Freestream Aircraft

Archived 27 May 2026

Challenger 605 vs Falcon 2000EX vs G200

Archived side-by-side comparison from the Freestream library

This comparison examines three large-cabin business jets from three distinct manufacturers that occupied the upper tier of the super-midsize and large-cabin segment. The Bombardier Challenger 605 brought North American wide-body comfort, the Dassault Falcon 2000EX delivered European long-range capability with a club-configured interior, and the Gulfstream G200 offered a purpose-built cross-section with a Gulfstream pedigree at lower operating cost.

All three aircraft are out of production and are available on the secondary market. Data is drawn from Conklin & de Decker (JSSI) using standardised assumptions. The Falcon 2000LX variant, which introduced winglets and extended range, is covered in a separate comparison.

0
Platforms
0
Longest Range (Falcon 2000EX)
488 kts
Highest Max Cruise (Challenger 605)
1,146 cu ft
Largest Cabin Volume (Challenger 605)

Bombardier Challenger 605

Twin • Production 2006 – 2016

The Challenger 605 is a large-cabin twin-engine business jet produced by Bombardier from 2006 to 2016, powered by two General Electric CF34-3B engines and equipped with the Rockwell Collins Pro Line 21 avionics suite. With a maximum cruise speed of 488 knots and a seats-full range of 3,756 nautical miles, it provided intercontinental reach within a notably wide cabin measuring 28.4 feet in length and 8.17 feet across. The type succeeded the Challenger 604 with an updated cabin architecture.

Bombardier Challenger 650

Challenger 650 shown; the 605 shares the airframe and is the predecessor variant.

Range
0
nm seats-full
Max Speed
488 kts
maximum cruise
Passengers
Up to 10
wide-body cabin
Ceiling
0
ft maximum certified
Cabin Length
28.4 ft
8.17 ft wide × 6.08 ft tall
Engines
CF34-3B
2× General Electric
Key Specifications
Production2006 – 2016
Long-Range Cruise Speed425 kts
Maximum Cruise Speed488 kts
Range, Seats-Full3,756 nm
Ferry Range4,123 nm
Rate of Climb4,345 ft/min
Engine-Out Ceiling20,000 ft
Balanced Field Length5,950 ft
Cabin Dimensions (L × W × H)28.4 × 8.17 × 6.08 ft
Baggage Volume (Total)115 cu ft (internal)
Max Takeoff Weight48,200 lb
Basic Operating Weight27,150 lb
Usable Fuel19,852 lb
Variable Cost Per Hour$4,808
Annual Fixed Cost$1,278,526

Dassault Falcon 2000EX

Twin • Production 2003 – 2004

The Falcon 2000EX is a twin-engine business jet produced in limited numbers by Dassault from 2003 to 2004, powered by two Pratt & Whitney Canada PW308C engines and equipped with the Rockwell Collins Pro Line 4 avionics suite. It carried up to ten passengers over a seats-full range of 3,878 nautical miles at a maximum cruise speed of 482 knots, with a cabin measuring 31.2 feet in length and 7.7 feet wide. Only 26 aircraft were delivered before production transitioned to the EASy-cockpit successors.

Dassault Falcon 2000

Falcon 2000 family render shown.

Range
0
nm seats-full
Max Speed
482 kts
maximum cruise
Passengers
Up to 10
club-configured cabin
Ceiling
0
ft maximum certified
Cabin Length
31.2 ft
7.7 ft wide × 6.2 ft tall
Engines
PW308C
2× Pratt & Whitney Canada
Key Specifications
Production2003 – 2004
Long-Range Cruise Speed426 kts
Maximum Cruise Speed482 kts
Range, Seats-Full3,878 nm
Ferry Range4,045 nm
Rate of Climb4,375 ft/min
Engine-Out Ceiling26,150 ft
Balanced Field Length5,500 ft
Cabin Dimensions (L × W × H)31.2 × 7.7 × 6.2 ft
Baggage Volume (Total)131 cu ft (internal)
Max Takeoff Weight42,200 lb
Basic Operating Weight23,190 lb
Usable Fuel16,660 lb
Variable Cost Per Hour$4,972
Annual Fixed Cost$1,133,071

Gulfstream G200

Twin • Production 1997 – 2011

The Gulfstream G200, originally certificated as the Galaxy by Israeli Aerospace Industries before Gulfstream's marketing adoption, was produced from 1997 to 2011 with 250 aircraft built. Powered by two Pratt & Whitney Canada PW306A engines and equipped with Rockwell Collins Pro Line 4 avionics, it carried up to eight passengers to 3,130 nautical miles at a maximum cruise speed of 470 knots. Its 7.2-foot cabin width and 6.25-foot height gave it a cross-section competitive with larger aircraft in the class.

