Cirrus Vision SF50 vs Embraer Phenom 300

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
Embraer Phenom 300
52 ft × 51 ft ⭥ 17 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 SF50Embraer Phenom 300
Stall speed 86 kt100 kt
Approach speed 85 kt104 kt
Cruise speed 317 kt464 kt
Range 1275 nm2010 nm
Service ceiling 31000 ft45000 ft
Rate of climb 1609 fpm4050 fpm
Fuel burn 70.0 gph183.0 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.
Embraer Phenom 300 Jet A
183.0 gph
Baseline
2,010 nm range 2.5 nm/gal 799 gal usable $1,098 fuel/hr 4h 21m endurance
Embraer Phenom 300: 183.0 gph at cruise, 2,010 nautical mile published range, 4 hour 21 minute endurance, 2.5 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.
Embraer Phenom 300 Jet A
$2,264 /hr
Baseline
Embraer Phenom 300: $2,264 per flight hour — fuel $1,098, maintenance and reserve $1,166.
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.
Embraer Phenom 300 Turbofan
$18,258 /yr Baseline
Embraer Phenom 300: $18,258 per year — insurance withheld, hangar $15,758, 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
Embraer Phenom 300 Turbofan
11 / 11 seats cargo 799 gal / 799 gal fuel 1,570 lbs wet payload 6,923 lbs useful 18,551 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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