Cirrus Vision SF50 vs Honda HA-420 Elite II

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Cirrus Vision SF50
39 ft × 31 ft ⭥ 11 ft
1× Turbofan Retractable Pressurized
Honda HA-420 Elite II
40 ft × 43 ft ⭥ 15 ft
2× Turbofan 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 Cirrus Vision SF50Honda HA-420 Elite II
Stall speed 86 kt92 kt
Approach speed 85 kt105 kt
Cruise speed 317 kt422 kt
Range 1275 nm1547 nm
Service ceiling 31000 ft43000 ft
Rate of climb 1609 fpm4100 fpm
Fuel burn 70.0 gph120.0 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.

Cirrus Vision SF50 Jet A
70.0 gph
Baseline
1,275 nm range 4.5 nm/gal 296 gal usable $420 fuel/hr 4h 13m endurance
Cirrus Vision SF50: 70.0 gph at cruise, 1,275 nautical mile published range, 4 hour 13 minute endurance, 4.5 nautical miles per gallon.
Honda HA-420 Elite II Jet A
120.0 gph
Baseline
1,547 nm range 3.5 nm/gal 472 gal usable $720 fuel/hr 3h 55m endurance
Honda HA-420 Elite II: 120.0 gph at cruise, 1,547 nautical mile published range, 3 hour 55 minute endurance, 3.5 nautical miles per gallon.
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 over 50 ft obstacle

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:
Cirrus Vision SF50 Jet A
$905 /hr
Baseline
Cirrus Vision SF50: $905 per flight hour — fuel $420, maintenance and reserve $485.
Honda HA-420 Elite II Jet A
$1,528 /hr
Baseline
Honda HA-420 Elite II: $1,528 per flight hour — fuel $720, maintenance and reserve $808.
Cirrus Vision SF50 Turbofan
$46,900 /yr Baseline
Cirrus Vision SF50: $46,900 per year — insurance $15,000, hangar $13,400, annual inspection $18,500.
Honda HA-420 Elite II Turbofan
$13,167 /yr Baseline
Honda HA-420 Elite II: $13,167 per year — insurance withheld, hangar $10,667, 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

+ cargo
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Cirrus Vision SF50 Turbofan
7 / 7 seats cargo 296 gal / 296 gal fuel 417 lbs wet payload 2,400 lbs useful 6,000 lbs MTOW
Honda HA-420 Elite II Turbofan
8 / 8 seats cargo 472 gal / 472 gal fuel 812 lbs wet payload 3,974 lbs useful 11,100 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

+ cargo
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