Lancair Evolution Turbine vs Lancair IV-P

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Lancair Evolution Turbine
37 ft × 30 ft ⭥ 10 ft
1× Turboprop Retractable Pressurized
Lancair IV-P
30 ft × 25 ft ⭥ 8 ft
1× Piston Retractable Pressurized

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 Evolution TurbineLancair IV-P
Stall speed 76 kt69 kt
Approach speed 79 kt81 kt
Cruise speed 300 kt278 kt
Range 1027 nm1090 nm
Service ceiling 28000 ft29000 ft
Rate of climb 4000 fpm3000 fpm
Fuel burn 37.0 gph18.0 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 Evolution Turbine Jet A
37.0 gph
Baseline
1,027 nm range 8.1 nm/gal 168 gal usable $222 fuel/hr 4h 32m endurance
Lancair Evolution Turbine: 37.0 gph at cruise, 1,027 nautical mile published range, 4 hour 32 minute endurance, 8.1 nautical miles per gallon.
Lancair IV-P Avgas
18.0 gph
Baseline
1,090 nm range 15.4 nm/gal 90 gal usable $117 fuel/hr 5h 00m endurance
Lancair IV-P: 18.0 gph at cruise, 1,090 nautical mile published range, 5 hour 0 minute endurance, 15.4 nautical miles per gallon.
Avgas range Jet A range each cell = 1 hr of cruise · width scales with speed

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 Evolution Turbine Jet A
$602 /hr
Baseline
Lancair Evolution Turbine: $602 per flight hour — fuel $222, maintenance and reserve $380.
Lancair IV-P Avgas
$211 /hr
Baseline
Lancair IV-P: $211 per flight hour — fuel $117, maintenance and reserve $94.
Lancair Evolution Turbine Turboprop
$9,902 /yr Baseline
Lancair Evolution Turbine: $9,902 per year — insurance withheld, hangar $7,402, annual inspection $2,500.
Lancair IV-P Piston
$7,927 /yr Baseline
Lancair IV-P: $7,927 per year — insurance withheld, hangar $5,427, annual inspection $2,500.

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 Evolution Turbine Turboprop
4 / 4 seats 168 gal / 168 gal fuel 774 lbs wet payload 1,900 lbs useful 4,550 lbs MTOW
Lancair IV-P Piston
4 / 4 seats 90 gal / 90 gal fuel 810 lbs wet payload 1,350 lbs useful 3,550 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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