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.
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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.
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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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