Attribute | ![]() Bombardier Q100 (Dash 8-100) × | ![]() Martin 2-0-2 × |
---|---|---|
General | ||
Manufacturer | Bombardier Aerospace | Glenn L. Martin Company |
Model | Bombardier Q100 (Dash 8-100) | Martin 2-0-2 |
Country | Canada | United States |
Manufactured from (year) | 1983 | 1946 |
Manufactured to (year) | - | 1948 |
Type | Light Passenger Jets | Passenger Turbo Props |
Icao | Q100 | - |
Performance | ||
Engine | Pratt & Whitney Canada PW120 | 2x Pratt & Whitney R-2800 CA-18 Double Wasp |
Power, hp (hp) | 2,000 | 2,400 |
Avionics | UNS-1Ew FMS, EFI-890R | - |
Max cruise speed (km/h) | 535 | 500 |
Approach speed (km/h) | 250 | 122 |
Travel range (km) | 2,084 | 1,022 |
Service ceiling (m) | 7,620 | 10,058 |
Rate of climb (m/sec) | 7.49 | 11.18 |
Take off distance (m) | 1,000 | 477 |
Landing distance (m) | 780 | 520 |
Weights | ||
Max take off weight (kg) | 15,650 | 18,098 |
Max payload (kg) | 4,536 | 4,200 |
Fuel tank capacity (l) | 3,161 | 6,587 |
Baggage volume (m³) | 8.5 | - |
Dimensions | ||
Seats | 4 | 4 |
Cabin height (m) | 1.95 | - |
Cabin width (m) | 2.5 | - |
Cabin length (m) | 9.16 | - |
Exterior length (m) | 22.25 | 21.74 |
Tail height (m) | 7.5 | 8.66 |
Fuselage diameter (m) | 2.69 | 2.8 |
Wing span (m) | 25.9 | 28.42 |
Wing tips | No Winglets | No Winglets |