Lancair LC-40 Columbia 300

Piston • single engine • Low Wing • Fixed gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
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Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
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Mission Profile

Endorsements & ratings:
  • High-Performance
191
KTAS
Cruise Speed
4
Occupants
950
nm
Max Range
612
lbs
Wet Payload

Estimated Ownership Costs

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About the Lancair LC-40 Columbia 300

Overview

The Columbia 300 is a four-seat, fixed-gear, low-wing composite single, the naturally aspirated original of the airframe that later became the turbocharged Columbia 400 and, under Cessna, the TTx. The Lancair Company certified the LC40 Columbia 300 in 1998 and began deliveries in 2000 from Bend, Oregon, on a 310-hp naturally aspirated Continental IO-550-N. It cruises at 190 knots true, fast for a fixed-gear normally aspirated single, and shares the 400’s clean carbon-fiber structure and Utility-category strength.

Production was short. The 300 was superseded around 2003 by the LC42 Columbia 350, and the line later passed to Cessna in 2007. The 300 itself predates the Cessna era and was never rebadged as a Cessna, so a buyer will find it only under the Lancair or Columbia names. The Cessna 350 Corvalis is the later LC42, a separate airframe on the same type certificate.

Against the naturally aspirated Cirrus SR22, the Columbia 300 offers comparable speed with a stiffer, more conventional feel and no airframe parachute. It is the value entry into the Columbia family: the same airframe and cabin as the 400, without the turbo system’s complexity, cost, or altitude reach.

Key Features for GA Buyers

  • Fast for a normally aspirated single. 190 KTAS at 75 percent on 310 hp, competitive with the SR22 and quick for a fixed-gear airframe.
  • Simple naturally aspirated engine. The IO-550-N carries a 2,000-hour TBO, longer than the turbocharged 400’s 1,700, and avoids turbo maintenance and heat-management complexity.
  • Composite Utility-category airframe. The same clean carbon-fiber structure as the 400, certified to plus 4.4 g and corrosion-free.
  • Value entry to the family. Earlier and lower-priced than the 400 or the Cessna TTx, with much of the same airframe character.
  • Long legs. 98 usable gallons gives roughly 950 nm at high cruise, stretching toward 1,300 nm at economy settings.

Trade-offs

  • No turbocharging. The 18,000-foot service ceiling and 190-knot cruise trail the turbocharged 400, and performance falls off at altitude where the 400 holds power.
  • Very short production run. Built only from 2000 to about 2003, so the fleet is small and parts or type-specific expertise can take effort to find.
  • Composite maintenance specialization. Carbon-fiber repair needs shops with composite experience, less common than metal-airframe shops.
  • Thin cost data. No methodology-disclosed operating-cost source exists for the 300, so the figures shown are estimates rather than sourced values.
  • No airframe parachute. Unlike the Cirrus it competes with, the Columbia has no whole-airframe parachute system.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 36.1 ft Height 9.0 ft
Length
25.2 ft
Parking area (ft2)
1392.22 ft2
Max Takeoff Weight
3,400 lbs
Max Landing Weight
3,230 lbs
Useful Load
1,200 lbs
Fuel Capacity
98 gal

Performance

Cruise Speed
191 KTAS
Never-Exceed (Vne)
230 KIAS
Max Structural Cruise (Vno)
180 KIAS
Approach Speed
78 KIAS
Stall, Clean (Vs1)
71 KIAS
Range
950 NM
Service Ceiling
18,000 ft
Rate of Climb
1340 fpm

Engine

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