Wednesday, 30 October 2019

Embraer E190 Specs, Interior, Cockpit, and Price

01:00
Embraer E190 Specs, Interior, Cockpit, and Price – The Embraer E190 is a commercial aircraft with a capacity of 78 passengers belonging to the E-Jet family produced by Embraer, Brazil. The E190 was launched in June 1999 and made its first flight in March 2004. It received the US Federal Aviation Administration (FAA) certification in September 2005 and entered service with JetBlue in January 2006. Certification of the steep approach to the Embraer E190 was received in 2010 to operate at the Airport London City.

The construction of the E190 aircraft involved various companies as suppliers of aircraft parts. The Japanese company Kawasaki supplies wing pieces, flaps and spoilers, surface control and front and rear ends. Gamesa Spain supplies parts of the rear fuselage and vertical and horizontal tail surfaces. Radome and forward fuselage are produced by Embraer, middle fuselage are by Embraer and Latecoere, rear fuselage by Gamesa and tailcone by Hamilton Sundstrand.

Embraer E190 Jetliner

Embraer E190 Specs

The E190 fuselage has a conventional low-wing monoplane design with two podded engines mounted under the wing. The wingtips are equipped with winglets to reduce wing vortex pull and provide increased lift and wing efficiency. This aircraft has a tailplane that moves all. Overall, the E-190 aircraft has a length of 36.24 m, wingspan 28.72 m, and a height of 10.57 m.

The E190 is equipped with front and rear doors on both sides of the fuselage. This makes the aircraft have a very complete airport turnaround time with a simultaneous service mechanism. In addition, the aircraft only takes ten minutes to refuel through a single point refueling container. The aircraft can carry 13,000 kg of fuel and is equipped with the Parker Hannifin fuel system.

The landing mechanism of the E190 aircraft is equipped with a retractable three-wheel type Liebherr landing gear. Each unit is equipped with twin wheels. The aircraft requires a minimum runway length of 1,463 m for takeoff and 1,280 m for landing. The minimum base width needed for a 180 ° turn is 18.04 m.

Embraer E190 Engine and Performance

The E190 Embraer is powered by two General Electric turbofan engines of type CF34-10E which are mounted under the wing. Each engine is able to provide a maximum thrust of 20,000 lb (89 kN). The engine is equipped with full authority digital machine control (FADEC).

A fully computerized management system can optimize engine performance, thereby reducing fuel consumption and maintenance requirements. The aircraft is equipped with additional Hamilton Sundstrand power units and electrical systems.

Embraer E190 aircraft has a maximum speed of Mach 0.82 (871 km / h) with a maximum range of 4,537 km. This makes the aircraft capable of operating between city pairs such as Dallas to Bogota, Paris to Moscow, Hong Kong to Bombay and Brasilia to Santiago. Field performance allows the aircraft to operate at sensitive airport restrictions that are located in strategic places such as Santos-Dumont Airport, Florence and London City.

Embraer E190 Interior

Embraer E190 Cabin and Interior

The E190 aircraft cabin has a double bubble type, making the cabin size larger (2.53 m on the floor and 2.74 m on the shoulder level) and easier access to overhead bins. The height in the passenger cabin is 2.00 m.

The cabin can accommodate 98 passengers with a four-parallel configuration. The cabin has an interior double-bubble seats design that offers spacious aisles and seating. The interior of the E190 cabin was designed by C&D Aerospace.

Embraer E190 Cockpit

Embraer E190 Cockpit and Avionics

The Embraer E190 aircraft has an all-digital cockpit. The cockpit is integrated with a modular and lightweight avionics suite. The avionics suite includes a Honeywell Primus Epic electronic flight system and an information system (EFIS) with five LCDs to display all flight data.

The E190 aircraft is equipped with fly-by-wire flight controls, thus reducing the pilot's work in controlling the aircraft. Flight control covers all primary controls, with the exception of ailerons.

Embraer E190 Price and Orders

The price of the latest Embraer E190 aircraft is around US $ 50.6 Million. At present, around 500 E190 aircraft have been operating with various airlines from all over the world including Air Canada, British Airways CityFlyer, Copa Airlines of Panama, TAME of Ecuador, a subsidiary of Air France Regional, Aerorepublica, HNA Group of China, US Airways, Lufthansa, Virgin Blue, KLM Cityhopper, NAS Air from Saudi Arabia, and TACA from El Salvador.

CDB Leasing Company ordered 30 Embraer E190 jets in 2011. The first aircraft were delivered in August 2011. TRIP Linhas Aereas awarded a $ 172 million contract to Embraer on March 1, 2011 to supply four Embraer E190 jets configured to a single 110-class seat.

Kazakhstan-based Air Astana ordered two Embraer E190 jets in June 2011 with an option for the other two. Kenya Airways ordered ten aircraft in August 2011 with the option to purchase 16 additional aircraft.

Azerbaijan Airlines (AZAL) received the first shipment of four Embraer E190 in July 2013. Venezuelan Airlines Consorcio Venezolano de Industrias Aeronáuticas y Servicios Aéreos (Conviasa) signed a contract for seven Embraer E190 jets, using the option of the original order released in July 2012 with which provided six firm orders and 14 options in June 2013.

Monday, 28 October 2019

Embraer E175 Specs, Interior, Cockpit, and Price

01:00
Embraer E175 Specs, Interior, Cockpit, and Price – The Embraer E175 is a commercial aircraft with a capacity of 78 passengers belonging to the E-Jet family produced by Embraer, Brazil. The E175 made its inaugural flight in June 2003 and has since obtained type certification for aircraft from several aviation authorities in Brazil, Europe and the US The aircraft entered service with Air Canada in July 2005 and the Federal Aviation Administration (FAA) Certification was received in September 2006.

Embraer currently produces E175 aircraft in three versions, namely standard (STD), long range (LR) and advanced range (AR). The AR version was introduced in 2007. It offers greater coverage and load capacity, which is generated from structural reinforcements. Embraer has launched a program to improve E-Jet aircraft, including E175. To reduce fuel combustion by 5%, the aircraft is being added with new wingtips, system improvements, and aerodynamics.

Embraer E175 Jetliner

Embraer E175 Specs

The E175 fuselage features a low-wing monoplane design with a conventional tail shape. Overall, the Embraer E175 has a length of 31.68 m, a wingspan of 26 m, and a height of 9.86 m. The maximum load capacity ranges from 10,080 kg to 10,360 kg depending on the aircraft version.

The E175 aircraft is equipped with integrated cost-effective design features with features to maximize passenger comfort. Two doors are provided at the front and rear for passengers. A series of similar doors are provided separately at the front and rear for service personnel and cargo.

The landing mechanism of the E175 aircraft is equipped with a tricycle type, two wheel type Liebherr landing gear. The aircraft requires a minimum runway length of 1,261 m for takeoff and 1,259 m for landing. The minimum base width needed for a 180 ° turn is 18.04 m.

Embraer E175 Engine and Performance

The Embraer E175 is powered by two General Electric type CF34-8E turbofan engines controlled by FADEC mounted under the wing. Each engine is able to provide a maximum thrust of 14,200 lb. The engine has an engine dry weight of 2,627 lb and a thrust-to-weight ratio of 5.41. The machine is fully interchangeable and has a maximum diameter of 136 cm. Engine noise complies with stage III and IV standards.

