Gulfstream

| Model | Range (NM) | Max Cruise Speed (Kts) | Takeoff Distance (Ft) | Landing Distance (Ft) | Max Takeoff Weight (lbs)|------------|-------------------------|------------------------|------------------------|----------------------------| | Gulfstream G650 | 7,500 | 516 (Mach 0.92) | 6,000 | 3,000 | 99,600 | | Gulfstream G550 | 6,750 | 488 (Mach 0.885) | 5,910 | 2,770 | 91,000 | | Gulfstream G500 | 5,300 | 561 (Mach 0.90) | 5,300 | 3,100 | 79,600 | | Gulfstream G450 | 4,350 | 459 (Mach 0.88) | 5,600 | 2,600 | 74,600 | | Gulfstream G350 | 3,800 | 500 (Mach 0.85) | 5,050 | 3,000 | 70,900 | | Gulfstream G280 | 3,600 | 482 (Mach 0.84) | 4,750 | 2,720 | 39,600 | | Gulfstream G200 | 3,400 | 470 (Mach 0.80) | 6,083 | 2,590 | 35,450 | | Gulfstream G-V | 6,500 | 488 (Mach 0.885) | 5,910 | 2,770 | 90,500 | | Gulfstream G-IVSP | 4,220 | 459 (Mach 0.88) | 5,450 | 3,200 | 74,600 | | Gulfstream G-IV | 4,200 | 459 (Mach 0.88) | 5,450 | 3,200 | 73,200 |

Notes: Data is based on manufacturer specs and industry publications; values can vary slightly depending on configuration and conditions.


Global

Model Range (NM) Max Cruise Speed (Kts) Takeoff Distance (Ft) Landing Distance (Ft) Max Takeoff Weight (lbs)
Global 8000 8,000 516 (Mach 0.94) 5,760 ~2,200* 115,000
Global 7500 7,700 516 (Mach 0.925) 5,800 2,520 114,850
Global 6500 6,600 516 (Mach 0.90) 6,160 2,670 99,500
Global 6000 6,000 513 (Mach 0.89) 6,476 2,670 99,500
Global 5500 5,900 488 (Mach 0.885) 5,490 2,207 92,500
Global 5000 5,200 488 (Mach 0.88) 5,540 2,207 92,500
Global Express XRS 6,305 513 (Mach 0.89) 6,476 2,670 99,500
Global Express 6,000 505 (Mach 0.88) 6,190 2,670 98,000

Notes: *Landing distance for Global 8000 is estimated; exact figures may vary as it’s a new entrant. These figures reflect typical manufacturer-published performance, under standard conditions at max takeoff weight.


Falcon

Model Range (NM) Max Cruise Speed (Kts) Takeoff Distance (Ft) Landing Distance (Ft) Max Takeoff Weight (lbs)
Falcon 10X 7,500 516 (Mach 0.925) 5,905 ~2,500* 115,000
Falcon 8X 6,450 488 (Mach 0.90) 5,910 2,240 73,000
Falcon 7X 5,950 488 (Mach 0.90) 5,710 2,070 70,000
Falcon 6X 5,500 516 (Mach 0.90) 5,480 2,480 77,460
Falcon 900LX 4,750 474 (Mach 0.84) 5,360 2,415 49,000
Falcon 2000LXS 4,000 482 (Mach 0.862) 5,878 2,260 42,800
Falcon 2000S 3,350 482 (Mach 0.862) 5,480 2,315 41,000
Falcon 2000EX EASy 4,000 482 (Mach 0.86) 5,585 2,180 42,800

Notes: *Landing distance for the Falcon 10X is estimated and subject to change upon certification. Dassault aircraft are known for short-field performance and fuel efficiency, often using three engines on long-range models (7X, 8X, 10X).


Challenger

Model Range (NM) Max Cruise Speed (Kts) Takeoff Distance (Ft) Landing Distance (Ft) Max Takeoff Weight (lbs)
Challenger 650 4,000 488 (Mach 0.85) 5,640 2,402 48,200
Challenger 605 4,000 488 (Mach 0.82) 5,840 2,402 48,200
Challenger 604 4,000 470 (Mach 0.82) 5,700 2,364 48,200
Challenger 3500 3,400 470 (Mach 0.83) 4,835 2,364 40,600
Challenger 350 3,200 470 (Mach 0.83) 4,835 2,364 40,600
Challenger 300 3,100 459 (Mach 0.82) 4,810 2,370 38,850

Notes: All ranges are maximum published values based on ideal conditions (NBAA IFR reserves, standard temperatures, and optimal payload). Real-world range can vary with winds, route changes, and weight. Takeoff and Landing Distances also assume ideal conditions and may increase significantly with wet runways, higher elevations, or maximum aircraft weights.