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Wednesday, 21 August 2019

ATR 72-500 Specs, Interior, Cockpit, and Price

22:31
ATR 72-500 Specs, Interior, Cockpit, and Price – ATR 72-500 is a regional twin-engine turboprop aircraft produced by Aerospatiale between 1997 and 2011. ATR, a joint venture formed by French aerospace company Aérospatiale and Italian aviation conglomerate Aeritalia (Alenia), with its headquarters in Toulouse.

The inaugural flight of the ATR 72-500 was completed in October 1988 and the aircraft began operating in October 1989. The ATR 72-500 is certified to operate on an unpaved runway by installing kits to ensure landing gear and lower fuselage protection. Special cold weather procedures allow operation at temperatures as low as -54 ° C.

ATR 72-500

ATR 72-500 Specs

ATR 72-500 is a high-wing monoplan aircraft with a fail-safe semi-monocoque fuselage built from light alloy. Composite materials make up 19% of the total structure weight. Composite materials include monolithic carbon structures, carbon / Nomex sandwiches and Kevlar / Nomex sandwiches, which are used for the main structure including horizontal tailplane and steering and outer wing box parts, as well as for secondary structures, including ailerons, engine covers and covers.

Alenia Aeronautica manufactures aircraft and tail units and is responsible for mounting landing gear. The wings are produced and tested at EADS Sogerma in Bordeaux. ATR in Toulouse is responsible for the final assembly and delivery to the customer.

ATR 72-500 is equipped with a hydraulically retractable three-wheel type landing gear, with Messier landing wheels, Dunlop wheels and brakes, Hydro-Aire Crane anti-skid control and Michelin tires. Goodyear tires are optionally installed for operation on unpaved runways. The Magnaghi hydraulic system strengthens the revocation of the landing gear and also serves other systems on the aircraft.

ATR 72-500 Engine

ATR 72-500 aircraft are powered by two PWF 127F. Maximum continuous thermodynamic power is 2,509 kW (3,365 shp) and 2,050 kW (2,750 shp) mechanical power for each engine, available up to 45 ° C. The aircraft is equipped with two integral fuel tanks having a fuel capacity of 5,700 l.

Standard 568F six-bladed Hamilton propeller equipped with electronic propeller control. All propellers are balanced, the pinner is made of aluminum and the engine cover is made of carbon / Nomex sandwich or Kevlar / Nomex sandwich construction. Engine intake in Kevlar / Nomex sandwiches is reinforced with a rigid carbon coating.

ATR 72-500 can sail with a maximum speed of 518 km / hour. The range and ceiling of aircraft services are 1,500 km and 7,620 m, respectively. This aircraft weighs around 12,950 kg and the maximum take-off weight is 22,500 kg.

ATR 72-500 cockpit

ATR 72-500 Cockpit and Avionics

The ATR 72-500 navigation system is based on the Honeywell Trimble HT1000 (GNSS) global navigation satellite sensor. The standard navigation system meets the latest rules and safety requirements, including CAT I AFCS. ATR aircraft are certified for ILS CAT II operations with a decision height of 80 feet available as an option.

The HT1000 GNSS system is combined with an automatic pilot, electronic flight instrumentation system (EFIS) and with a VHF omnidirectional radio starting steering guide with distance measuring equipment data (VOR / DME).

The ATR 72-500 aircraft is equipped with Rockwell Collins TTR 921 radar for ACAS II. Honeywell Primus 660 weather radar is displayed in four colors on the electronic horizontal situation indicator (EHSI).

Weather radar can also be used in MAP mode to display obstructions on land. Honeywell MARK VIII is enhanced with a ground proximity warning system (E-GPWS) integrating warning and terrain awareness display, along with cleaning the terrain floor in an electronic flight information system (EFIS).

ATR 72-500 interior

ATR 72-500 Cabin and Interior

ATR 72-500 aircraft can carry up to 74 passengers in a configuration of four aisles behind. Standard configuration includes two cargo compartments. The 5.8 m front cargo compartment is located between the flight deck and the passenger cabin and the 4.8 m rear compartment is behind the passenger cabin. The maximum load is 7,450 kg.

The ATR 72-500 aircraft cabin is equipped with a quick change kit to provide fast change capability for passenger and container transportation operations and separately ATR cargo conversion to convert aircraft into cargo.

The quick replacement kit provides the ability to reconfigure the cabin in 45 minutes to carry ATR special containers using standard front cargo doors.

