ARMSNET
Military Equipment Database
Initializing 0%

ATR 72-600

ATR 72-600

Turboprop Airplanes
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
ATR 72-600
Designation
ATR 72-600
Alternate Designation
Equipment Type
Turboprop Airplanes
Manufacturer
ATR
Date of Introduction
2011
Description

The ATR 72-600 is a further development of the ATR 42 aircraft family encompassing the latest technological enhancements while building upon the proven ATR 72-500 airframe and retaining thus the low fuel burn and operating cost. The -600 series aircraft family was announced early in October 2007 and was projected for delivery in the second of 2010 replacing the -500 series aircraft as production standard. The new airplane will represent a major boost in avionics, engine performance, cabin comfort and LED technology for the ATR 42/72 aircraft family. The ATR 72-600 turboprop aircraft will feature the Pratt & Whiney PW127M engine with increased power which translates into aircraft's improved performance for hot climate and high conditions. Additionally, the ATR 72-600 will have a maximum take-off weight increase of 300 kg helping to cope with demands for more weight available for passenger and baggage. ATR will introduce extensively more durable and energy efficient LED (Light Emitting Diode) technology replacing the lighting systems inside the cabin and external navigation and anti-collision lights as well. The new avionics suite meant for the -600 series will include a glass cockpit with 5 wide LCD screens replacing the current EFIS system and provided with upgraded avionics instrumentation which encompasses navigation, recording, auto- pilot and communications. ATR project to provide the new aircraft with a multi-purpose computer (MPC) for safer and more reliable operations. In addition to the upgraded performance, the new avionics suite will result lighter, more durable and reliable with a lower energy consumption.

Air & Air Defense Specifications
Range 1664.9 km
Overview (Deagel)
Group Turboprop Airplanes
Status Active
Origin France, Italy
Contractor ATR
Initial Operational Capability (IOC) August 19, 2011
First Flight October 1, 2009
Total Production 770
Unitary Cost USD $25 million
Specifications (Deagel)
Number of Engines 2
Passengers 74
Mass — Max Takeoff Weight 23,000 kilogram
Mass — Payload 7,500 kilogram
Performance — Max Range 899 nautical mile
Power — Max Power at TakeOff 5,500 hp
Gear (Deagel)
Item 1 Turboprop Engines: PW127M (2)
Item 2 Turboprop Engines: PW127XT-M (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
Width
Height
Weight
23000 kg
Operators (43)
United States
France
United Kingdom
Japan
South Korea
Sweden
India
Iran
Brazil
Spain
Algeria
Argentina
Austria
Bahamas
Botswana
Canada
Colombia
Denmark
Gabon
Greece
Indonesia
Ireland
Laos
Madagascar
Malaysia
Maldives
Mexico
Morocco
Myanmar
New Zealand
Papua New Guinea
Philippines
Romania
Saudi Arabia
Senegal
Singapore
Taiwan
Tanzania
Thailand
Trinidad and Tobago
Tunisia
United Arab Emirates
Uzbekistan
Something went wrong. Please reload the page. Reload