Engine and Performance

The Boeing 737-800 is powered by two CFM56-7B24 International CFM turbofan engines, each of which produces a thrust of 110 kN to 120 kN. Each engine is mounted on a pod engine under the wing. The aircraft is equipped with an additional Honeywell 131-9B power unit, which provides 90 kVA and air start capability.

Noise on the ground is reduced to 12 dB by installing a new diffuser channel and dampers on the cooling vents on additional power units. A new quiet operating fan has been installed in the environmental control system and in the electronic cooling system.

Boeing 737-800 can fly with a maximum speed of 876 km / h and a cruising speed of 842 km / h. The capacity of the fuel that can be carried by the aircraft is 26,025 l. The aircraft has an empty weight of 41,413 kg and a maximum take-off weight of 79,010 kg. The aircraft can cover a range of up to 2,935 nmi (5,436 km).

Boeing 737-800 interior

Boeing 737-800 Next-Generation Cabin and Interior

The Boeing 737-800 cabin can accommodate 162 passengers in a two-class configuration, usually arranged with four first class passengers following and six tourist class passengers following. The maximum capacity that can be accommodated by the cabin is 189 seats. Air-conditioned cab with an air cycle environmental control system. Airstairs is optional for the front cabin, which allows the aircraft to operate in an airport measuring conveyor.

Boeing 737-800 cockpit

Boeing 737-800 Next-Generation Cockpit and Avionics

The Boeing 737-800 cockpit accommodates pilot and co-pilot. The new cockpit is equipped with a Common Display System (CDS) from Honeywell Air Transport Systems which combines six flat panel liquid crystal displays. The CDS software can be programmed to enable the presentation of data in the replication format of the main Boeing 777 electronic flight system and navigation display.

Boeing 737-800 cockpit has also been equipped with Head Up Display (HUD). This equipment is usually used on military aircraft / combat aircraft. Its function is to facilitate the pilot in determining the plane's tilt both vertically and horizontally. In addition, this aircraft can be equipped with an optional global positioning system, satellite communications, and dual flight management systems.

Boeing 737-800 Next-Generation Price and Orders

The price of the latest Boeing 737-800 Next-Generation aircraft is around US $ 106.1 million. To date, more than 4,000 737-800 aircraft have been ordered and operate with various airlines throughout the world. Major customers include American Airlines, Delta Airlines, Ryan Air, Qantas, Virgin Blue, Air Europa, Hainan Airlines, Shandong Airlines, GOL, Alaskan Airlines, Air China, Air Berlin, Malaysia Airlines and Garuda Indonesia.

Tuesday, 10 March 2020

Boeing 737-700 Next-Generation Specs, Interior, Cockpit, and Price

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Boeing 737-700 Next-Generation Specs, Interior, Cockpit, and Price – The Boeing 737-700 is a medium sized twin engine aircraft that belongs to the Boeing 737 Next-Generation (NG) family. The first flight was made in February 1997 and entered service with the launch customer of Southwest Airlines in 1998. This aircraft allowed the airline to provide domestic routes and short-haul international flights for more than 30 years.

The Boeing 737-700 is the basis for the Boeing (BBJ) business jet. There is also a conversion version, 737-700C, which is offered in all passengers or all cargo layouts and ordered by the US Naval Reserve (designated C-40A Clipper). In January 2006, Boeing launched the long-range version, 737-700ER. The 737-700ER aircraft has a 737-700 fuselage with landing wings and 737-800 wheels, expanding its range by 3,972 km (2,145 nmi).

Boeing 737-700 Next-Generation

Boeing 737-700 Next-Generation Specs

The Boeing 737-700 fuselage was built using safe aluminum material. The aircraft wing has a fail-safe design with an aluminum alloy structure with corrosion resistant leather. Nosecone fairing, wings and fuselage, fin tips, fairing of flap actuators and other non-pressure components are constructed of glass fiber and carbon reinforced plastic (GFRP and CFRP). The back of the engine nacelles is built from graphite, Kevlar and glass fiber composites. Overall, the dimensions of the Boeing 737-700 include 33.6 m in length, 12.5 m in height, and 35.8 m in wingspan.

The landing system of the Boeing 737-700 is a landing gear that can be pulled hydraulically into a tricycle type. The gears are equipped with oleo-pneumatic shock absorbers designed by Boeing. The main wheel pulls in with the wheels forming a well seal; the well has no door. The main wheels are equipped with Honeywell or Goodrich wheel brakes. Twin nose wheel pulled forward.

Boeing 737-700 Next-Generation Engine and Performance

The Boeing 737-700 is powered by two CFM International CFM-56 turbofan engines, each generating thrust of 10.890 kg. Each engine is mounted on a pod engine under the wing. The aircraft is equipped with an additional Honeywell 131-9B power unit, which provides 90 kVA and air start capability.