This kit allows ATR 72-500 aircraft to be operated as passenger aircraft during the day and as a cargo plane at night. Each optimized container has a volume of 2.8 m³ and can transport goods up to a total weight of 500 kg. ATR 72 can carry up to 13 ATR containers.

ATR 72-500 Price and Orders

The price of the latest ATR 72-500 aircraft is around US $ 14.4 Million. Air Algeria awarded a $ 82 million contract to ATR in December 2009 to supply four ATR 72-500 aircraft. The first of the four aircraft was sent in February 2010 when the ceremony was held in Toulouse. In June 2011, the ATR 72-500 shipment to Air Algeria was concluded, increasing the aircraft fleet to 12.

As of January 2011, 1,074 aircraft (423 ATR 42s and 651 ATR 72s) were ordered, of which 915 (412 ATR 42s and 503 ATR 72s) were delivered. In October 2009, Air Vanuatu received a new ATR 72-500, configured with 68 seats and was powered by a 127 million PW engine under a $ 20.5 million contract signed in 2008.

The Royal Thai Air Force received the first of four ATR 72-500 aircraft in September 2009. The contract to purchase four ATR 72-500 was signed in 2007. All shipments have been completed.

In 2008, TAT Group received 40 ATR 72-500. Vietnam Airlines bought six ATR-500s in 2008. Orders in 2007 included TRIP Linhas Aereas (seven) in January, Swiftair (three) in April, Malaysia Airlines (20) in June 2007, Batavia (ten) in August, Vietnam Airlines (11) , Berjaya Air (four) and Malaysia Airlines (20) in December.

Monday, 19 August 2019

ATR 42-600 Specs, Interior, Cockpit, and Price

01:00
ATR 42-600 Specs, Interior, Cockpit, and Price – ATR 42-600 is a twin turboprop passenger aircraft developed and produced by Aerospatiale and Aeritalia. ATR, with headquarters in Toulouse, is a joint venture between EADS and Finmeccanica / Alenia Aeronautica.

ATR 42-600 is a new generation aircraft equipped with new engines, new propellers, increased heat and high performance, increased weight capacity and increased passenger cabin. ATR 42-600 was certified in 2012.

Another variant of the ATR 42 aircraft is the ATR 42MP which is an aircraft for maritime patrol, operating with Guardia in Finanza Italia (three aircraft) and coast guard (two aircraft).

ATR 42-600

ATR 42-600 Specs

ATR 42-600 is a high wing monoplan with a fail-safe semi-monocoque fuselage made of light alloy. Composite materials, such as monolithic carbon structures, carbon / Nomex sandwiches and Kevlar / Nomex sandwiches, are widely used and represent 19% of the total structure weight.

Alenia Aeronautica is responsible for making the fuselage, tail unit and landing gear installation. The wings are produced and tested at EADS Sogerma, in Bordeaux. ATR has full responsibility for the final assembly and delivery to the customer.

Specifications for special variants such as the ATR 42MP are equipped with search radars, Galileo Avionica mission systems, electronic support measures Elettronica (ESM), forward-looking infrared (FLIR) and TV cameras. The aircraft can spend up to eight hours at the station, at 200nm from the base.

ATR 42-600 Engine

The ATR 42-600 is powered by two Pratt & Whitney Canada PWC 100 Series turboprop engines. This engine is equipped with two six-bladed Hamilton Sundstrand 568F propellers with Propeller Electronic Control. Blades are all counterweighted. Pinner is made of aluminum, while the engine cover is made of carbon / Nomex sandwich or Kevlar / Nomex sandwich. Engine intake is in Kevlar / Nomex sandwiches with a rigid carbon coating.

Thermodynamic power, under maximum continuous conditions, is 2,315 kW (3,148 shp) and mechanical power is 1,765 kW (2,400shp) for each engine. To support this large engine power, the ATR 42-600 equipped with two integral fuel tanks can carry 5,700 liters of fuel.

A pneumatic de-icing system is provided for engine air intake, edge leading edges, and horizontal tailplane edges. The electric anti-icing system is installed for the propeller blades, windshield and horn.

This aircraft has a tricycle that can be pulled hydraulically. Landing landing feet are provided by Messier, wheels and brakes by Dunlop, anti-slip control by Hydro-Aire cranes and tires by Michelin (or optional Goodyear tires for operation on non-paved runways). Magnaghi's hydraulic system provides landing gear retraction and also serves other systems on the plane.