The maximum speed of the E175 aircraft is 0.82 mach (871 km/ h). The aircraft takes 18 minutes to climb and can fly with maximum operating speed. The E175 can fly to a maximum height of 41,000 ft and a maximum range of 3,151 km for the STD version, 3,521 km for the LR version, and 4,074 km for the AR version.

Embraer E175 Interior

Embraer E175 Cabin and Interior

The E175 can accommodate 78 to 88 passengers, depending on the version chosen by the operator. The cabin is spacious, 21.2 m long, 2.74 m wide and 2 m high. The four-parallel seating configuration and interior design of the double-bubble chair offer spacious aisles and seating. Thus allowing passengers to board the plane more easily.

The E175 aircraft cabin with 78 seats configuration has a arrangement of 19 double seats on the left and 20 double seats on the right. This arrangement can be optionally modified to double the first class seat on the right and the first class seat on the left. The cabin also accommodates one observer and two flight attendants. Additional seats for the second observer can be installed optionally.

The E175 aircraft is equipped with two cargo compartments under the floor. Compartments are located in the front and rear wing. The front compartment is bigger, with a volume of 9.92 m3 and a loading capacity of 1,500 kg. The rear compartment is smaller, with a cargo volume of 7.2 m3 and a loading capacity of 1,150 kg. Door nets are installed at each cargo door, while vertical nets can also be optionally installed.

Embraer E175 Cockpit

Embraer E175 Cockpit and Avionics

The E175 cockpit has two seats for pilots and co-pilots, with controls and systems that are easily accessible. It's acoustic and thermally insulated. The hand microphone is mounted on the left front door. The circuit breaker is located directly below it. The steering handle is conveniently located next to the hand microphone.

The cockpit is equipped with a series of digital avionics systems, including multifunctional LCDs, guide panels, electronic instrument systems (EIS) and primary flight displays (PFD).

Embraer E175 Price and Orders

The price of the latest Embraer E175 aircraft is around US $ 46 Million. At present, E175 has operated with 12 well-known passenger airlines, including Air Canada, Oman Air, Republic Airlines, Royal Jordanian Airlines, Northwest Airlines, Jet Airways, and others. More than 150 E175 are in operational services.

United Airlines placed a contract for 30 E175 jets in April 2013 and the first aircraft were delivered in April 2014. Mesa Airlines operates new aircraft under the United Express brand. United Airlines booked $ 1.1 billion at Farnborough Airshow in July 2018 for 25 E175 jets.

American Airlines booked $ 2.5 billion for 60 E175 aircraft plus options for 90 more in December 2013. The first aircraft was delivered in February 2015. The airline ordered $ 705 million for 15 E175 aircraft, increasing the total to 104. Shipping scheduled to begin in 2020.

In July 2014, Trans States Holdings ordered 50 E175-E2 jets. The $ 2.4 billion contract also includes an option for an additional 50 units. Deliveries are scheduled to begin in June 2020.

SkyWest placed a $ 301 million order for seven E175 jets in November 2014, as part of a previous order from the company for 100 E-Jets (40 companies and 60 reconfirmables) in 2013. This contract was followed by a new $ 422 million contract awarded in January 2018 for nine E175 jets, increasing the number of orders to 158. Deliveries begin in 2019.

Saturday, 26 October 2019

Embraer E170 Specs, Interior, Cockpit, and Price

01:00
Embraer E170 Specs, Interior, Cockpit, and Price – The Embraer E170 is a commercial aircraft with a capacity of 70 passengers belonging to the E-Jet family produced by Embraer, Brazil. The E170 was launched in June 1999 and made its maiden flight in February 2002. It obtained Brazilian, US and European certification in February 2004 and entered service with the Polish LOT airline in March 2004.

The E170 is the first member in the E-Jet family developed by Embraer. In addition to the aircraft, other members of the E-Jet family include E175 (78 passengers), E190 (98 passengers), and E-195 (108 passengers). Embraer has launched a program to improve E-Jet aircraft, including the E170. To reduce fuel combustion by 5%, the aircraft is being added with new wingtips, system improvements, and aerodynamics.

Embraer E170 Jetliner

Embraer E170 Specs

The E170's fuselage has a low-wing monoplane design with a podded engine mounted under the wing. The wingtips are equipped with winglets to reduce the pull of the vortex end and provide increased lift and increase wing efficiency. Overall, the Embraer E170 has a length of 29.90 m, a wingspan of 26.00 m, and a height of 9.85 m.

The E170 aircraft's fuel tanks are located on both wings. The tank has a maximum capacity of 9,470 kg and is equipped with the Parker Hannifin fuel system. The remote variant ERJ-170 is equipped with an additional fuel tank mounted in the trunk compartment.

The fuselage has front and rear doors on both sides, allowing passengers to get on and off with simultaneous service. This aircraft has a one-point refuel for ten minutes and under-wing engines can be serviced from the ground without a stand.

The landing mechanism of the E170 aircraft is equipped with a retractable three-wheel type Liebherr landing gear. Each unit is equipped with twin wheels. For takeoff, the aircraft requires a runway with a minimum length of 1,261 m. The minimum base width needed for a 180 ° turn is 18.04 m.

Embraer E170 Engine and Performance

The E170 is powered by two General Electric turbofan engines of type CF34-8E mounted under the wing. Each engine is capable to provide a maximum thrust of 14,200 lb. The engine is controlled by a full authority digital engine control (FADEC). A fully computerized flight management system that optimizes engine performance in each flight phase, thereby reducing fuel consumption and maintenance costs.

The maximum speed of the E170 aircraft is 0.82 mach (871 km/ h). The E170 can fly to a maximum height of 41,000 ft and a maximum range of 3,982 km at long distance cruising speeds and with full passenger seating. The aircraft is able to operate between the city pairs of Dallas to Halifax, Paris to Moscow, Hong Kong to New Delhi, and Brasilia to Caracas.

Embraer E170 Cockpit

Embraer E170 Cockpit and Avionics

The E170 aircraft is equipped with an all-digital cockpit that is integrated with a lightweight modular-architecture avionics suite. The Avionics Suite includes Honeywell Primus Epic Electronic Aviation and Information Systems (EFIS) with five LCDs to display all flight data.

Flight control of E170 is a computer control with fly-by-wire technology. All aircraft flight mechanisms are controlled with this technology, except for ailerons.

Embraer E170 Interior

Embraer E170 Cabin and Interior

The E170 aircraft cabin can accommodate 70 passengers. The cabin has a four-parallel configuration with a double-double seat arrangement, thus providing wider aisle and seating access with 81 cm seat pitch. The interior of the E170 aircraft was designed by C&D Aerospace.

Embraer E170 Price and Orders

The price of the latest Embraer E170 aircraft is around US $ 42 Million. At present, 193 Embraer E170s have been ordered and are operating with various airlines throughout the world, including Alitalia, British Airways City Flyer, Switzerland, GE Capital Aviation Services (GECAS), US Airways, LOT Airlines, PB Air, Air Caraibes, Republic Airways Holdings, Finnair, TAME of Ecuador, Saudi Arabian Airlines, Egyptair, Virgin Blue, Air France Regiona, and Virgin Nigeria.

Thursday, 24 October 2019

AVIC AG600 Kunlong Specs, Engine, and Price

01:00
AVIC AG600 Kunlong Specs, Engine, and Price – AG600 (TA-600) is the largest amphibious aircraft in the world that is being developed by Aviation Industry Corporation of China (AVIC). This aircraft is available in fire, search and water rescue variants. AVIC also plans to develop other aircraft variants including maritime surveillance, passengers, cargo, and tourism. The aircraft's main mission will include search and rescue operations and air firefighters.