Noise on the ground is reduced to 12dB by installing a new diffuser duct and dampers on the cooling vents on additional power units. A new quiet operating fan has been installed in the environmental control system and in the electronic cooling system.

Boeing 737-700 can fly with a maximum speed of 876 km/ h and a cruising speed of 828 km/ h. The capacity of the fuel that can be carried by the aircraft is 26,025 l. The aircraft has an empty weight of 38,147 kg and can cover a range of up to 6,370 km.

Boeing 737-700 interior

Boeing 737-700 Next-Generation Cabin and Interior

The Boeing 737-700 cabin can accommodate 126 passengers in a two class configuration, usually arranged with four first class passengers following and six tourist class passengers following. The maximum capacity that can be accommodated by the cabin is 149 seats. Air-conditioned cab with an air cycle environmental control system. Airstairs is optional for the front cabin, which allows the aircraft to operate in an airport measuring conveyor.

Boeing 737-700 cockpit

Boeing 737-700 Next-Generation Cockpit and Avionics

The Boeing 737-700 cockpit accommodates pilot and co-pilot. The cockpit is equipped with a Common Display System (CDS) from Honeywell Air Transport Systems which combines six flat panel liquid crystal displays. The CDS software can be programmed to enable the presentation of data in the replication format of the main Boeing 777 electronic flight system and navigation and navigation display.

The cockpit can also be installed head up screen as an option. In addition, this aircraft can be equipped with an optional global positioning system, satellite communications, and dual flight management systems.

Boeing 737-700 Next-Generation Price and Orders

The price of the latest Boeing 737-700 Next-Generation aircraft is around 89.1 million. In August 2011, Boeing sent 737-700 to Xiamen Airlines. This Next-Generation aircraft features a high-altitude / high-temperature package and a Boeing Sky Interior.

Sunday, 8 March 2020

Boeing 777-200LR Specs, Interior, Cockpit and Price

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Boeing 777-200LR Specs, Interior, Cockpit and Price – The Boeing 777-200LR is an ultra-long-range aircraft designed by the Boeing Company, United States to be the long-haul aircraft in the world. The aircraft program was originally known as 777-200X and was launched in February 2000. Work on the aircraft was stopped in October 2001 but resumed in March 2003.

The first Boeing 777-200LR flight took place in March 2005. In November 2005, this aircraft achieved a world record for commercial non-stop flights with a distance of 21,601 km (11,664 nmi) from Hong Kong to London Heathrow.

Boeing 777-200LR jetliner

Boeing 777-200LR Specs

The fuselage is built using aluminum alloys and composites. It displays a twin-aisle cabin configuration. The dimensions of the Boeing 777-200LR include a length of 63, 7 m, a height of 18.6 m, and a wingspan of 64.8 m. The aircraft is also equipped with tapered wingtip extensions to reduce takeoff distance, grade performance and fuel efficiency.

The Boeing 777-200LR has a retractable tricycle type landing gear supplied by Measco and Messieur Bugatti. The main landing gear is equipped with Honeywell Carbenix 4000 brakes. Initial activation of the brakes during transport uses brakes to the group alternating from just three wheels to minimize wear on the brakes. Two-wheeled nose and can be controlled. The rear axle control of the steering wheel is automatically connected to the steering angle of the nose gear.

Boeing 777-200LR specs

Boeing 777-200LR Engine and Performance

The Boeing 777-200LR is powered by two GE90-115BL turbofan engines developed by General Electric, which produce a thrust of 511 kN (115,000 lb). The engine is mounted in a pod under the wingtip just like any commercial aircraft.

The main fuel tank is installed in the wing torsion box with a spare tank and spikes on the inner side of the wing. The Boeing 777-200LR has an additional fuel tank in the rear cargo space to bring the total fuel capacity to 195,285 liters. This aircraft can fly with a maximum cruise speed of 945 km / h and cover a range of up to 8,555 nmi (15,843 km). The aircraft has a service sky of 43,100 ft.

Boeing 777-200LR cockpit

Boeing 777-200LR Cockpit and Avionics

The Boeing 777-200LR cockpit accommodates two pilots. The cockpit is equipped with an electronic flight information system of five 8 in (203 mm) liquid crystal screens, including two main flight screens, two navigation screens, and one engine indication and crew warning system (EICAS).

The central control panel between the two pilots has three multipurpose control units and a display unit for aircraft information management systems, information systems, flight management functions, thrust control and communication.

