Comparison of Bombardier Q100 (Dash 8-100) and Grumman C-1 Trader [S]ave
| Attribute |  Bombardier Q100 (Dash 8-100) × |  Grumman C-1 Trader × |
|---|---|---|
| General | ||
| Manufacturer | Bombardier Aerospace | Grumman |
| Model | Bombardier Q100 (Dash 8-100) | Grumman C-1 Trader |
| Country | Canada | United States |
| Manufactured from (year) | 1983 | 1955 |
| Type | Light Passenger Jets | Military Propellor Planes |
| Icao | Q100 | G96 |
| Performance | ||
| Engine | Pratt & Whitney Canada PW120 | 2x Wright R-1820-82WA Cyclone |
| Power, hp (hp) | 2,000 | 1,525 |
| Avionics | UNS-1Ew FMS, EFI-890R | - |
| Max cruise speed (km/h) | 535 | 444 |
| Approach speed (km/h) | 250 | - |
| Travel range (km) | 2,084 | 1,778 |
| Service ceiling (m) | 7,620 | 7,620 |
| Rate of climb (m/sec) | 7.49 | 9.91 |
| Take off distance (m) | 1,000 | - |
| Landing distance (m) | 780 | - |
| Weights | ||
| Max take off weight (kg) | 15,650 | 13,222 |
| Max payload (kg) | 4,536 | 3,000 |
| Fuel tank capacity (l) | 3,161 | - |
| Baggage volume (m³) | 8.5 | - |
| Dimensions | ||
| Seats | 4 | 3 |
| Cabin height (m) | 1.95 | - |
| Cabin width (m) | 2.5 | - |
| Cabin length (m) | 9.16 | - |
| Exterior length (m) | 22.25 | 12.9 |
| Tail height (m) | 7.5 | 4.9 |
| Fuselage diameter (m) | 2.69 | 1.7 |
| Wing span (m) | 25.9 | 21.2 |
| Wing tips | No Winglets | No Winglets |
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