The development of the AG600 aircraft has been carried out since 2009 by a group of 70 aircraft component manufacturers and a research team working with more than 150 institutions in 20 provinces and cities in China. The AG600 prototype aircraft was first introduced in July 2016 at a production facility located in Zhuhai in Guangdong Province, South China. The first AG600 flight will take place on December 24, 2017 and will be expected to start operating in 2022.

AVIC AG600 Kunlong Amphibious Aircraft

AVIC AG600 Specs

The AG600 amphibious aircraft are designed to carry out various missions, both on land and at sea. This seaplane have a boat-type fuselage design with one hull that integrates a high-mounted cantilevered wing, a T-tail wing and a tricycle landing gear. Overall, the AG600 has an overall length of 36.9 m, a height of 12.1 m, and a wingspan of 38.8 m.

The AG600 amphibious aircraft can take off and land from bodies of water as high as 1,500 m, 200 m wide and 2.5 m. It has the capacity to collect 12 t of water in 20 seconds and can carry up to 370 t of water in one fuel tank.

This seaplane can evacuate up to 50 people in a search and rescue mission (SAR) on the water. This can be equipped with special equipment for conducting maritime surveillance, resource detection, and passenger and cargo transportation missions.

AVIC AG600 Kunlong Engine

AVIC AG600 Engine and Performance

The AG600 amphibious aircraft is powered by four WJ-6 turboprop engines to drive four six-bladed propellers. The WJ-6 engine is a Chinese-made machine developed based on the Ivchenko AI-20 engine. The engine is capable of producing an output power of 3,805 kW (5,103 hp).

The AG600 aircraft can fly with a maximum speed of 560 km / h, and a cruising speed of 500 km / h. This amphibious aircraft has a maximum range of 4,500 km and a service ceiling of 6,000 m, while the minimum level of flight height is 50 m.

The AG600 seaplane can take off and land in adverse weather conditions with a wave height of 2 m. The maximum takeoff weight (MTOW) of an aircraft on a runway is 53.5 t and 49 t above water.

AVIC AG600 Kunlong Specs

AVIC AG600 Price and Orders

Until now there has been no official information from AVIC related to AG600  amphibious aircraft prices. However, since it was first introduced, AVIC has received orders from the Chinese Government of 17 aircraft for domestic use, but is expected to order more than 50 additional aircraft in the near future. Archipelagic countries including New Zealand and Malaysia have also shown interest in the AG-600. However, until now the company has not received export orders from foreign customers.

Tuesday, 22 October 2019

Beriev Be-200 Specs, Interior, Cockpit, and Price

01:00
Beriev Be-200 Specs, Interior, Cockpit, and Price – The Beriev Be-200 is a twin turbofan multi-role amphibious aircraft produced by Berieva Aviatsionnyi Kompaniya (Beriev Aviation Company), with the Russian Irkutsk Aircraft Production Association (IAPO). The aircraft was developed under a collaborative program that included major aviation industry companies such as Beriev Aircraft, Airbus, EADS-Irkut Seaplane (EISP) and EADS. The Be-200 test aircraft completed its maiden flight in September 1998. Meanwhile the Be-200ES first production aircraft made its first flight in June 2003.

The Be-200 aircraft can be configured to carry out various operations, including fire fighting, search and rescue, sea patrol and environmental monitoring, cargo and passenger transportation operations. It can take off and land on water and on runways that are not ready.

Beriev Be-200 Amphibious Aircraft

Beriev Be-200 Specs

The design of the Be-200 fuselage is a high-wing T-tail monoplane with a one-step design hull that can provide stability in water. The fuselage is made of aluminum alloy and coated with corrosion protection material. Overall, the Be-200 aircraft has a length of 31.43 m, a height of 8.9 m, and a wingspan of 32.78 m.

Designed as a multirole amphibious platform, the Be-200 can be configured for various missions. Be-200 has significant maritime characteristics for conducting coastal and blue waters operations. The aircraft provides flight characteristics similar to conventional aircraft.

In terms of the landing mechanism, the Be-200 aircraft is equipped with a hydraulic retractable retractable landing unit. Each unit has two wheels besides water steering, which provides steering in water. Underwing stabilizers mounted on the wings provide stability in water.

Beriev Be-200 Engine and Performance

The Be-200 amphibious aircraft is powered by two Progress D-436TP ZMKB turbofans and a TA 12-60 auxiliary power unit. Each engine is capable of producing an output power of 73.6 kN. The machine was developed by the Progress Design Bureau and produced by the Motorsich factory in Zaporozhye.

The D-436TP turbofan engines produce higher performance in hot and high conditions compared to turboprop engines mounted on similar fire engines. The engine has been developed with sophisticated materials and innovative solutions that are equipped with an engine control system, and an engine vibration monitoring system.

Be-200 aircraft can fly with a maximum speed of 680 km / h with a range of 3,300 km and a service ceiling of 8,000 m. The aircraft can ride at speeds of 3,350 ft per minute. The maximum take-off weight of Be-200 on the runway is 41,000 kg and in water is 37,900 kg.

Beriev Be-200 Cockpit

Beriev Be-200 Cockpit and Avionics

The Be-200 amphibious aircraft is equipped with a partial glass cockpit. The cockpit is equipped with a digital flight control system (fly-by-wire) and a modern navigation system, including satellite navigation (GPS), flight management system (FMS), autopilot and weather radar. The flight control system, integrated with an aerodynamic design, provides high maneuverability at low speeds as well as better handling and safety capabilities, and reduces pilot workload.

The Be-200 aircraft is equipped with a complete avionics circuit for all weather requirements. The avionics integrated all-weather ARIA 200-M system displays six 152 mm × 203 mm (6in × 8in) LCDs and an Electronic Flight and Information System (EFIS) to display all flight information to pilots. This system was developed by Honeywell together with the Moscow Research Institute for Aircraft Equipment.

Beriev Be-200 Interior

Beriev Be-200 Cabin and Interior

The Be-200 cabin can be arranged in a passenger, item, or mixed layout (goods and passengers). Passenger cabs can be configured with up to 66 tourist class seats or between ten and 32 first class and business seats. The cabin interior is provided by AIM Aviation (Fliteform) Ltd, from Alfreton, Derbyshire from England.

In cargo configuration, this aircraft has a capacity of up to 7,500 kg of cargo. In a mixed passenger / cargo configuration, 19 passengers and up to 3,000 kg of cargo can be transported. The cabin is equipped with a cargo door that has a height of 1.70 m and a width of 2.00 m, making it easy to access for large loads. The cabin can hold up to nine shipping containers.

Beriev Be-200 Specs

Beriev Be-200 Variant

The Be-200 amphibious aircraft has several variants adapted to the mission including fire fighter, search and rescue, cargo ships, passenger aircraft and ambulances. Fire fighting variants have a crew of two members, and are equipped with fire and water tanks. The aircraft can drop 12,000 litres of water in the fire area without refueling.

Search and rescue (SAR) variants can operate within an area of ​​200 miles for 6.5 hours. The aircraft is equipped with inflatable rubber dinghy, thermal imaging, and optical search aids and first aid kits. The SAR variant can be configured to carry 45 passengers.