The Boeing 777-200LR has fly-by-wire control with flight envelope protection and pilot functions and automatic stabilization. The fly-by-wire system sends back-driven signals to the steering wheel and pilot control column to give pilots sensory awareness about automatic system activity. This aircraft has a triple-redundant digital autopilot and flight director designed by Rockwell Collins.

The Boeing 777-200LR avionics suite includes an ARINC 629 digital data bus that is connected to the main and standby navigation system. The navigation system includes ADIRS Honeywell air data and an inertia reference system with a six-ring laser gyroscope, Honeywell field impact avoidance system (TCAS) and global channel positioning systems for Honeywell 12 channel channels and BAE Systems. The aircraft is also equipped with Honeywell weather radars and Honeywell and Racal satellite communication systems.

Boeing 777-200LR interior business class

Boeing 777-200LR Cabin and Interior

The Boeing 777-200LR cabin has twin aisle configurations that can accommodate up to 317 passengers in 2 classes. The cabin is equipped with a flight crew rest area in the form of two beds mounted on the port side of the flight deck. An optional installation is the rest of the crew module on the lower floor. The crew rest module holds six beds and occupies the same floor area as a standard cargo pallet.

Boeing 777-200LR Price and Orders

The price of the latest Boeing 777-200LR is around US $ 346.9 million. The launch customer is Pakistan International Airlines (PIA), which received the first 777-200LR in February 2006. Until now the aircraft has been sent and operates with various airlines including EVA Airways, Air India, Qatar Airways, ILFC, Jet Airways, Emirates, Air Canada and Air India.

Qatar Airways signed an agreement worth $ 501 million with Boeing in July 2010 to obtain two additional Boeing 777-200LR. In November 2010, Boeing sent 777-200LR aircraft to Ethiopian Airlines. The airline received its fifth aircraft in September 2011.

Friday, 6 March 2020

Boeing 777-9X Specs, Interior, Cockpit and Price

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Boeing 777-9X Specs, Interior, Cockpit and Price – The Boeing 777-9X is a twin aisle commercial aircraft developed and produced by the Boeing Company, United States. This aircraft is the second variant in the Boeing 777X family after the 777-8X variant. The Boeing 777-8X will be a replacement for the 777-300ER version while the Boeing 777-9X will be an expanded variant.

The aircraft development program was launched in November 2013, while aircraft production began in 2017. The first flight of the Boeing 777-9X was carried out on January 25, 2020. This aircraft will be the largest and most efficient twin-engined jet aircraft in the world competing with the Airbus A350XWB. The aircraft is scheduled to enter service in 2020.

Boeing 777-9X largest aircraft

Boeing 777-9X Specs

The Boeing 777-9X design was carried out by the Boeing engineering team based in Charleston, Huntsville, Long Beach, Philadelphia and St. Louis, USA, with the help of the Boeing Design Center in Moscow. It was designed to be the most sophisticated commercial aircraft and saves fuel by up to 12 percent, thanks to commercial fuel-efficient engines and environmentally friendly emission standards that greatly reduce carbon dioxide emissions. The Boeing 777-9X will offer the lowest operating costs per seat of all commercial aircraft.

The Boeing 777-9X fuselage is built from an advanced aluminum-lithium alloy composite. This uses a higher proportion of composite materials in construction than other aircraft models currently, in line with technological improvements. The aircraft's wings are equipped with wingtips that can be folded to improve aerodynamics. The overall dimensions of the Boeing 777-9X cover a length of 76.72 m, a wingspan of 71.75 m, and a height of 19.7 m.

Boeing 777-9X specs

Boeing 777-9X Engine and Performance

The Boeing 777-9X is powered by two GE9X turbofan engines supplied by GE Aviation. Each engine will produce 99,500 lb of thrust. The aircraft can fly with a maximum speed of 850 km / h with a range of up to 7,285 nmi (13,500 km). The aircraft has an empty weight of 255,000 kg (562,000 lb) and a maximum take-off weight of 351,534 kg (775,000 lb).

Boeing 777-9X interior business class

Boeing 777-9X Cabin and Interior

The Boeing 777-9X can accommodate 426 in a two class configuration. The 5.96 m wide modern cabin has large windows, new lighting and new architecture that will increase passenger comfort during flights. The wider cab installs 18.0 wide seats in economy class 10-parallel arrangements. The cabin will have bigger windows, higher ceilings, more humidity, and reduce cabin height to 1,800 m. Interior cabin open LED modern ceiling.

Boeing 777-9X is equipped with a large cabin window, which is larger than the window found on other types of aircraft. In addition, the window also has a higher size, thus increasing comfort while watching, without the need to bow your head or lean at an uncomfortable angle. Windows Equipped with Gentex technology which can be dimmed electronically.