ATR 42-600 interior

ATR 42-600 Cabin and Cargo

ATR 42-600 can carry up to 70 passengers in a four-aisle configuration. Standard configuration includes two cargo compartments. The 4.8 m front cargo compartment is located between the flight deck and the passenger cabin and the 4.8 m³ rear compartment is located behind the passenger cabin.

The ATR 42-600 cab is equipped with a quick replacement kit that has the ability to reconfigure the cabin in 30 minutes to carry ATR special containers using standard front cargo doors.

This kit allows the aircraft to operate as a passenger plane during the day and as a cargo plane at night. Each optimized container has a volume of 2.8m³ and can transport goods up to a total weight of 500kg. ATR 42 can carry up to nine ATR containers.

The standard front cargo door of 1.52m × 1.27m can be replaced with a large cargo door of 2.95mx1.8m to carry standard container unit (ULD) containers, such as LD3 and 88in × 108in containers.

ATR 42-600 can carry five LD3 containers plus 10.0 m³ for bulk shipments. The alternative load arrangement consists of three 88in × 108in containers, one 63in × 88in container and an additional 11.9 m³ of bulk transportation.

ATR 42-600 cockpit

ATR 42-600 Cockpit and Avionics

ATR 42-600 is equipped with Rockwell Collins TTR 921 radar for ACAS II. Honeywell Primus 660 weather radar is displayed in four colors on the electronic horizontal situation indicator (EHSI). Weather radar can also be used in MAP mode to display obstructions on land. Honeywell MARK VIII is enhanced with a ground proximity warning system (E-GPWS) integrating warning and terrain warning display, plus cleaning the terrain floor in an electronic flight information system (EFIS).

ATR 42-600 is equipped with a digital Thales avionics suite that includes five LCD screens, a new flight management system, new communication, a new navigation system with a global navigation satellite system / wide area augmentation system (GNSS / WAAS) and a new automatic pilot for the CAT III approach .

ATR 42-600 Price and Orders

The price of the latest ATR 42-600 aircraft is around US $ 19.5 Million. At present, 30 ATR cargoes are operating with 12 carriers, while 27 ATR 42-320 for FedEx are in conversion. Only two of these aircraft are equipped with large cargo doors: one ATR 72 is operated by Farnair and one ATR 42 is flown by Northern Air Cargo Alaska. FedEx aircraft are equipped with standard cargo doors.

Saturday, 17 August 2019

ATR 42-500 Specs, Interior, Cockpit, and Price

01:00
ATR 42-500 Specs, Interior, Cockpit, and Price – Regional Avions de Transport (ATR) 42-500 or is a regional commuter civil airplane turboprop with a capacity of 42 passengers made by Aerospatiale in France and Aeritalia in Italy . ATR 42-500 aircraft were produced by the two companies between 1994 and 2012.

Aerospatiale and Aeritalia initially made the ATR (Avions de Transport Regional) series for local flights. The ATR 42 was the first series to be launched in October 1981. The first prototype went on air on August 16, 1984, received airworthiness certification from France and Italy in September 1984 and in December 1984 began operating by airlines. Despite many improvements, only in 1995 was launched ATR 42-500 with a more powerful engine than the previous variant, 6-bladed propeller and a computerized cockpit.

ATR 42-500

ATR 42-500 Specs

ATR 42-500 has a length of 22.67 m, a height of 7.59 m, and a wing span of 24.57 m. This aircraft has an empty weight of 11,250 kg and a maximum weight at take-off of 18,600 kg. It has a maximum take-off weight of 41,005 lbs and a maximum landing weight of 40,344 lbs.

The ATR 42-500 aircraft is driven by two Hamilton blades with a six-bladed Hamilton Sundstrand 568F propeller electronic control. Blades are all counterweighted. Pinner is made of aluminum, while the engine cover is made of carbon / Nomex sandwich or Kevlar / Nomex sandwich. Engine intake is in Kevlar / Nomex sandwiches with a rigid carbon coating.

A pneumatic de-icing system is provided for engine air intake, edge leading edges, and horizontal tailplane edges. The electric anti-icing system is installed for the propeller blades, windshield and horn.

The landing mechanism on the ATR 42-500 aircraft is equipped with a hydraulically retractable tricycle. Landing landing feet are provided by Messier, wheels and brakes by Dunlop, anti-slip control by Hydro-Aire cranes and tires by Michelin (or optional Goodyear tires for operation on non-paved runways). Magnaghi's hydraulic system provides landing gear retraction and also serves other systems on the plane.