The cargo transportation variant is equipped with cargo handling equipment mounted on the floor to transport loose cargo, as well as cargo loaded in standard containers and pallets. This aircraft has a payload capacity of up to 7,500 kg.

Passenger variants, designated as Be-210, can carry 72 passengers. It has a maximum range of 1,850 km. Meanwhile, the Be-200 ambulance variant can accommodate ten medical staff as well as 30 people who were injured with stretchers. This aircraft is equipped with emergency diagnostics and intensive care facilities.

Beriev Be-200 Price and Orders

The price of the latest Beriev Be-200 amphibious aircraft is around US $ 45 to 70 million according to the specifications ordered. The Russian Ministry of Emergency Situations (Emercom) was the first customer to receive an aircraft in July 2003 based on seven Be-200 fire and rescue orders. The Ministry of Emergencies, Azerbaijan, received the shipment of a Be-200ES aircraft in 2008.

The Russian Navy plans to buy four Be-200 aircraft for reconnaissance and search and rescue assignments, with deliveries scheduled between 2010 and 2013. The Navy of the People's Liberation Army (PLAN) China is also in discussions with Russia to buy maritime search and rescue variants.

Sunday, 20 October 2019

Bombardier Dash 8 Q400 Specs, Interior, Cockpit, and Price

01:00
Bombardier Dash 8 Q400 Specs, Interior, Cockpit, and Price – Bombardier Dash 8 Q400 is one of the quietest turboprop aircraft in the world developed by Bombardier Aerospace De Havilland Canada. The development of this aircraft is intended to meet the requirements of regional airlines for larger aircraft on high density routes and short distances. Q400 is the largest member of the Dash 8 family that can accommodate up to 80 passengers.

The Q400 program was launched in 1995 as a broad version of the Q300 series. The first flight of the Q400 aircraft was carried out in 1998 and entered commercial service in February 2000. The aircraft was equipped with a noise and vibration suppression (NVS) system introduced in the Dash 8 turboprop family in 1996.

The latest variant of the Q400 aircraft, the Q400 NextGen, was announced in March 2008. The new aircraft has improvements in the cabin environment, including LED lighting, new ceiling panels, sidewall windows and larger bins. Q400 NextGen participated in the 2012 FIDAE Air Show held in Santiago, Chile in April 2012.

Bombardier Dash 8 Q400

Bombardier Dash 8 Q400 Specs

The transverse section near the circle of the fuselage and the tail section are manufactured by Mitsubishi. The wings, tail plane, and front end of the fins are equipped with a de-icing system. The Q400 aircraft is equipped with a R408 type six bladed composite propeller supplied by Dowty. The propeller is equipped with an electric current removal system. Overall, the Q400 aircraft has a length of 32.84 m, a height of 8.36 m, and a wing span of 28.42 m.

In terms of electricity, the Q400 aircraft powered by an Allied Signal electric power system includes two starter / generators for DC power, two transformer units and two nickel cadmium batteries. There are two engine-driven AC generators to supply variable frequency AC power.

The Q400 aircraft landing mechanism features a retractable Menasco tricycle type landing gear. Each unit has twin wheels equipped with Goodrich anti-skid brakes. Two independent hydraulic systems are supplied by Parker Bertea Aerospace.

The fuel tank located on the wing of the aircraft has a total capacity of 6,526 l. The Q400 test aircraft became the first Canadian aircraft to fly using D7566 bio-fuel. D7566 is certified by the American Society for Testing and Materials (ASTM). Porter Airlines is Canada's first biofuel-powered revenue flight on its Q400 aircraft.

Bombardier Dash 8 Q400 Engine and Performance

The Q400 aircraft is powered by two PW150A turboprop engines supplied by Pratt & Whitney Canada. Each engine is capable of producing an output power of 5,071 shp or 3,800 kW. The engine is equipped with full digital engine control (FADEC). With the support of the PW150A engine, the Q400 is capable of flying with a maximum cruise speed of 650 km / h with a maximum distance of 2,519 km.

Bombardier Dash 8 Q400 cockpit

Bombardier Dash 8 Q400 Cockpit and Avionics

The Q400 aircraft is equipped with a dual control cockpit that can accommodate pilot and co-pilot. The cockpit is integrated with an electronic flight instrumentation system (EFIS) with five high-resolution LCDs, 6 in x 8 in to display all flight information. The cockpit is also equipped with an emergency locator transponder, solid state cockpit voice recorder, and a holographic guidance system from Flight Dynamics.

The avionics suite of Q400 aircraft supplied by Thales Avionics includes a flight management system, global positioning system and a traffic warning and collision avoidance system, TCAS II. The aircraft communication suite includes dual VHF navigation and S communication and transponder mode. Navigation equipment includes weather radar, proximity proximity warning receivers, radar altimeters, automatic direction finders, and distance measuring equipment.

Bombardier Dash 8 Q400 interior

Bombardier Dash 8 Q400 Cabin and Interior

The Q400 aircraft cabin can be configured for a class or two class layout that can hold 68 to 78 passengers. Meanwhile, cabin with business class configurations can only accommodate 58 seats. The cabin is equipped with an air ladder mounted at the front of the cabin, allowing the aircraft to use the airport with limited ground support facilities. Two passenger doors and one service door allow the aircraft to get up and down quickly. This aircraft provides more than 14 m³ of baggage space.

Bombardier Dash 8 Q400 Price and Orders

The price of the latest Bombardier Dash 8 Q400 aircraft is around US $ 32.2 Million. More than 413 Q400s have been ordered, with 389 delivered in December 2011. Major operators include: SAS Commuter (launch customer), Augsburg Airways from Germany, Horizon Air USA, Austrian Tyrolean Airways, Qantas Airways, Horizon Air, Flybe, Colgan Air / Pinnacle , Porter Airways and All Nippon Airways Japan. Meanwhile orders for the NextGen Q400 include 20 aircraft from Eurolot in March 2012, five aircraft for Ethiopian Airlines and two for Horizon Air in February 2012.

Friday, 18 October 2019

Bombardier Dash 8 Q300 Specs, Interior, Cockpit, and Price

01:00
Bombardier Dash 8 Q300 Specs, Interior, Cockpit, and Price – Bombardier Dash 8 Q300 is a regional aircraft turboprop engine that was introduced in 1998 by Bombardier Aerospace De Havilland Canada. This aircraft can accommodate up to 56 passengers. This Bombardier aircraft is equipped with a noise and vibration suppression system (NVS). NVS technology was introduced to the Dash 8 turboprop family in 1996 and the Dash 8 aircraft series was renamed the Q series.

The Dash 8 Q series family also includes Q100 (37 seats), Q200 (39 seats) and Q400 (68 to 78 seats). The Q300 has a larger fuselage and wingtips added and has a more powerful engine compared to the Bombardier Q200 aircraft. The Q300 aircraft variant consists of Q300MSA for maritime and Q300HGW for heavy transport. Maritime task variants are equipped with crew station interiors, large conformal observation windows, and structural fuselage mods. While the heavy duty variant is equipped with a more powerful engine and greater payload capacity.

Bombardier Dash 8 Q300

Bombardier Dash 8 Q300 Specs

The Q300 aircraft is an extended version of the Q200 aircraft. The overall length of the fuselage length is 25.7 m. The fuselage is almost circular in the transverse section. The upper center line of the fuselage carries a large dorsal fin which blends with the swept T-vertical tail fin. This aircraft has conventional and powered flight controls, as well as digital automatic flight control systems. The Q300 aircraft is equipped with a tricycle-type landing gear drawn by Dowty Aerospace equipped with twin Goodrich wheels and brakes. The landing gear is equipped with the Hydro-Aire mk3 anti-skid unit.