Boeing 777-9X cockpit

Boeing 777-9X Cockpit and Avionics

The Boeing 777-9X cockpit imported a number of flight control systems from the Boeing 787 Dreamliner. The cockpit is equipped with a touch screen replacing the cursor control device and folding wingtip control. The 777X program will also feature a general cockpit and type-rating, which allows pilots to fly both of them. In addition, the 777-9X cockpit features a touch screen for entering and changing flight data and a special folding wing switch on the overhead panel.

Boeing 777-9X is equipped with the latest generation of Smoother Ride technology which was previously introduced in the 787 Dreamliner. Smoother Ride technology is like a stability control system in a car, which reduces the impact of turbulence when the aircraft enters airspace with changes in air pressure and temperature. When a plane experiences turbulence, hundreds of sensors detect changes and provide data to a special computer that tells flight controls to reduce the impact of turbulence felt by passengers.

Boeing 777-9X Price and Orders

The price of the latest Boeing 777-9X is around US $ 442.2 million. Emirates Airlines ordered $ 55.6 billion consisting of 150 Boeing 777X aircraft, including 115 Boeing 777-9X and 35 Boeing 777-8X at Dubai Airshow in November 2013. Boeing also received orders for 50 aircraft from Qatar Airways and 25 aircraft from Etihad Airways . Lufthansa Airlines also ordered 34 777X aircraft. In December 2013, Cathay Pacific placed an order worth $ 7.48 bn to supply 21 Boeing 777-9X aircraft. Airplane delivery is expected to be completed between 2021 and 2024.

Boeing received a $ 18.6 billion contract from International Airlines Group for the delivery of 42 777X aircraft in February 2019. The order included a firm contract for 18 aircraft and options for 24 additional aircraft. In the same month, Boeing also received orders for 358 777X aircraft worth more than $ 100 billion from eight international airlines around the world.

Monday, 2 March 2020

Nextant 604XT Specs, Interior, Cockpit and Price

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Nextant 604XT Specs, Interior, Cockpit and Price – Nextant 604XT is a twin-engine, super-sized medium-sized business jet developed by Nextant Aerospace, United States, to operate on domestic and international air routes. Nextant 604XT is one of the fastest business jets in space. This aircraft was launched in 2017 with the Rockwell Collins ProLine Fusion flight and made its maiden flight in October 2018.

Nextant 604XT aircraft

Nextant 604XT Specs

The Nextant 604XT aircraft was built based on the Bombardier Challenger 604. Nextant made several improvements and improvements to the Challenger 604 including a new interior design and range improvement of up to 500 nmi through a program of drag reduction and wing extension as well as modernization in the avionics suite. The dimensions of the aircraft include a length of 20.8 m, height 6.27 m, and wingspan 19.6 m.

The Nextant 604XT landing system integrates a retractable tricycle type landing gear. Each unit is equipped with Dowty shock absorbers. The wheels are equipped with multi-disc anti-skid carbon brakes Aircraft Braking Systems.

Nextant 604XT Engine and Performance

The Nextant 604XT is powered by two General Electric CF34-3B turbofan engines. The aircraft can fly with a maximum cruise speed of 870 km / h and climb directly to altitude (FL450). The aircraft has a range of up to 4,524 nmi (8,378 km).

Nextant 604XT interior

Nextant 604XT Cabin and Interior

Nextant 604XT offers the latest cabin interior which includes seating, entertainment and VIP zones. The cabin is equipped with ergonomic features and advanced technology designed for an optimal flying experience. All features contained in the cabin are handmade, including cabinets and tables, and other soft items. The Nextant 604XT cabin can accommodate up to 9 passengers and 2 crew (pilots and co-pilots).

Nextant 604XT cockpit

Nextant 604XT Cockpit and Avionics

The Nextant 604XT cockpit is fully integrated with Rockwell Collins Pro Line Fusion's latest avionics suite. This avionics suite features more advantages including three large format displays, touch interactive maps with advanced flight planning, synthetic vision, high resolution topography, real-time weather radar overlay, and special use airspace and search patterns for enhanced situation awareness to reduce the workload of pilots. The aircraft is also equipped with a MultiScan weather radar that is able to detect and provide a complete weather picture to reduce the risk of accidental thunderstorms.

Nextant 604XT Price and Orders

The latest Next4 604XT price is US $ 8 million. On October 29, 2019, Constant Aviation sent 23 Production 604XT with the Next Flight Deck Next Generation. Constant Aviation expects to complete 30 shipments by the end of 2019 with significant guarantees until 2020.

Saturday, 29 February 2020

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

01:00
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.

Thursday, 27 February 2020

Cirrus Perception Specs, Sensor, Cockpit, and Price

01:00
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.

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

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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.