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The ATR ATR-72

Photos
More photos of ATR ATR-72

More passenger cabin photos...

More cockpit photos...

Powerplants
ATR-72-200 - Two 1610kW (2160shp) Pratt & Whitney Canada PW-124B turboprops driving four blade Hamilton Sundstrand propellers.
ATR-72-210 - Two 1850kW (2480shp) P&WC PW-127 turboprops driving four blade Hamilton Sundstrand propellers.
ATR-72-500 - Two 2051kW (2750shp) P&WC PW-127F turboprops driving six blade Hamilton Sundstrand propellers.
Performance
ATR-72-200 - Max cruising speed at 15,000ft 526km/h (284kt), economical cruising speed 460km/h (248kt). Range with reserves at max optional weight 1195km (645nm), range with 66 pax 2665km (1200nm).
Weights
ATR-72-200 - Operating empty 12,400kg (27,337lb), max takeoff 21,500kg (47,400lb), optional 22,000kg (48,501lb).
ATR-72-210 - Operating empty 12,450kg (27,447lb), max takeoff same as ATR-72-200.
ATR-72-500 - Operating empty 12,950kg (28,550lb), max takeoff 22,000kg (48,501lb), optional 22,500kg (49,604lb).
Dimensions
Wing span 27.05m (88ft 9in), length 27.17m (89ft 2in), height 7.65m (25ft 1in). Wing area 61.0m2 (656.6sq ft).
Capacity
Flightcrew of two. Max seating for 74 passengers at four abreast and 76cm (30in) pitch. More typical seating for between 64 and 70 passengers, with seat pitch starting from 81cm (32in). With larger forward freight door fitted it can accommodate a payload of 7200kg (15,875lb) in 13 containers. ATR-52C - 7500kg (16,535lb) payload comprising pallets or five LD3 containers.
Production
As at late 2001 292 ATR-72s had been ordered, with 270 delivered.
Type
70 seat turboprop regional airliner

History

The ATR-72 is a stretched development of the popular ATR-42 and was launched in January 1986.

The first of three ATR-72 development aircraft flew for the first time on October 27 1988, followed by the awarding of French and then US certification in late 1989. Entry into service was on October 27 1989 with Kar Air of Finland. Some other early operators are Foshing Airlines, NFD (later Eurowings), CSA, American Eagle, TAT, Air Littoral, LOT, and Olympic Aviation.

Significant differences between the ATR-72 and the smaller and older ATR-42 include a 4.50m (14ft 9in) fuselage stretch and reworked wings. The ATR-72's wings are new outboard of the engine nacelles and with 30% of it made up of composite materials, comprising composite spars and skin panels and a carbon fibre wing box.

Aside from the baseline ATR-72-200, two developments have been offered, the ATR-72-210, and the ATR-72-500 (previously ATR-72-210A). The ATR-72-210 is optimised for operations in hot and high conditions. It has more powerful PW-127 engines for better takeoff performance.

The ATR-72-500 (renamed from ATR-72-210A on May 18, 1998) further improved hot and high model was certificated in early 1997. It features PW-127Fs driving six blade composite Hamilton Sundstrand propellers.

The ATR-52C is an as yet unlaunched derivative with a redesigned tail to incorporate a rear loading ramp, intended for military and commercial operators. As with the ATR-42, a military maritime patrol version, known as the Petrel 72, has also been offered.

The ATR-72 would have formed the basis for the ATR-82, a 78 seat stretched development. The ATR-82 would have been powered by two Allison AE-2100 turboprops (ATR studied turbofans for a time) and would have a cruising speed as high as 610km/h (330kt). The ATR-82 was suspended when AI(R) was formed in early 1996.

The ATR ATR-42

More photos of ATR ATR-42

More passenger cabin photos...

More cockpit photos...

Powerplants
ATR-42-300 - Two flat rated 1340kW (1800shp) Pratt & Whitney Canada PW-120 turboprops driving four blade c/s Hamilton Standard propellers.
ATR-42-320 - Two flat rated 1417kW (1900shp) PW-121s.
ATR-42-500 - Two PW-127Es derated to 1610kW (2160shp) driving six blade RatierFagiec/Hamilton Standard props.
Performance
ATR-42-300 - Max cruising speed 490km/h (265kt) economical cruising speed 450km/h (243kt). Range with max fuel and reserves at max cruising speed 4480km (2420nm), or 5040km (2720nm) at economical cruising speed.
ATR-42-320 - Same as ATR-42-300 except max cruising speed 498km/h (269kt).
ATR-42-500 - Cruising speed 563km/h (304kt). Max range 1850km (1000nm).
Weights
ATR-42-300 - Operating empty 10,285kg (22,674lb), max takeoff 16,700kg (36,817lb).
ATR-42-320 - Operating empty 10,290kg (22,685lb), max takeoff as per 42-300.
ATR-42-500 - Operating empty 11,250kg (24,802lb), max takeoff 18,600kg (41,005lb).
Dimensions
Wing span 24.57m (80ft 8in), length 22.67m (74ft 5in), height 7.59m (24ft 11in). Wing area 54.5m2 (586.6sq ft).
Capacity
Flightcrew of two. Maximum passenger accommodation for 50, 48 or 46 at 76cm (30in) pitch and four abreast. Typical seating arrangement for 42 at 81cm (32in) pitch.
ATR-42 Cargo - Nine containers with a 4000kg payload.
Production
As at late 1998 total orders for all versions of the ATR-42 stood at 343 with 336 delivered.
Type
42 seat turboprop regional airliner


History

Aerospatiale and Aeritalia (now Alenia) established Avions de Transport Regional as a Groupement d'Intéret Economique under French law to develop a family of regional airliners. The ATR-42 was the consortium's first aircraft and was launched in October 1981.

The first of two ATR-42 prototypes flew for the first time on August 16 1984. Italian and French authorities granted certification in September 1985 and the first ATR-42 entered airline service on December 9 1985.

The initial ATR-42-300 was the standard production version of the ATR-42 family until 1996 and features greater payload range and a higher takeoff weight than the prototypes. The similar ATR-42-320 (also withdrawn in 1996) differed in having the more powerful PW-121 engines for better hot and high performance, while the ATR-42 Cargo is a quick change freight/passenger version of the 42-300.

The ATR-42-500 is the first significantly improved version of the aircraft and features a revised interior, more powerful PW-127Es for a substantially increased cruising speed (565km/h/305kt) driving six blade propellers, a 1850km (1000nm) maximum range, the EFIS cockpit, elevators and rudders of the stretched ATR-72 (described separately), plus new brakes and landing gear and strengthened wing and fuselage for higher weights. The first ATR-42-500 delivery was in October 1995.

ATR was part of Aero International (Regional), the regional airliner consortium established in January 1996 to incorporate ATR, Avro and Jetstream. AI(R) handled sales, marketing and support for both the ATRs, plus the Avro RJs and the Jetstream 41, until its disbandment in mid 1998 when ATR regained its independence.

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