Range
0
nm seats-full
Max Speed
470 kts
maximum cruise
Passengers
Up to 8
single-zone cabin
Ceiling
0
ft maximum certified
Cabin Length
24.5 ft
7.2 ft wide × 6.25 ft tall
Engines
PW306A
2× Pratt & Whitney Canada
Key Specifications
Production1997 – 2011
Long-Range Cruise Speed430 kts
Maximum Cruise Speed470 kts
Range, Seats-Full3,130 nm
Ferry Range3,530 nm
Rate of Climb3,700 ft/min
Engine-Out Ceiling23,720 ft
Balanced Field Length6,991 ft
Cabin Dimensions (L × W × H)24.5 × 7.2 × 6.25 ft
Baggage Volume (Total)150 cu ft (25 internal, 125 external)
Max Takeoff Weight35,450 lb
Basic Operating Weight19,950 lb
Usable Fuel15,000 lb
Variable Cost Per Hour$4,776
Annual Fixed Cost$1,091,146

Fleet Comparison at a Glance

Key metrics across all three platforms. Hover a column to highlight; best values in each row are accented. Acquisition cost excluded by design.

Challenger 605 Falcon 2000EX G200
Performance
Range, Seats-Full 3,756 nm 3,878 nm 3,130 nm
Ferry Range 4,123 nm 4,045 nm 3,530 nm
Maximum Cruise Speed 488 kts 482 kts 470 kts
Long-Range Cruise Speed 425 kts 426 kts 430 kts
Maximum Altitude 41,000 ft 47,000 ft 45,000 ft
Rate of Climb 4,345 ft/min 4,375 ft/min 3,700 ft/min
Engine-Out Ceiling 20,000 ft 26,150 ft 23,720 ft
Balanced Field Length 5,950 ft 5,500 ft 6,991 ft
Max Takeoff Weight 48,200 lb 42,200 lb 35,450 lb
Cabin
Cabin Length 28.4 ft 31.2 ft 24.5 ft
Cabin Width 8.17 ft 7.7 ft 7.2 ft
Cabin Height 6.08 ft 6.2 ft 6.25 ft
Passenger Capacity 10 10 8
Baggage Volume (Total) 115 cu ft 131 cu ft 150 cu ft
Operating Economics
Variable Cost / Hour $4,808 $4,972 $4,776
Fuel / Hour $1,645 $1,420 $1,390
Engine Reserves / Hour $938 $1,278 $1,182
Annual Fixed Cost $1,278,526 $1,133,071 $1,091,146

Range Comparison (nm, Seats-Full)

G200
3,130
Challenger 605
3,756
Falcon 2000EX
3,878

Operating Cost Snapshot

Assumes 250 flight hours per year, $5.00 per US gallon Jet A, $105 per hour maintenance labour, 600 nm average trip.

Challenger 605
$4,808
per flight hour
$1,279K
annual fixed
Falcon 2000EX
$4,972
per flight hour
$1,133K
annual fixed
G200
$4,776
per flight hour
$1,091K
annual fixed

Notes

Source

Performance and operating cost data sourced from Conklin & de Decker (JSSI) via Freestream's subscription, pulled 27 May 2026. All figures reflect the standard production variant of each aircraft type unless otherwise stated.

Operating cost assumptions

Hourly variable and annual fixed costs are modelled at 250 flight hours per year, $5.00 per US gallon Jet A, $105 per hour maintenance labour, and a 600 nm average trip. Crew, hangar, insurance, and training are included in the fixed line. Acquisition cost is excluded.


Independent Advice on Large-Cabin Platforms

Freestream Aircraft operates as an independent advisory firm, representing principals in the acquisition, sale, and management of business aircraft worldwide. With active coverage of the large-cabin segment, Freestream provides counsel on platforms including the Challenger 605, Falcon 2000 family, and G200.

Each aircraft in this comparison has distinct operating characteristics that warrant careful evaluation relative to a principal's mission profile. Freestream's team provides independent guidance on condition, market pricing, and transaction execution for buyers and sellers at any stage of the process.

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