ATR 72-212

The ATR 72 is a turboprop regional airliner that has been in service since 1989. It is derived from the ATR 42 with a 4.5 m stretched fuselage in order to increase seating capacity (from 48 to 66). The two aircraft feature a high degree of commonality: the same cross-section, and the same cockpit for cross-crew qualification. The derivative version of the basic ATR 72, the ATR 72-210 is equipped with two higher power 2,750 SHP PW127 engines.

The main characteristics of the 210 versions are excellent “hot & high” and short field capabilities. It also features enhancements to cabin comfort particularly in terms of advanced internal noise treatment and superior cabin air conditioning. A leader in its market segment, the ATR 72 has won hundred orders worldwide and achieves an in-service dispatch reliability largely exceeding 99%.

Aircraft Data

ATR 72-212 Specifications

• Origin of manufacture: France
• Place of maintenance: Europe
• Cockpit crew: 2
• Cabin crew: 2
• Passengers: 64 Passengers Maximum

External Dimensions

• Wingspan : 27.05 m / 88.7 ft
• Length: 27.22 m / 89.3 ft
• Height: 7.65 m / 25.1 ft

Main Cabin Dimensions

• Length: 17.95 m / 58.9 ft
• Width: 2.57 m / 8.4 ft
• Height: 1.91 m / 6.3 ft
• Volume cabin: 75.5 m3 / 2666.3 ft3

ATR 72-212 Door Sizes

• Passenger Door : 1.29 x 1.6 m / 50.9 x 62.8 in
• Cargo Door : 1.25 x 1.57 m / 49.4 x 6 in
• Rear Cargo Door : 0.65 x 1.22 m / 25.5 x 48.2 in

Baggage Compartment

• Volume : 13.5 m3 / 476.7 ft3
• Baggage per pax: 33 kg
• Maximum capacity: 2160 kg / 4762 lb

Operating Weight

• Max. Take-off Weight: 22000 kg / 48502 lb
• Max. Landing Weight: 21350 kg / 47069 lb
• Max. Zero Fuel Weight: 19700 kg / 43431 lb
• Empty Weight: 13519 kg / 29804 lb
• Maximum Payload: 6181 kg / 13627 lb
• Maximum Fuel Load: 5000 kg / 11023 lb

Performance

• Cruising Speed: 490 km/h / 265 kts
• Service Ceiling: 7620 m / 25000 ft
• Maximum Range: 1852 km / 1000 nm