| 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 |