Columbia 400 Specifications
Weight Data |
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| Takeoff Weight | 3600 lbs. | (Maximum) | ||||||||||||
| Ramp Weight | 3612 lbs. | (Maximum) | ||||||||||||
| Empty Weight | 2568 lbs. | (Approximate) | ||||||||||||
| Useful Load | 1032 lbs. | (Approximate) | ||||||||||||
| Landing Weight | 3420 lbs. | (Maximum) | ||||||||||||
| Baggage Weight | 120 lbs. | (Maximum) | ||||||||||||
Speed Data |
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| Maximum Operating Maneuvering Speed | 158 KIAS | (3600 lbs. gw) | ||||||||||||
| Maximum Flap Extended Speed | 117 KIAS | (Full Flaps) | ||||||||||||
| Maximum Takeoff Flap Extended Speed | 127 KIAS | (Takeoff Flaps) | ||||||||||||
| Maximum Structural Cruising Speed | 181 KIAS | |||||||||||||
| Never Exceed Speed | 230 KIAS | |||||||||||||
| Stall Speed in Landing Configuration | 59 KIAS | |||||||||||||
| Stall Speed (Takeoff Flaps) | 65 KIAS | |||||||||||||
| Stall Speed (No Flaps) | 69 KIAS | |||||||||||||
General Information* |
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| The All-Electric Columbia 400 comes standard with Dual Independent Electrical Systems** | Cross-Tie ability during alternator failure | Dual Batteries | ||||||||||||
| Dual Alternators and Regulators | Starting Ability with Either Battery or Both Batteries During Cold Weather | Essential Bus Automatically Fed from Either System | ||||||||||||
| Avionics Bus Automatically Fed from Either System | Dual Pointer Ammeter Displaying Either Both Batteries or Alternator Conditions | *Specifications provided represent base aircraft. 400i, SL/SLX may vary. **Components are subject to change without notice. Columbia Aircraft has the right to substitute other equipment that it believes has comparable features. |
** Options are subject to certification and availability at time of delivery. Contact your Columbia Aircraft Salesperson for latest information. | |||||||||||
