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COLUMBIA 400
Specifications
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Cruise Data |
Maximum Cruise Speed (25,000 ft.) |
235 KTAS (270 mph) |
Power Plant |
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Continental:
(TCM) TSIO-550-C, 310 hp @ 2600 RPM
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Propeller |
Hartzell 3 Blade,
Constant Speed, 77 in. dia. |
Time Between Overhauls |
(TBO) 2000 hrs. or 12 years |
Displacement |
550 cu. in. 9.0 L |
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Compression Ratio |
7.5:1 |
Weight (Dry) |
442 lbs 200 kg |
Dimensions and Capacities |
Length |
25.2 ft. |
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Height |
9 ft. |
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Wingspan |
36 ft. |
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Wing Area |
141.2 sq. ft. |
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Wing Aspect Ratio |
9.2 |
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Wing Loading |
24 lbs./sq. ft. |
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Power Loading |
10.97 lbs./hp |
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Maximum Fuel (US Gallons) |
98 Usable |
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Oil Capacity |
8 qts. |
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Wheel Track |
88 in. |
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Wheel Base |
80.2 in. |
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Performance Data |
| Takeoff Distance (Sea Level – Standard Temp.) |
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Ground Run (No wind at 3600 lbs. gw) |
750 ft. |
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Over 50 ft. Obstacle (No wind at 3600 lbs. gw) |
1900 ft. (Total Distance) |
| Landing Distance (Sea Level – Standard Temp.) |
Over 50 ft. Obstacle (No wind at 3400 lbs. gw) |
2600 ft. (Total Distance) |
Ground Run (No wind at 3400 lbs. gw) |
1550 ft. |
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Maximum Rate of Climb |
1500 fpm |
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Service Ceiling |
25,000 ft. (FL 250) |
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Weight Data |
Takeoff Weight |
3600 lbs. |
(Maximum) |
Ramp Weight |
3612 lbs. |
(Maximum) |
Empty Weight |
2500 lbs. |
(Approximate) |
Useful Load |
1100 lbs. |
(Approximate) |
Landing Weight |
3420 lbs. |
(Maximum) |
Baggage Weight |
120 lbs. |
(Maximum) |
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Speed Data |
Maximum Operating Maneuvering Speed |
158 KIAS |
(3600 lbs. gw) |
Maximum Flap Extended Speed |
117 KIAS |
(Full Flaps) |
Maximum Takeoff Flap Extended Speed |
126 KIAS |
(Takeoff Flaps) |
Maximum Structural Cruising Speed |
181 KIAS |
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Never Exceed Speed |
230 KIAS |
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Stall Speed in Landing Configuration |
69 KIAS |
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Stall Speed (Takeoff Flaps) |
65 KIAS |
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Stall Speed (No Flaps) |
69 KIAS |
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General Information |
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 |
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GARMIN G1000
Features |
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| Dual 10.4-inch diagonal measure color flat-panel displays. |
Solid state Attitude and Heading Reference System (AHRS). |
| Dual integrated avionics systems with dual nav/com radios, dual VOR/LOC/ILS receivers, and dual GPS receivers. |
Integrated digital air-data computer.
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Garmin GFC 700
Autopilot. |
Integrated radio modules that provide WAAS-upgradeable IFR oceanic-approved GPS. |
| Integrated engine-monitoring display with full screen engine graphics. |
| In-flight reversionary capabilities that allow flight critical information to transfer to a single display. |
| XM Satellite Radio integrated weather data link. |
| Mode S Transponder with Traffic Alert System (TAS). |
| Integrated Terrain Awareness and Warning System (TAWS) with worldwide terrain and obstacle database. |
| Garmin GCU 476 full alpha-numeric keypad (READY pad ®). |
| Digital audio panel/intercom with ATC playback recording. |
| XM Satellite Radio entertainment system. |
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