The Q300 aircraft can be equipped with an optional Turbomach T-40 additional power unit. The DC power unit consists of two sets of starters / generators, two sets of transformers and rectifiers and two nickel cadmium batteries. This aircraft is equipped with a DC outlet mounted on the nose on the port side. The aircraft's AC power system consists of two engine-driven AC generators with three static inverters. A grounded AC outlet is installed on the rear right side nacelle engine.

This aircraft has two hydraulic systems that operate independently. Each hydraulic system consists of an engine-driven displacement pump, an electrically powered standby pump, an accumulator and a manually operated emergency pump.

Bombardier Dash 8 Q300 Engine and Performance

The Q300 aircraft is powered by two Pratt & Whitney Canada PW123 turboprop engines mounted on the wing. Each engine is able to provide an output power of 1,775 kW to drive the Hamilton Sundstrand 14SF-23 four blades propeller. The propeller has a diameter of 3.96 m and is equipped with an electric eraser system.

The Q300HGW heavy duty variant is powered by a 123B PW turbo engine which provides increased power for operation from cold and low airport conditions. The PW123B engine is capable of producing an output power of 1,864 kW. The Q300HGW has a maximum load of 6,126kg, larger than the standard version of the Q300 with a payload of 5,166 kg.

The Q300 aircraft fuel tank located on the wing has a total fuel capacity of 5,700 l consisting of 3,160 l of operational fuel and 2,540l of additional fuel. The fuel tank is equipped with a Simmonds fuel monitoring system, a gravity fill point on the upper wing and a single pressure refueling point on the right engine nacelle.

The maximum speed of the Bombardier Q300 aircraft is 528 km / hour. The aircraft can fly to a maximum height of 7,620 m and a maximum distance of 1,558 km. The aircraft take-off and landing distances are 1,178 m and 1,041 m, respectively. The aircraft has a maximum take-off weight of 19,505 kg.

Bombardier Dash 8 Q300 cockpit

Bombardier Dash 8 Q300 Cockpit and Avionics

The Q300 aircraft cockpit has Honeywell electronic dual flight control (EFIS) connected to the SPZ-8000 Honeywell automatic digital dual flight control system. The cockpit can be equipped with Flight Dynamics HGS2000 head-up guidance system to provide Cat IIIa capabilities to the aircraft. The autopilot system is also integrated on the Q300 aircraft.

The standard avionics suite on the Q300 aircraft is Honeywell. But other avionics series, including Rockwell Collins can be installed as an alternative. Meanwhile, the navigation suite on this aircraft includes the KNR 806 automatic direction finder (ADF), the KDM 706A (DME) distance measuring device, the Honeywell Gold Crown III communication and navigation system and the optional global positioning system and Primus P660 color weather radar.

Bombardier Dash 8 Q300 interior

Bombardier Dash 8 Q300 Cabin and Interior

The cabin of the Q300 aircraft has a length of 12.65 m. The cab can be configured in one aisle seating arrangements, four seats in line for 50 passengers in standard seats or 56 passengers in economy class
seat. The cabin has a luggage room with a capacity of 8.5 m³. The pressurized cabin is equipped with two air conditioning units.

The cabin is equipped with an upstairs door mounted on the left side of the cabin for passengers and crew, allowing airplane access to a small airport with limited facilities. Meanwhile, a large door is also mounted on the rear side of the stern of the wing to load cargo and luggage.

Bombardier Dash 8 Q300 Price and Orders

The price of the latest Bombardier Dash 8 Q300 aircraft is around US $ 17 Million. More than 267 Q300 aircraft have been ordered and sent. This aircraft is in service with Air Nippon, ALM, Augsberg Airways, Avline, Brymon Airways, GPA Jetprop, Hamburg Airline, Clay, Mark Air, National Jety, Petroleum Services, QantasLink, SA Express, Time Air, Tyrolean, Union Airways, Wideroe and Zhejlang Airlines. Around 172 aircraft currently operate in the Asia Pacific region.

Thursday, 17 October 2019

AVIC Xian MA60 Specs, Interior, Cockpit, and Price

01:00
AVIC Xian MA60 Specs, Interior, Cockpit, and Price – AVIC MA60 is a twin turboprop engine passenger aircraft manufactured by AVIC Commercial Aircraft Co., a subsidiary of the Aviation Industry Corporation of China (AVIC). The aircraft is used for short and domestic air routes, and is designed for transportation of passengers and goods, maritime patrols, medical evacuations, and operations to bring down paratroopers.

The inaugural flight of the MA60 aircraft was carried out in February 2000. The MA60 aircraft received certification from the Chinese Civil Aviation Administration (CAAC) in June 2000 and began operating with Sichuan Airlines in August 2000. It was accredited with the type of certification of the Indonesian Directorate of Civil Aviation (IATDG) in 2006. The MA60 aircraft variants are MA60-100, MA60-MPA Fearless Albatross, MA40, MA60H-500, and Xian MA600.

AVIC Xian MA60

AVIC Xian MA60 Specs

The AVIC MA60 is a stretch version of the Xian Y7-200A, which is produced based on the Antonov An-24. This aircraft is designed to take off and land on unprepared airstrips, grass runways, and sandstone and has short take-off and landing (STOL) capabilities. The MA60 is equipped with a de-icing system allowing the aircraft to fly in snowy weather conditions in winter.

The MA60 aircraft landing mechanism is equipped with a retractable tricycle-type landing gear consisting of two main gears, a single nose wheel that can be controlled, two disc brakes, and tubular resistant anti-explosion tires. Overall, the AVIC MA60 aircraft has a length of 24.71 m, a wingspan of 29.2 m, and a height of 8.86 m. The aircraft has an empty weight of 30,203 lb and a Maximum Take-Off Weight (MTOW) of 48,060 lb. The aircraft's flight range reaches 1,600 km (860 nmi).

AVIC Xian MA60 Cockpit

AVIC Xian MA60 Cockpit and Avionics

AVIC MA60 aircraft cockpit accommodates pilots and co-pilots. The cockpit is equipped with a primary flight display and a 10 x 8 inch high-resolution multifunction LCD that displays flight information, including the EFIS-84 electronic flight instrumentation system, EICAS-4000 engine indication and crew warning system, automatic flight control system, central warning system, data system dual air and dual navigation attitude systems.

The MA60 aircraft is equipped with a Pro Line 21 avionics suite supplied by Rockwell Collins. The avionics package includes the FMS-3000 flight management system, communications, radio navigation and surveillance sensors (CNS), the AHS-3000 attitude heading reference system and the TWR-80 weather radar.

AVIC Xian MA60 Interior

AVIC Xian MA60 Cabin and Interior

The AVIC MA60 aircraft cabin is 10.8 m long, 2.7 m wide and 1.9 m high. The spacious cabin can accommodate up to 60 passengers in a four-seat configuration. The cabin is also equipped with an air conditioning system to regulate the flow of air inside the cabin and maintain a soothing temperature.

