Lancair Columbia 400 User Manual

Columbia 400 (LC41-550FG)
Information Manual
Revision No. 3 – (November 2004)
THE INFORMATION IN THIS MANUAL WAS TAKEN DIRECTLY
FROM THE FAA APPROVED AIRPLANE FLIGHT MANUAL.
SINCE THE DATA IN THE LANCAIR COLUMBIA 400 (LC41-550FG)
INFORMATION MANUAL MAY NOT BE CURRENT AND CANNOT
BE REVISED, THIS MANUAL CANNOT BE USED FOR FLIGHT
OPERATIONS. IT IS NOT A SUBSTITUTE FOR THE OFFICIAL
FAA APPROVED PILOT’S OPERATING HANDBOOK AND
AIRPLANE FLIGHT MANUAL.
The Lancair Company
22550 Nelson Road Bend Municipal Airport
Bend, Oregon 97701-9710
Phone (541) 318-1144 Fax (541) 318-1177
CustomerService@Lancair.com
http://www.lancair.com/
This document meets GAMA Specification No. 1, Specification for Pilot’s Operating
Handbook, issued February 15, 1975 and revised September 1, 1984.

Lancair Columbia 400 Specifications

General

Manufacturer	Lancair
Model	Columbia 400
Type	Light Aircraft
Category	General Aviation
Seating Capacity	4
Engine	Continental TSIO-550-C
Service Ceiling	25, 000 ft (7, 620 m)
Maximum Takeoff Weight	3, 600 lb (1, 633 kg)
Horsepower	310 hp
Max Speed	235 knots (435 km/h, 270 mph)
Wingspan	36 ft (11 m)
Height	9 ft (2.7 m)
Fuel Capacity	98 US gallons (371 L)
Range	1, 200 nautical miles (1, 380 mi, 2, 220 km)