ATR 42-500 Engine

The ATR 42-500 is powered by two Pratt & Whitney Canada PWC 127Es turboprop engines capable of producing power in maximum continuous conditions of 2,315 kW (3,148 shp) and mechanical power of 1,765 kW (2,400shp) for each engine. This machine is equipped with 6 blades blades. This aircraft has a maximum speed of 563 km / h (304 miles / hour) with a cruise range of 1,850 km.

To support such large engine power, the ATR 42-500 is equipped with two integral fuel tanks that can carry 5,700 liters of fuel. Cruise speeds vary greatly during flights, during climbing, sailing, and descent. In addition, there is a speed limit of 250 knots under 10,000 feet which will have an impact on the average speed for shorter flights which is greater than longer flights.

ATR 42-500 interior

ATR 42-500 Cabin and Interior

The ATR 42-500 cabin is 31.3 feet long, 8.3 feet wide and 6.3 feet high, giving a total cabin volume of 1,631.9 cubic feet. With its large cabin, the ATR 42-500 can carry up to 50 passengers in a four-aisle configuration. Standard configuration includes two cargo compartments.

In addition to the standard configuration, ATR 42-500 can be specially configured to accommodate the specific needs of the operator. The ATR 42 cab is equipped with a quick replacement kit that has the ability to reconfigure the cabin in 30 minutes to carry ATR special containers using a standard front cargo door.

Front standard cargo doors of 1.52 m × 1.27 m can be replaced with 2.95m × 1.8m large cargo doors to carry standard load unit (ULD) container devices, such as LD3 and 88 in × 108 in containers.

ATR 42-500 cockpit

ATR 42-500 Cockpit and Avionics

The ATR 42-500 cockpit is equipped with Rockwell Collins TTR 921 radar for ACAS II. Honeywell Primus 660 weather radar is displayed in four colors on the electronic horizontal situation indicator (EHSI). Weather radar can also be used in MAP mode to display obstructions on land. Honeywell MARK VIII is enhanced with a ground proximity warning system (E-GPWS) integrating warning and terrain warning display, plus cleaning the terrain floor in an electronic flight information system (EFIS).

The ATR 42-500 navigation system is based on the Honeywell Trimble HT1000 global navigation satellite sensor (GNSS). The HT1000 GNSS system is combined with an automatic pilot, electronic flight instrumentation system (EFIS) and with a VHF omnidirectional radio starting steering guide with distance measurement equipment (VOR / DME) data.

ATR 42-500 Price and Orders

The price of the latest ATR 42-500 aircraft is around US $ 12.1 Million. At present, 343 ATR 42-500 have been ordered and 336 have been sent to every airline in the world.

Thursday, 15 August 2019

Boeing Business Jet (BBJ) MAX 7 Specs, Interior, Range, and Price

00:00
Boeing Business Jet (BBJ) MAX 7 Specs, Interior, Range, and Price – Boeing Business Jet (BBJ) MAX 7 is the latest variant in the BBJ MAX family of aircraft, which is designed to offer high quality, mobility, and comfort for passengers. BBJ MAX 7 is the optimal combination of size, performance, efficiency and comfort. It offers improved aerodynamics, an updated flight deck, and a 40% reduced noise profile. Flying wire spoilers improve flight control and provide easy maneuverability.

BBJ MAX 7

BBJ MAX 7 Specs

BBJ MAX 7 has a dihedral-swept wing configuration with split-tip winglets, which use laminar airflow to reduce drag. Tip-tip winglets increase effective wing span, result in higher fuel savings, and increase range up to 2.5% during long-haul flights.

BBJ MAX 7 has a length of 35.6m, height of 12.3m, and has a wingspan of 35.9m. This business jet has an mechanically movable automatic air ladder that is integrated, allowing hassle-free boarding and deboarding. The ladder with integrated handrails can automatically re-enter its compartment under the main cabin.

BBJ MAX 7 Engine

BBJ MAX 7 is powered by a CFM LEAP-1B engine. The optimized engine core and fan, which is 8in longer in diameter than the B737 engine fan, has a higher bypass ratio.

This business jet offers a greater range than BBJ MAX 8 and BBJ MAX 9. It can fly up to 12,966 km with eight passengers on board and can last up to 12,412 km while carrying 19 passengers.

The maximum usable fuel carried by BBJ MAX 7 is 39,735l, while the maximum take-off weight is 80,286 kg. This aircraft has a maximum landing weight of 66,043 kg.