AVIC Xian MA60 Engine and Performance

The AVIC MA60 is powered by two Pratt & Whitney Canada PW127J turboprop engines to drive two Hamilton Sundstrand composite four-blades propellers. Each engine is capable to producing 2,051 kW of thrust. With this engine, MA60 can fly with a maximum speed of 514 km / hour and cruising speed of 430 km/ hour. The range and ceiling of aircraft services are 1,600 km and 7,620 m, respectively.

The PW127J engine is equipped with a two-stage centrifugal compressor, back-flow burners, one-level low-pressure and high-pressure turbines, two-stage electric turbines, unadjusted reduction gearboxes, and an electronic engine control system. Overall, this aircraft engine has a length of 2.1 m, width of 0.6 m and height of 0.8 m.

AVIC Xian MA60 Price and Orders

The price of the latest AVIC Xian MA60 aircraft is around US $ 22 Million. AVIC Commercial Aircraft Co. has received 250 MA60 orders from various customers throughout the world until October 2011. Customer orders for MA60 include: YingAn Airlines, Zest Airways, CDS Regional Express, Cameroon International Air Transport, Air Burundi, and Air Congo International. Military customers include the Ecuadorian Air Force, the Ghana Air Force, the Sri Lankan Air Force, the Zambia Air Force, and the Bolivian Air Force.

Tuesday, 15 October 2019

AVIC Xian MA700 Specs, Range, Cockpit, and Price

23:59
AVIC Xian MA700 Specs, Range, Cockpit, and Price – AVIC MA700 is the latest medium range turboprop aircraft developed by AVIC Commercial Aircraft Co., a subsidiary of the Aviation Industry Corporation of China (AVIC). This aircraft will be intended for the short and medium term regional passenger transportation sector, which includes routes within 800 km. The basic version of the MA700 can also be used to support medical missions, emergency rescue and disaster relief, meteorological, and scientific.

The development of the MA700 aircraft first began in 2008. Meanwhile, the construction of the aircraft began in 2013 involving several contractors, including Safran Electrical & Power as a supplier of major and additional power generation systems, Saft as a provider of ultra-low maintenance batteries (ULM), AVIC Xi'an Aviation Brake Technology as supplying wheel and brake systems, Zodiac Aerospace as a supplier of airborne equipment, and AMETEK Sensors and Fluid Management Systems (SFMS) as providers of aircraft fuel measurement systems.

From 2016 to 2019, AVIC Commercial Aircraft Co. continuously testing a number of aircraft components, including the fuselage, wings and avionics. The inaugural flight of the MA700 aircraft is scheduled to take place in 2020. The aircraft is expected to receive certification from the Chinese Civil Aviation Administration (CAAC) in 2021 and is scheduled to begin operations in 2022.

AVIC Xian MA700

AVIC Xian MA700 Specs

AVIC MA700 aircraft are equipped with advanced aerodynamic technology and fuel-efficient turboprop propulsion systems, the aircraft will be able to operate at high altitudes and temperatures. This will offer the benefits of reducing fuel consumption and maintenance costs.

The MA700 aircraft design integrates a conventional wing mounted high in the mid-fuselage, T-tail, and tricycle type landing gear configurations. This aircraft will have a length of 30.5 m and a height of 8.1 m and will have a wingspan of 27.5 m. The fuselage can be shortened or extended while maintaining the basic design of the cabin and cockpit interface.

AVIC Xian MA700 cockpit

AVIC Xian MA700 Cockpit and Avionics

The AVIC MA700 aircraft is equipped with a digital glass cockpit integrated with the Safran flight control system. It will also be equipped with a fly-by-wire fly control actuation system provided by Parker Aerospace. So that it can ease the workload of pilots in flying a plane.

AVIC Xian MA700 Cabin and Interior

The MA700 aircraft base cabin configuration can accommodate seating for 78 passengers, while the high density cabin configuration can accommodate up to 86 passengers. The spacious cabin allows a spacious and comfortable seating layout. The cabin is also equipped with a wide entrance staircase, allowing passengers to ride quickly and comfortably.

AVIC Xian MA700 specs

AVIC Xian MA700 Engine and Performance

The AVIC MA700 will be powered by two Pratt & Whitney Canada (P&WC) PW150C turboprop engines with a Dowly Propellers R504 six-blades propulsion system. With this engine, the MA700 aircraft will have a maximum speed of 637 km/ h and fly at a maximum height of 7,620 m. It will be able to reach a maximum range of 2,700 km and will have a maximum take-off weight of 58,000 lb.

AVIC Xian MA700 Price and Orders

The price of the latest AVIC Xian MA700 aircraft is around US $ 25 Million. In September 2019, commercial Aircraft Co. has received 285 orders from 11 operators for MA700 aircraft, consisting of China Joy Air, China Okay Airways, China CDB Leasing, China CMB Leasing, China Chongqing General Aviation Financing and Leasing, China Poly Technologies, Nepal Air Avenues, Cambodia Cambodia Bayon Airlines , United Arab Emirates EGA Group Emirates, Pakistan Hybrid Aviation, and South Africa Segers Aero.

Saturday, 12 October 2019

Yakovlev Yak-130 Jet Trainer Specs, Cockpit, Radar, and Price

01:00
Yakovlev Yak-130 Jet Trainer Specs, Cockpit, Radar, and Price – Yakovlev Yak-130 (NATO reporting name: Mitten) is an advanced two-seat jet trainer and subsonic light fighter aircraft designed and produced by Yakovlev and the Irkut company. The Yak-130 can be used as a light attack aircraft or as a trainer for various fourth or fifth generation fighter jets.

The joint program for the development of coaches between Russian Yakovlev and Italian Aermacchi began in 1993. The Yak/ AEM-130D demonstrators flew in 1996. In 1999, the partnership was dissolved and the Yakovlev Yak-130 and Aermacchi M346 became separate programs.

In the second quarter of 2003, the Yak-130 prototype successfully completed 450 flights, including demonstration flights with high maneuverability such as a 42 ° controlled attack angle.

Yak-130 completed the first phase of a joint state test in April 2009 which included entering basic weaponry. Arrived at the Lipetsk Air Base in February 2010. The aircraft flew in a line of sophisticated digital avionics developed by KRET in June 2014.

Yakovlev Yak-130 Jet Trainer

Yakovlev Yak-130 Specs

The Yak-130 fuselage has a classic swop-wing design and empennage monoplane with lightweight carbon fiber alloy construction. Kevlar armored guards are installed in the engine, cockpit and avionics compartments. The high lift wings which are swept up medium and the low tail plane all move allows the pilot to choose a high angle of attack. The airframe is designed for a 30-year work period with 10,000 flight hours or 20,000 landings.

The Yak-130 jet trainer is equipped with leading edge blades and a three-position Fowler flap, so it can operate on short airfields. Fowler flaps are split flaps that move back and then down the track to provide a large increase in lift and lift height and drag for landing maneuvers.

The Yak 130 trainer can be operated from non-paved runways and small unprepared airfields because the landing gear is designed with a high takeoff. The intricately installed fly-by-wire control system allows the aircraft to feature automatic flight control systems, active flight safety systems, stability training, and control characteristics.

Yakovlev Yak-130 Specs

Yakovlev Yak-130 Engine and Performance

The Yak-130 jet trainer is powered by two AI-222-25 turbofan engines developed under the Russian and Ukrainian programs by Motor Sich, the Zaporozh'e Progress Design Bureau and the Moscow Salyut Motor Building Production Company. Each machine has a thrust of 2,500 kg. Meanwhile, the Yak-130 export variant can be paired with a DV-2SM engine.

