ATR 72-600
ATR aircraft are suitable for all business models and every region around the world, in any type of conditions (cold, hot, high altitude runways, harsh environments, etc.) and a wide range of airports (steep approach, unpaved airfields and short or narrow runways). Their broad appeal and flexibility lead to strong asset values and wide acceptance of the aircraft in the airline and financing community.
With its lighter structure, optimised speed and an engine designed for short sectors, the ATR 72-600 is by far the most fuel-efficient regional aircraft. ATR’s fuel burn advantage drives lower costs and emissions and makes it the optimal aircraft for regional markets. The ATR 72-600 is the benchmark aircraft on the regional market, offering unbeatable economics. Operating costs on competing turboprop aircraft are 20% higher than ATR, while regional jets are at least 40% higher.
- Cruise speed: 510 km/h
- 70 seats
- Range: 1,528 km
- Fuel/seat km: 0,253 l/10 km
- Custom catering concepts
- WC
- Cabin crew
- Oven
Specifications Factsheet
Performance
| Take-off power | Take-off power – One engine | Max continuous | Max climb |
|---|---|---|---|
| 2, 475 SHP | 2, 750 SHP | 2, 500 SHP | 2, 192 SHP |
| Max cruise |
|---|
| 2, 132 SHP |
Ceiling
Blades: 6: Diameter: 3,93 m – 12,9 ft
Hamilton Standard
568F
Weight
| Max take-off weight (basic) | Max take-off weight (option) | Max landing weight (basic) | Max zero fuel weight (basic) |
|---|---|---|---|
| 22,800 kg – 50,265 lb | 23,000 kg – 50,705 lb | 22,350 kg – 49,272 lb | 20,800 kg – 45,855 lb |
| Max zero fuel weight (option) | Operational empty weight (Tech. spec.) | Operational empty weight (Typical in-service) | Max payload (at typical in-service OEW) |
|---|---|---|---|
| 21,000 kg – 46,296 lb | 13,311 kg – 29,346 lb | 13,500 kg – 29,762 lb | 7,500 kg – 16,534 lb |
| Max fuel load |
| 5,000 kg – 11,023 lb |
Airfield performance
| Take-off Distance: Basic (MTOW – ISA – SL) | Option (MTOW – ISA – SL) | at TOW for 300 Nm – Max pax – SL – ISA | at TOW for 300 Nm – Max pax – 300 ft – ISA + 10 |
|---|---|---|---|
| 1,333 m – 4,373 ft | 1,367 m – 4,485 ft | 1,175 m – 3,855 ft | 1,410 m – 4,626 ft |
| Take-off speed (V2 min @ MTOW): 116 KCAS. Landing field length (JAR25), Basic (MLW – SL) | At LW (max pax + reserves) – SL | Reference speed at landing |
|---|---|---|
| 914 m – 2,299 ft | 863 m – 2,832 ft | 133 KIAS |
En-route performance
| Optimum climb speed | Rate of climb (ISA, SL, MTOW) | Max cruise speed (95% MTOW – ISA – Optimum FL) | Fuel flow at cruise speed |
|---|---|---|---|
| 170 KCAs | 1,355 ft/min | 275 KTAS – 510 km/h | 762 kg/h – 1,680 lb/h |
| Range with max pax (70 seats) | 200 Nm block fuel | CO2 Emission | 200 Nm block time |
|---|---|---|---|
| 825 Nm | 618 kg – 1,363 lb | 1,947 kg – 4,292 lb | 55,6 min |
| 300 Nm block fuel | CO2 Emission | 300 Nm block time |
|---|---|---|
| 859 kg – 1,894 lb | 2,706 kg – 5,966 lb | 78,0 min |
