Comparison of Bombardier Q100 (Dash 8-100) and Martin 2-0-2 [S]ave
| 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 |
| Travel range (km) | 1,022 | 2,084 |
| Service ceiling (m) | 10,058 | 7,620 |
| Rate of climb (m/sec) | 11.18 | 7.49 |
| 1↑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 |
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