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Columbia Aircraft Columbia 400

AircraftColumbia AircraftColumbia 400 › Columbia 400

The Columbia 400 is a model in the 400 family. It is described here as a Four-seat composite low-wing piston single.

Columbia Aircraft Columbia 400 specifications

ManufacturerColumbia Aircraft
ModelColumbia 400
Aircraft typeFour-seat composite low-wing piston single
Seats4
Landing gearFixed tricycle
CertificationFAA

Columbia Aircraft Columbia 400 weights and capacities

Maximum takeoff weight3,600 lb
Maximum landing weight3,420 lb
Standard fuel capacity106 gal total / 98 gal usable
Maximum baggage120 lb combined

Columbia Aircraft Columbia 400 engine and configuration

EngineContinental · TSIO-550-C · 310 hp

Columbia Aircraft Columbia 400 history and development

The Columbia 400 is the turbocharged member of the Columbia line. The TSIO-550-C is rated at 310 hp. Published POH/specification data give 3,600 lb MTOW, 3,420 lb MLW, 3,300 lb MZFW and 106 gallons total with approximately 98 gallons usable in the represented configuration. These aircraft later entered the Cessna/Corvalis type-design lineage, so model identity and POH branch are important when comparing specifications.

Columbia Aircraft Columbia 400 fuel capacity

Standard total fuel: 106 U.S. gallons. Standard usable fuel: 98 U.S. gallons. Usable fuel can depend on POH revision and tank calibration; verify aircraft-specific documentation.

Columbia Aircraft Columbia 400 model applicability and configuration

Use the Columbia POH/AFM applicable to the exact model and serial number. Do not substitute 300/350/400 weight or engine data between models.

Columbia Aircraft Columbia 400 weight and balance

Maximum takeoff weight: 3,600 lb. Maximum landing weight: 3,420 lb. Maximum zero fuel weight: 3,300 lb. Maximum combined baggage: 120 lb. The represented maximum takeoff weight is 3,600 lb and usable fuel is approximately 98 U.S. gallons. Operational loading must use the current empty-weight/CG record. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Columbia 400 calculator.

Always verify aircraft applicability. Check the current POH or AFM, equipment list and weight and balance records for the individual aircraft.

Columbia Aircraft Columbia 400 frequently asked questions

What engine does the Columbia 400 use?

The engine listed for this model is Continental TSIO-550-C.

What is the maximum takeoff weight of the Columbia 400?

The represented maximum takeoff weight is 3,600 lb.

How much usable fuel does the Columbia 400 carry?

The represented standard usable fuel capacity is 98 U.S. gallons.

Reference sources

Columbia Aircraft: Applicable Columbia Pilot's Operating Handbook

FAA / type-design records: Lancair Certified / Columbia / Cessna lineage

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