Wednesday, 21 August 2019

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

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.

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