Bombardier Challenger 350 vs Embraer Praetor 600

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Bombardier Challenger 350
69 ft × 69 ft ⭥ 20 ft
2× Turbofan Retractable Pressurized
Embraer Praetor 600
70 ft × 67 ft ⭥ 21 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 Bombardier Challenger 350Embraer Praetor 600
Stall speed 95 kt
Approach speed 125 kt107 kt
Cruise speed 459 kt466 kt
Range 3200 nm4018 nm
Service ceiling 45000 ft45000 ft
Rate of climb 4000 fpm
Fuel burn 297.0 gph298.0 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.

Bombardier Challenger 350 Jet A
297.0 gph
Baseline
3,200 nm range 1.5 nm/gal 2,096 gal usable $1,782 fuel/hr 7h 03m endurance
Bombardier Challenger 350: 297.0 gph at cruise, 3,200 nautical mile published range, 7 hour 3 minute endurance, 1.5 nautical miles per gallon.
Embraer Praetor 600 Jet A
298.0 gph
Baseline
4,018 nm range 1.6 nm/gal 2,385 gal usable $1,788 fuel/hr 8h 00m endurance
Embraer Praetor 600: 298.0 gph at cruise, 4,018 nautical mile published range, 8 hour 0 minute endurance, 1.6 nautical miles per gallon.
Jet A 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 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:
$3,731 /hr
Baseline
Bombardier Challenger 350: $3,731 per flight hour — fuel $1,782, maintenance and reserve $1,949.
$3,704 /hr
Baseline
Embraer Praetor 600: $3,704 per flight hour — fuel $1,788, maintenance and reserve $1,916.
$28,700 /yr Baseline
Bombardier Challenger 350: $28,700 per year — insurance withheld, hangar $26,200, annual inspection $2,500.
$28,691 /yr Baseline
Embraer Praetor 600: $28,691 per year — insurance withheld, hangar $26,191, 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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Bombardier Challenger 350 Turbofan
12 / 12 seats cargo 2,096 gal / 2,096 gal fuel 1,757 lbs wet payload 15,800 lbs useful 40,600 lbs MTOW
Embraer Praetor 600 Turbofan
14 / 14 seats cargo 2,385 gal / 2,385 gal fuel 1,968 lbs wet payload 17,948 lbs useful 42,857 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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