ATR 72
First flight year — 1988
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ATR 72 Specifications
| ATR 72-200 | ATR 72-500 | |
| Dimensions | ||
| Length (m) | 27.2 | 27.2 |
| Wingspan (m) | 27.0 | 27.0 |
| Height (m) | 7.6 | 7.6 |
| Wing area (m2) | 61.0 | 61.0 |
| Weight | ||
| Maximum take-off weight (kg) | 21 500 | 22 000 - 22 800 |
| Maximum landing weight (kg) | 21 850 | |
| Operating empty weight (kg) | 12 400 | 12 950 |
| Maximum zero fuel weight (kg) | 20 000 - 20 800 | |
| Maximum payload (kg) | 7 050 - 7 350 | |
| Standard fuel capacity (litres) | 6 400 | |
| Performance | ||
| Range with max payload (km) | 1 195 | 1 330 - 1 650 |
| Cruise speed (km/h) | 460 | 510 |
| Maximum speed (km/h) | 525 | 640 |
| Maximum operating altitude (m) | 7600 | 7 600 |
| Take-off field length (m) | 1 220 | |
| Landing field length (m) | 1 050 | |
| Engines | P&WC PW124B, 2 x 2160 hp | P&WC PW127F, 2 x 2750 hp |
| Cabin Data | ||
| Passengers (1-class) | 64-74 | 62-74 |
| Economy seat pitch (cm) | 76-81 | 76-81 |
| Cabin width (m) | 2.57 | 2.57 |
Typical Cabin Configuration of ATR 72
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