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ATR 42/72

ATR 42/72

Turboprop Airplanes
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Basic Information
Name
ATR 42/72
Designation
ATR 42/72
Alternate Designation
Equipment Type
Turboprop Airplanes
Manufacturer
ATR
Date of Introduction
Description

In the early 1980s Alenia Aeronautica of Italy, a Finmeccanica company, and EADS/Airbus France founded a joint venture company, ATR (Avions de Transport Régional/Regional Transport Airplanes), to compete in the regional market with a new family of twin-turboprop passenger aircraft. The ATR 42 model entered service in 1985 followed by the increased seating capacity ATR 72 in 1989 all together these aircraft cover the range of 40 to 70 seats. The high-wing ATR 42/72 family of aircraft provides high degree of passenger comfort, operational flexibility, spare parts commonality, and low operating costs while delivering outstanding performance. In 1996, ATR launched the -500 series aircraft which marked the beginning of a new generation ATR 42/72 characterized for savings in terms of training, maintenance operations, spare parts supply and cross crew qualification. In addition, existing ATR 42/72 aircraft can be converted into freighters - ATR 42 F and ATR 72 F - with a cargo door at the front of the aircraft or an optional large cargo door. As of July 2005, more than 739 ATR 42/72 aircraft have been ordered from 125 operators in 72 countries with around 680 airplanes already delivered. The Pratt & Whitney Canada PW100 turboprop engine family is the primary motorization for the ATR 42/72 family with the latest variant the PW127 powering the newest ATR 72-500 aircraft. Wide use of composite in latest models has translated into reduced airframe weight and improved overall performance.

Air & Air Defense Specifications
Crew 2
Max Speed 558.0 km/h
Overview (Deagel)
Group Turboprop Airplanes
Status Active
Also Known As ATR 42 F, ATR 42-300, ATR 42-320, ATR 42-500
Origin France, Italy
Contractor ATR
Initial Operational Capability (IOC) 1985
Total Production 411
Unitary Cost USD $18.0 million
Specifications (Deagel)
Crew 2
Number of Engines 2
Passengers 50
Dimensions — Height 7.6 meter
Dimensions — Length 22.7 meter
Dimensions — Wingspan 24.5 meter
Mass — Empty Weight 11,250 kilogram
Mass — Max Takeoff Weight 18,600 kilogram
Mass — Payload 5,450 kilogram
Performance — Ceiling 3,750 meter
Power — Max Power at TakeOff 4,800 shp
Speed — Cruise Speed 155 mps
Gear (Deagel)
Item 1 Turboprop Engines: PW100 (2)
Variants
Variant 1 ATR 42
Variant 2 ATR 72
Variant 3 ATR 42 Surveyor
Variant 4 ATR 72 ASW
Variant 5 ATR 72-600
Variant 6 ATR 42-600
Variant 7 ATR 72-600F
Variant 8 ATR NEO
Details
Country of Origin France
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
22.7 m
Width
24.5 m
Height
7.6 m
Weight
18600 kg
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