Attribute | ![]() Bombardier Q400 × | ![]() Antonov An-32 × |
---|---|---|
General | ||
Manufacturer | Bombardier Aerospace | Antonov |
Model | Bombardier Q400 | Antonov An-32 |
Country | Canada | Ukraine |
Manufactured from (year) | 1983 | 1982 |
Type | Passenger Turbo Props | Military Propellor Planes |
Icao | - | AN32 |
Performance | ||
Engine | 2 X Pratt and Whitney PW150A - | 2x 2 × ZMKB AI-20DM turboprop |
Power, hp (hp) | 5,071 | 5,112 |
Avionics | Rockwell Collins Pro Line Fusion | - |
Max cruise speed (km/h) | 667 | 463 |
Travel range (km) | 2,522 | 2,408 |
Fuel economy (km/l) | 0.391 | 0.954 |
Service ceiling (m) | 7,620 | 9,510 |
Rate of climb (m/sec) | 0.06 | 6.4 |
Take off distance (m) | 1,402 | 1,240 |
Landing distance (m) | 1,287 | 1,700 |
Weights | ||
Max take off weight (kg) | 142,196 | 59,525 |
Max payload (kg) | 8,669 | 6,700 |
Fuel tank capacity (l) | 6,424 | 2,998 |
Baggage volume (m³) | 14.2 | 30 |
Dimensions | ||
Seats | 78 | 5 |
Seats - business class | 68 | 42 |
Seats - first class | - | 24 |
Cabin height (m) | 1.95 | - |
Cabin width (m) | 2.51 | - |
Cabin length (m) | 18.8 | - |
Exterior length (m) | 32.84 | 23.78 |
Tail height (m) | - | 8.75 |
Fuselage diameter (m) | 2.69 | - |
Wing span (m) | 28.42 | 29.2 |
Wing tips | No Winglets | No Winglets |