72-200 specifications
- Max landing weight
- 21,350 kg (47,069 lb)
- Max zero-fuel weight
- 19,700 kg
- Max ramp weight
- 21,530 kg
Models & engines
| Model | Engines | Certified |
|---|---|---|
| ATR 72-101 | Pratt & Whitney Canada PW124B | 25 Sep 1989 |
| ATR 72-201 | Pratt & Whitney Canada PW124B | 25 Sep 1989 |
| ATR 72-102 | Pratt & Whitney Canada PW124B | 14 Dec 1989 |
| ATR 72-202 | Pratt & Whitney Canada PW124B | 14 Dec 1989 |
The ATR 72-200 is a landplane with 2 turboprop engines built by ATR. Air-traffic control and flight-tracking sites identify it by the ICAO type code AT72, while airline timetables and booking sites use the IATA code AT7. It belongs to the medium wake-turbulence category.
72-200 size and dimensions
The 72-200 is has a wingspan of 26.82 m.
72-200 weight and fuel
The maximum take-off weight is 21,500 kg (47,399 lb) and it may land at up to 21,350 kg — 99% of take-off weight. Among turboprops it ranks #4 of 13 by weight. Without fuel it may weigh at most 19,700 kg, leaving up to 1,800 kg for fuel at maximum take-off weight.
72-200 speed and range
On final approach it flies at around 114 knots (211 km/h).
72-200 models and engines
Our database lists 4 certified models of the 72-200: ATR 72-101, ATR 72-201, ATR 72-102 and ATR 72-202. The first was certified in September 1989, the latest in December 1989. Engines come from Pratt & Whitney Canada.
Aircraft similar to the 72-200
Comparable turboprops include Grumman S-2 Turbo Tracker, Grumman E-2 Hawkeye, Airbus Defence and Space CN235 and Antonov An-70.
Frequently asked questions
What is the ICAO code of the ATR 72-200?
How big is the ATR 72-200?
Which engines does the ATR 72-200 use?
Data: What is flying? database (ODbL 1.0). Live traffic: adsb.lol (ODbL). Photos under their Creative Commons licences, credited above.