The internal fuel tank of Yak 130 trainer, consists of two wing tanks and a central fusel that can carry up to 2,179 l of fuel. With two suspended fuel tanks (450 l each), the maximum total fuel load is 3,100 l. The aircraft is equipped with single point pressure or optional gravity refueling. This training aircraft can be equipped with a refueling probe in flight.

Yakovlev Yak-130 Cockpit

Yakovlev Yak-130 Cockpit and Avionics

The cockpit of the Yak-130 jet trainer has a two-seat tandem configuration. The air-conditioned and pressurized cockpit is equipped with an NPO Zvezda K-36LT3.5 zero-ejection seat. This jet trainer has an all-glass cockpit. Both pilot positions are compatible with night vision goggles (NVG) and are equipped with three multifunctional 6 in x 8 in color liquid crystal screens.

Pilots in the front cockpit can use helmet-mounted vision to designate targets. The cockpit is equipped with internal and external MS communication and a voice warning system provided by AA.S. Popov GZAS joint-stock company. The pilot has a holistic view through the blister canopy. The front pilot has a view to the nose of the aircraft by -16 °, while the rear pilot has a view of -6 °.

The Yak-130 avionics suite is fully digital integrated with Avionica's fly-by-wire flight control system which functions to adjust stability and control characteristics and flight safety systems to simulate a number of fighter aircraft such as MiG-29, Su-27, Su-30, F- 15, F-16, F-18, Mirage 2000, Rafale, Typhoon and future fighters like the F-35.

The pilot chose the software model of the simulation aircraft control system on the Yak-130 on-board computer. Pilots can choose the model during the flight. This system can be forgiving to allow cadet pilots to obtain piloting skills easily. The jet trainer is equipped with an avionics open architecture suite including two computers and a three-channel information exchange multiplexer. The navigation suite includes a laser gyroscope and GLONASS / NAVSTAR global positioning.

Yakovlev Yak-130 Radar

The Yak-130 jet trainer is equipped with 8 GHz to 12.5 GHz Osa or Oca (Wasp) radar, which is supplied by NIIP Zhukovsky. Radar has the capacity to track eight targets in the air simultaneously, simultaneously involving four targets in all angles and simultaneously tracking two ground targets. The detection range of the 5m² cross-section target is 40 km in the back and 85km in the forward direction. The locking range for operation in automatic tracking mode is 65 km. The radar has an adaptive waveform and sidelob, has a surface mapping mode that includes freezing and enlarging the image in the area of ​​interest.

The electronic warfare suite on the Yak-130 combat trainer includes chaff and flare dispensers, radar warning receivers and active jammers.

Yakovlev Yak-130 Weapon

Yakovlev Yak-130 Weapons

The Yak-130 can simulate the tactics of various existing fighter planes. The aircraft can carry weapons, suspended fuel tanks, surveillance pods and various electronic war pods including radar jammers and infrared countermeasures. There is one diameter of the fuselage line and the number of wing hooks for arms suspension has been increased to eight with six underwings and two wing tips, increasing the weight of combat loads to 3,000 kg.

The open architecture suite installed on the Yak-130 allows a variety of heavy weapons systems, Vikhr laser guided missiles, R-73 infrared guided air-to-air missiles (as NATO 11-Archer), Kh-25 ML (as NAT-10 AS- 10 Karen) air-to-surface laser, AIM-9L Sidewinder, Magic 2 and AGM-65 Maverick missiles. Platan's electro-optical guide pod is mounted under the fuselage for the placement of KAB-500Kr guided bombs.

This fighter training aircraft is equipped with a 30 mm GSh-301 cannon or a GSh-23 cannon mounted under the fuselage. It can also use B-8M and B-18 missiles that are not aimed, bombs 250 kg and 50 kg and cluster bombs.

Yakovlev Yak-130 Price and Orders

The price of the latest Yakovlev Yak-130 advanced jet trainer is US $ 46 Million. In March 2006, it was announced that Algeria had ordered 16 Yak-130 trainers. Deliveries were completed in 2011.

In December 2011, the Russian Ministry of Defense ordered with Irkut for the shipment of 55 Yak-130 combat trainers in 2012. The first batch of six aircraft was sent to the Russian Air Force in October 2012. The second batch of three Yak -130 was delivered in November 2012. A total of 15 aircraft were sent to the Russian Air Force in 2012.

Bangladesh ordered 16 Yak-130s in January 2014. The Russian Ministry of Defense placed orders for the supply of 12 additional aircraft in February 2014. A total of 36 Yak-130 aircraft are expected to be sent to Syria in 2016. Russia also plans to export aircraft to the Azerbaijan military.

Thursday, 10 October 2019

Tupolev Tu-95MS Bombers Specs, Range, Cockpit, Price

01:00
Tupolev Tu-95MS Bombers Specs, Range, Cockpit, Price – Tupolev Tu-95MS (NATO reporting name: Bear-H) is a strategic long-range turboprop-powered bomber developed by Russian aerospace and defense company JSC Tupolev Design Bureau. The operator is currently in service with the Russian Air Force. The Tu-95MS aircraft is a modern version of the Tu-95 Bear strategic bomber. It is equipped with a stand-off cruise missile and can be used in combat missions to defeat cruise missiles and strategic enemy targets.

The first flight test was conducted in May 2011, two Tu-95MS aircraft conducted a 17-hour patrol flight over the Aleutian Islands. This was followed by a 10-hour air patrol flight in the Pacific Ocean in November 2011. Two Tu-95MS strategic bombers also conducted patrol flights over the Aleutian Islands. Arctic Ocean for 20 hours in April 2012. Another patrol flight, which lasted 13 hours, was executed in the Norwegian Sea in November 2013. The Tu-95MS successfully launched six high-precision cruise missiles at ground targets during a 7-hour tactical flight test in June 2014 .

Tupolev Tu-95MS Bear-H Bombers

Tupolev Tu-95MS Specs

The Tu-95MS fuselage is made entirely of metal construction and has a high aspect ratio spar wing design. It was able to engage the main stationary enemy targets under extreme weather conditions both in the day and night. The aerodynamic design of the fuselage allows it to fly at high speeds at safe altitudes. Two large fairings are mounted on the wing to reduce drag. Overall the Tu-95MS has a length of 49.6 m and a height of 13.3 m, and is equipped with a semi-monocoque aircraft.

The Tu-95MS landing mechanism is equipped with a retractable tricycle type landing gear consisting of a controllable two-wheel nose unit and a four-wheeled main unit. The maximum take-off and landing weights are 185 t and 135 t respectively and the maximum load capacity is 20,000 kg. The wing is swept back at 35 ° and the wing span is 50.05 m.

Tupolev Tu-95MS Specs

Tupolev Tu-95MS Engine

Tupolev Tu-95MS bomber is powered by four NK-12MP turboprop engines supplied by the Kuznetsov Design Bureau. Each engine drives an eight-bladed AV-60N counter-rotating propeller. The engine has a takeoff power of 15,000 hp (11,000 kW) and a pressure ratio of 9.7.

The internal fuel capacity of the aircraft is 84 t. Fuel is stored in four integrated tanks in the outer wing, two middle wing tanks, and in the central fuselage tank. An air-to-air refueling probe is mounted on the nose.

