ATR 42 introducted in 1985 and produced until today . They were built 422 airplanes with average cost about $12-16 million.ATR 42 is a turboprop airliner for short-ranges . Airplane until today is Operational with varius airlines and made its first flight in 16 August 1984.. All airplanes were manufactured by ATR in France and Italy
Specifications
| ATR 42-200 | ATR 42-300 | ATR 42-320 | ATR 42-500 | ATR 42-600 | |
|---|---|---|---|---|---|
| Flight deck crew | 2 | ||||
| Seating, typical | 42–50 | ||||
| Length | 74 ft 5 in (22.67 m) | ||||
| Wingspan | 80 ft 7 in (24.57 m) | ||||
| Height | 24 ft 11 in (7.59 m) | ||||
| Wing area | 587 sq ft (54.5 m2) | ||||
| Wing aspect ratio | 11.1:1 | ||||
| Wheelbase | 28.8 ft (8.78 m) | ||||
| Cabin length | 45.4 ft (13.85 m) | ||||
| Empty weight | 23,148 lb (10,500 kg) |
24,802 lb (11,250 kg) |
|||
| Maximum takeoff weight (MTOW) |
34,280 lb (15,550 kg) |
37,258 lb (16,900 kg) |
37,258 lb (16,900 kg) |
41,005 lb (18,600 kg) |
|
| Cruise speed | 267 knots (494 km/h) at cruise altitude | 299 knots (554 km/h) at cruise altitude | 300 knots (560 km/h) at cruise altitude | ||
| Range, loaded | 480 nmi (885 km) | 840 nmi (1,555 km) | 842 nmi (1,560 km) | ||
| Maximum fuel capacity | 1,486 US gal (5,625 L) | ||||
| Service ceiling | 25,000 ft (7,600 m) | ||||
| Engines (×2) | Pratt & Whitney Canada PW120 | Pratt & Whitney Canada PW121 | Pratt & Whitney Canada PW127E | Pratt & Whitney Canada PW127M | |