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