The BAe ATP is a twin-engined turboprop regional airliner with a capacity of maximum 72 passengers produced by the British manufacturer BAe, British Aerospace (today BAE Systems).
| Crew | 2 | |
| Passengers | max. 72 | |
| Propulsion | 2 Turboprop Engines | |
| Engine Model | Pratt & Whitney Canada PW126A | |
| Engine Power (each) | 1978 kW | 2653 shp |
| Speed | 493 km/h | 266kts |
| Service Ceiling | 7.620 m | 25.000ft |
| Range | 1.824 km | 985 NM |
| Empty Weight | 14.193 kg | 31.290lbs |
| max. Takeoff Weight | 22.930 kg | 50.552lbs |
| Wing Span | 30,63 m | 100,5 ft |
| Wing Area | 78,3 m² | 843 ft² |
| Length | 26,00 m | 85,3 ft |
| Height | 7,14 m | 23,4 ft |
| First Flight | 01.04.1984 | |
| Production Status | out of production | |
| Total Production | 64 | |
| Developed from | Hawker Siddeley HS 748 | |
| Data for (Version) | BAe ATP |
Remarks
The ATP -(A)dvanced (T)urbo (P)rop- is a development of the Hawker Siddeley HS 748.
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