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Garmin and Columbia

 
 
 

Familiarize yourself with the world's premiere general aviation avionics suite, the Garmin G1000, on a complete flight in the world's fastest certified piston single, the Columbia 400. The flight provides continuous commentary explaining features of the Columbia 400 and Garmin G1000 during actual flight operations.

The Columbia 400 is an intercooled, twin turbocharged, four-place aircraft certified for flight up to 25,000 feet. This 310 HP all-composite aircraft enjoys cruise speeds of 235 knots and an unrefueled range of 1,300 miles. Aside from exceptional performance, Columbia aircraft are well known for their luxury interiors, stunning ramp appeal, safety and durability.

Garmin's G1000 is an all-glass avionics suite that can present traditional cockpit information in a single highly integrated system. This includes all primary flight, navigation, autopilot, terrain avoidance, communication, engine, and aircraft sensor data, all on dual 10-inch displays.

Join us at the Columbia Aircraft Manufacturing facility in Bend, Oregon where we begin with information about the Columbia 400 aircraft. You are then presented with a briefing on G1000 features, including basic operation of the primary and secondary displays and the data entry module.

The flight takes us from the high desert of Central Oregon over the Cascade Mountain Range to Portland International Airport where we make the approach in weather at near instrument flight minimums.

On the return flight we shoot the complete approach into the Sunriver Resort before completing the last leg back to the factory in Bend . (Filmed in MultiCam HD)

 
 
 
 
 
 
   
   
   

COLUMBIA 400
Specifications

 

Cruise Data
Maximum Cruise Speed (25,000 ft.)
235 KTAS (270 mph)
Power Plant

Engine

Continental:
(TCM) TSIO-550-C, 310 hp @ 2600 RPM

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
Compression Ratio
7.5:1
Weight (Dry)
442 lbs 200 kg
Dimensions and Capacities
Length
25.2 ft.
Height
9 ft.
Wingspan
36 ft.
Wing Area
141.2 sq. ft.
Wing Aspect Ratio
9.2
Wing Loading
24 lbs./sq. ft.
Power Loading
10.97 lbs./hp
Maximum Fuel (US Gallons)
98 Usable
Oil Capacity
8 qts.
Wheel Track
88 in.
Wheel Base
80.2 in.
Performance Data
Takeoff Distance (Sea Level – Standard Temp.)
Ground Run (No wind at 3600 lbs. gw)
750 ft.
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.
Maximum Rate of Climb
1500 fpm
Service Ceiling
25,000 ft. (FL 250)
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)
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
Never Exceed Speed
230 KIAS
Stall Speed in Landing Configuration
69 KIAS
Stall Speed (Takeoff Flaps)
65 KIAS
Stall Speed (No Flaps)
69 KIAS
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
 
 

GARMIN G1000
Features

 
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.

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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