Lancair LC-40 Columbia 300 vs Lancair LC-41 Columbia 400

Side-by-side specs, range, and operating costs.

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Lancair LC-40 Columbia 300
36 ft × 25 ft ⭥ 9 ft
1× Piston Fixed Unpressurized
Lancair LC-41 Columbia 400
36 ft × 25 ft ⭥ 9 ft
1× Piston Fixed Unpressurized

Flight Profile

Service ceiling, range, and climb rate.

Tap legend to isolate

Arc represents the climb-cruise-descent profile based on published service ceiling and range. Climb rate annotated on ascent. FL180 (18,000 ft) shown for reference.

Mission Performance

Stall, approach, cruise, range, ceiling and climb: best values are at the top.

Mission performance specifications
Specification Lancair LC-40 Columbia 300Lancair LC-41 Columbia 400
Stall speed 71 kt72 kt
Approach speed 78 kt78 kt
Cruise speed 191 kt235 kt
Range 950 nm1107 nm
Service ceiling 18000 ft25000 ft
Rate of climb 1340 fpm1285 fpm
Fuel burn 17.0 gph21.0 gph

Each axis is scaled independently across the compared aircraft and printed in its own units; every vertex sits at the published figure. Higher is better on all axes: Stall, Approach and Fuel Burn are inverted (lower = higher). A missing figure breaks the line at that axis.

Fuel Burn & Range

Range, endurance, and what the fuel costs by the hour.

Lancair LC-40 Columbia 300 Avgas
17.0 gph
Baseline
950 nm range 11.2 nm/gal 98 gal usable $110 fuel/hr 5h 45m endurance
Lancair LC-40 Columbia 300: 17.0 gph at cruise, 950 nautical mile published range, 5 hour 45 minute endurance, 11.2 nautical miles per gallon.
Lancair LC-41 Columbia 400 Avgas
21.0 gph
Baseline
1,107 nm range 11.2 nm/gal 98 gal usable $136 fuel/hr 4h 40m endurance
Lancair LC-41 Columbia 400: 21.0 gph at cruise, 1,107 nautical mile published range, 4 hour 40 minute endurance, 11.2 nautical miles per gallon.
Avgas range each cell = 1 hr of cruise · width scales with speed tank-dry · at this cruise burn

Bars show published still-air range: select a cell to view cruise-hours and fuel usage. Endurance is full tank at the displayed cruise burn rate; the extra is reserve and economy margin. Estimates only. Always verify against the POH.

Runway Performance

Density altitude adjusted estimates

Outside Air Temp
0°F57°F115°F
Field Elevation
SL4,0008,000 ft

Takeoff over 50 ft obstacle

Landing ground roll

Density Altitude

Monte cristo

Base distance DA penalty
Scale: 6,000 ft

FAA 10%/1,000 ft DA rule of thumb (FAA-H-8083-25B). Turboprops and jets are less sensitive in practice. Always verify against the POH.

Estimated Operating Costs

Hourly direct and annual fixed costs

Scale:
Lancair LC-40 Columbia 300 Avgas
$164 /hr
Baseline
Lancair LC-40 Columbia 300: $164 per flight hour — fuel $110, maintenance and reserve $54.
Lancair LC-41 Columbia 400 Avgas
$233 /hr
Baseline
Lancair LC-41 Columbia 400: $233 per flight hour — fuel $136, maintenance and reserve $97.
Lancair LC-40 Columbia 300 Piston
$8,765 /yr Baseline
Lancair LC-40 Columbia 300: $8,765 per year — insurance withheld, hangar $6,265, annual inspection $2,500.
Lancair LC-41 Columbia 400 Piston
$15,115 /yr Baseline
Lancair LC-41 Columbia 400: $15,115 per year — insurance $5,150, hangar $6,265, annual inspection $3,700.

Estimates only. Hourly direct operating cost, based on fuel price and reserves; Annual fixed costs (insurance, hangar, and inspection). Costs vary by location, pilot profile, and market conditions. See individual aircraft pages for source notes.

Capability & limits

Payload vs useful load limit

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Lancair LC-40 Columbia 300 Piston
4 / 4 seats 98 gal / 98 gal fuel 612 lbs wet payload 1,200 lbs useful 3,400 lbs MTOW
Lancair LC-41 Columbia 400 Piston
4 / 4 seats 98 gal / 98 gal fuel 512 lbs wet payload 1,100 lbs useful 3,600 lbs MTOW

Shows selected occupants against full fuel, within the aircraft's useful-load limit. Fuel weight at 6.7 lb/gal jet-A, 6.0 lb/gal avgas; pax and luggage are 190 + 30 . Change payload weights in global settings.

Payload-Range Map

Origin: · two fingers to move map

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