The maximum zero fuel weight of the aircraft is 62,913 kg and the operating empty weight is 48,060 kg. The interior weight allowance for the cabin is 7,257kg.

BBJ MAX 7 interior

BBJ MAX 7 Interior and Cabin

BBJ MAX 7 offers additional passenger cabin space than traditional BBJ. MAX 7 has a luxurious, spacious and comfortable cabin for a relaxed and at home experience while flying. The spacious cabin has a cross section length of 3.53m, which allows the free movement of passengers.

BBJ MAX 7 cabin is 1.93 m longer than normal BBJ. The total cabin length is 26.11m, while the total area is 82.13m². The cabin offers a spacious living room, furnished business room, dining room, private room, kitchen and bath. This business jet provides 275ft³ of cargo space under the deck despite having an additional fuel tank.

This variant offers high passenger comfort by providing a lower cabin height. This maintains a maximum cabin height of 6,500 feet in maximum cruising altitude, while the average cabin pressure that is maintained during long distance flights is 5,600 feet.

The BBJ MAX 7 flight deck accommodates a new large format display with additional graphics and an improved pilot interface.

BBJ MAX 7 cockpit

BBJ MAX 7 Price and Orders

The price of BBJ MAX 7 is around US $ 91.2 Million. Boeing received its first order for delivery of MAX 7 aircraft from Orient Global Aviation in December 2016. Seacons Trading ordered the BBJ MAX 7 during the 2018 Farnborough International Airshow which was held in July 2018.

Sunday, 11 August 2019

XTI TriFan 600 Specs, Interior, Cockpit, and Price

01:00
XTI TriFan 600 Specs, Interior, Cockpit, and Price – TriFan 600 is a six-seat VTOL aircraft that is being developed by the XTI Aircraft Company, Denver, US. The aircraft was developed as the world's first long-distance  vertical take-off and landing (VTOL) jet. XTI developed the TriFan 600 aircraft to target business flights, and high-value corporate and individual executives. The company expects to sell between 40 and 100 TriFan 600 aircraft per year.

XTI began its preliminary design to develop the first prototype TriFan 600 aircraft in November 2015. Honeywell Aerospace was contracted to supply the HTS900 engine for use in the first prototype in August 2016. The scope of the contract also included an additional engine for the XTI for land propulsion test systems.

XTI TriFan 600 VTOL

XTI TriFan 600 Specs

TriFan 600 aircraft will be built using carbon fiber and epoxy structures. The initial design of the aircraft involved work on computational fluid dynamics (CFD), including wind tunnel testing using computers.

The aircraft will include three fans channeling 72in and two wing fans. It takes off vertically using three fan channels and the wing fan will spin forward to offer a transition for high-speed flights. The aircraft can also land vertically on a paved surface the size of a helipad.

Aircraft can fly faster, have greater reach, and save time by eliminating trips to and from the airport, XTI said. This can take off directly from a paved helipad-sized space.

XTI TriFan 600 specs

XTI TriFan 600 Engine

TriFan 600 will be powered by two HTS900 turboshaft engines with high performance reaching 2,600HP. This machine was developed by Honeywell Aerospace. The engine will use a digital engine control system (FADEC) full dual channel authority with manual backup.

The TriFan 600 aircraft will have a maximum cruise speed of 630 km / h (390 mph), a maximum cruise height of 35.00 ft, and a range of 1,500 nm. This will reach maximum height in 11 minutes and maximum cruising speed in 90 seconds.

XTI TriFan 600 Cabin and Interior

The TriFan 600 aircraft will accommodate five passengers and one pilot, with adequate space for bags. This will display the comfort of a pressurized cabin integrated with a modern luxury seating arrangement with a stylish surface and interior. The aircraft will include a sliding door that will cover the third distributed fan for future flights.

XTI TriFan 600 interior

XTI TriFan 600 Cockpit and Avionics

The TriFan 600 aircraft will be equipped with a fly-by-wire flight control system that is integrated with advanced avionics. This will include the rules of a single pilot instrument flight (IFR) and will also feature advanced safety features, including autopilot and computerized controls for takeoff and landing.

XTI TriFan 600 Price

The estimated price of TriFan 600 is US $ 6.5 Million. Since its introduction at the 2017 National Business Aviation Association (NBAA) convention, XTI has received 76 orders for TriFan 600 aircraft. If all goes according to plan with the testing and certification process, it is expected that TriFan 600 will be shipped in 2023.