Bombardier Challenger 300 vs Bombardier Challenger 3500

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Bombardier Challenger 300
63.8 × 68.7 ft 20.2 ft tall
2× Turbofan Retractable Pressurized
Bombardier Challenger 3500
69.0 × 68.7 ft 20.2 ft tall
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 300Bombardier Challenger 3500
Stall speed
Approach speed
Cruise speed 459 kt459 kt
Range 3100 nm3400 nm
Service ceiling 45000 ft45000 ft
Rate of climb
Fuel burn 295.0 gph297.0 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 300 Jet A
295.0 gph
Baseline
3,100 nm range 1.6 nm/gal 2096 gal usable $1,770 fuel/hr 7h 06m endurance
Bombardier Challenger 300: 295.0 gallons per hour at cruise, 3,100 nautical mile published range, 7 hour 6 minute endurance, 1.6 nautical miles per gallon.
Bombardier Challenger 3500 Jet A
297.0 gph
Baseline
3,400 nm range 1.5 nm/gal 2096 gal usable $1,782 fuel/hr 7h 03m endurance
Bombardier Challenger 3500: 297.0 gallons per hour at cruise, 3,400 nautical mile published range, 7 hour 3 minute endurance, 1.5 nautical miles per gallon.
Jet A range each cell = 1 hr of cruise · width scales with speed

Bars show published still-air range. Endurance is usable fuel divided by the published cruise burn. 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
Density Altitude

Takeoff over 50 ft obstacle

Landing ground roll

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

Scale:
$3,699 /hr
Baseline
Bombardier Challenger 300: $3,699 per flight hour — fuel $1,770, maintenance and reserve $1,929.
$3,731 /hr
Baseline
Bombardier Challenger 3500: $3,731 per flight hour — fuel $1,782, maintenance and reserve $1,949.
$27,009 /yr Baseline
Bombardier Challenger 300: $27,009 per year — insurance withheld, hangar $24,509, annual inspection $2,500.
$28,700 /yr Baseline
Bombardier Challenger 3500: $28,700 per year — insurance withheld, hangar $26,200, annual inspection $2,500.

Estimates only. Costs vary by location, pilot profile, and market conditions. See individual aircraft pages for source notes.

Capability & limits

Each bar stacks your selected occupants against full fuel and the aircraft's useful-load limit (the black line). The open gap between them is spare payload. Add an occupant and the gap closes; once it's gone, fuel has to give.

lb

+ lb / pax

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Bombardier Challenger 300
11 / 11 seats 2,096 / 2,096 gal fuel 1,307 lb wet payload 15,350 lb useful 38,850 lb MTOW
Bombardier Challenger 3500
12 / 12 seats 2,096 / 2,096 gal fuel 1,757 lb wet payload 15,800 lb useful 40,600 lb MTOW

Occupants at 190 + 30 lb each. Fuel at 6.7 lb/gal jet-A, 6.0 lb/gal avgas.

Payload-Range Map

Origin: · two fingers to move map

lb

+ lb / pax

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