The maximum speed of the Tu-95MS is 830 km/ h and the cruising speed is 550 km/ h. This aircraft has a flight range of 10,500 km. This range can be extended up to 14,100 km with one flight refueling. Take-off and landing rolls from the bombers were 2,540 m and 1,700 m respectively, and the service ceiling was 10,500 m.

Tupolev Tu-95MS Weapon

Tupolev Tu-95MS Weapons

The Tu-95MS aircraft is armed with two 23-mm double-barreled Gryazev-Shipunov GSh-23 automatic cannons at the rear for defense against air threats. Each cannon has a shot rate of 2,400 rounds per minute. Six Kh-15 air launch cruise missiles with a range of 2,500 km are carried out in a drum launcher. The aircraft can be further modified to carry up to eight Kh-101 air launch cruise missiles or 14 Kh-65 anti-ship missiles.

Tupolev Tu-95MS Cockpit

Tupolev Tu-95MS Cockpit and Avionics

The Tupolev Tu-95MS bomber aircraft can accommodate seven crew members, including a pilot and co-pilot. The Avionik Tu-95MS suite includes the ANS-2009 celestial navigation system, developed by Concern Radio-Electronic Technologies (KRET), to determine aircraft coordinates. The new generation BINS-SP-2M strapdown inertia navigation system, which was also developed by KRET, determines the location of objects and provides navigation and flight data in the absence of satellite navigation.

The aircraft is also equipped with Leninetz Obzor-MS clam pipe navigation and pulse-doppler radar attacks, and the Mak-UT approach warning system infrared (MAWS). It can be upgraded with new equipment to increase reliability.

The Tu-95MS bomber is equipped with a self-defense system from guided missiles, the SPS-160 Geran Jammer series. Electrical defrosting systems are installed to protect the leading canopies, propellers, pilots and wing tips. The onboard electronic countermeasures (ECM) also includes the Meteor-NM computer-controlled ECM system, APP chaff / flare dispenser and Avtomatika SPO-32/ L150 digital warning receiver.

Tupolev Tu-95MS Price and Orders

The price of the latest Tupolev Tu-95MS Bear-H Bombers is around US $ 26.28 Million. The first production aircraft was deployed by the 121st Heavy Bomber Regiment at the Engels Air Base and the 73rd Heavy Bomber Flight Division at the Ukrainka Air Base.

In December 2014, Tupolev handed over two Tu-95MS strategic bombers that were enhanced with improved avionics and flight efficiency to the Russian Air Force, as part of the country's defense orders. Further shipments of the upgraded Tu-95MS took place in January 2015. The Russian Ministry of Defense bought 20 modern bombers by the end of 2016. The aircraft is expected to continue to operate with them until 2040.

Tuesday, 8 October 2019

Tupolev Tu-22M3 Strategic Bomber Specs, Cockpit, Price

01:00
Tupolev Tu-22M3 Strategic Bomber Specs, Cockpit, Price – Tupolev Tu-22M3 (NATO reporting name: Backfire-C) is a long-range strategic and maritime strike bomber developed by Tupolev for the Russian Air Force. The aircraft is currently in service with the Russian Air Force and Russian Navy Aviation. This aircraft is mainly used to carry out nuclear attacks and conventional attack operations. This can also be used in anti-ship missions and maritime surveillance.

The earliest pre-production aircraft produced was the Tu-22M0. Its production is limited to a small amount due to inadequate performance. Then followed by the Tu-22M1 pilot production aircraft for the Russian Naval Aviation. Production in the first major production version, the Tu-22M2 began in 1972. It was equipped with extended wings and a redesigned fuselage, twin engines and new undercarriage.

The Tu-22M3 is based on the Tu-22M aircraft design. The first Tu-22M0 prototype completed its maiden flight in August 1969. The Tu-22M1 first flew in July 1971 and the Tu-22M was first used in combat missions in Afghanistan between 1987 and 1989. The Tu-22M3 was used by Russia for combat operations in Chechnya in 1995.

The Tu-22M3 is introduced with enhanced features to overcome the disadvantages of its predecessor. This aircraft completed its first flight in June 1977 and was installed in inventory in 1983. Some Tu-22Ms were also modified to Tu-22MR and Tu-22ME standards. The Russian Ministry of Defense intends to increase up to 30 aircraft from around 60 Tu-22M3 which are currently in service to the advanced Tu-22M3M variant. The first modernized aircraft was launched during the launch ceremony at the Kazan Aviation Plant. It made its maiden flight on December 28, 2018.

Tupolev Tu-22M3 Strategic Bomber

Tupolev Tu-22M3 Specs

The Tupolev Tu-22M3 incorporates a variable wing length design. This aircraft has a stepped cockpit and variable-geometry outer wing panels. The tail fin is swept back and tapered with a square tip. Flats mounted in the middle of the body are shown with a blunt end and each wing includes a middle and two outer panels. The outer wing attaches to the center through a hinged joint.

Overall, the Tu-22M3 has a length of 42.4 m, a maximum wing span of 34.2 m, and a height of 11.05 m. The maximum empty weight and takeoff weight of the aircraft are 53,500 kg and 126,400 kg, respectively.

The Tupolev Tu-22M3 is equipped with a tricycle landing gear to support operations on unprepared runways. The nose includes twin wheels that are pulled back. Each main landing unit consists of six wheels in a 2 × 3 bogie arrangement. These are pulled directly into the fuselage.

Tupolev Tu-22M3 Specs

Tupolev Tu-22M3 Engine

The Tu-22M3 is powered by two Kuznetsov NK-25 turbofan engines mounted on the body with large air intakes and dual exhausts. Each engine produces a maximum thrust of 25,000 kg and results in better fuel savings.

The Tupolev Tu-22M3 has a cruise speed of 900 km/ h and a maximum speed of 2,300 km/ h. This aircraft can fly at a maximum altitude of 14,000 m and the level of climbing aircraft is 15 m/ s. The operational range of the aircraft is 7,000 km. This aircraft can be equipped with refueling probes to enable refueling in flight for longer distances.

Tupolev Tu-22M3 Cockpit

Tupolev Tu-22M3 Cockpit and Avionics

The Tupolev Tu-22M3 semi-glass cockpit can accommodate four crew members on an ejection seat that leads upwards. This is equipped with a special panel for pilots, navigator-operators and commanders, with entrances provided through individual doors. The pressurized cockpit is equipped with a climate control system.

Tupolev Tu-22M3 Sensor and Radar

The Tupolev Tu-22M3 aircraft is equipped with a PN-A/ PN-AD blasting-navigation radar system, an Argon-2 radar fire control system and a TV-based bomb backup optical sight. Countermeasures are provided by updated radar warning receivers, radio frequency jammers, and defensive countermeasures.

Tupolev Tu-22M3 Engine

Tupolev Tu-22M3 Weapons

The Tupolev Tu-22M3 aircraft has a number of hard points that can be armed with Kh-32 missiles which are sophisticated derivatives of Raduga Kh-22 or US-4 Kitchen Cold War era, Kh-15 or Kh-15P anti-radar missiles, and bombs dropped free FAB-250 or FAB-1500. Wingparts and fuselage and internal weapons chambers are provided with the capacity to carry 24,000 kg of cargo. The aircraft is also armed with a GSH-23 double barrel (23 mm) pistol in the tail tower that is controlled remotely.

Tupolev Tu-22M3 Price

The price of the latest Tupolev Tu-22M3 Strategic Bomber is around US $ 40 Million.