Scroll down to view the entire Gulfstream Line Performance Data
G 150 PERFORMANCE
* Maximum Range 2,950 nm / 5,467 km (Mach 0.75, 4 passengers, 2 crew and NBAA IFR reserves)
Long-Range Cruise Speed Mach 0.75 / 430 ktas / 796 km/h Normal Cruise Speed Mach 0.80 / 459 ktas / 850 km/h Mmo (Maximum Operating Mach Number) Mach 0.85 Takeoff Distance (SL, ISA, MTOW) 5,000 ft / 1,524 m Landing Distance (SL, ISA, MLW) 2,880 ft / 878 m Initial Cruise Altitude 41,000 ft / 12,497 m Maximum Cruise Altitude 45,000 ft / 13,716 m
WEIGHTS
Maximum Takeoff Weight 26,100 lb / 11,839 kg Maximum Landing Weight 21,700 lb / 9,843 kg Maximum Zero Fuel Weight 17,500 lb / 7,938 kg ** Basic Operating Weight (including 2 crew) 15,100 lb / 6,849 kg ** Maximum Payload 2,400 lb / 1,089 kg ** Payload with Maximum Fuel 850 lb / 386 kg Maximum Fuel Weight 10,300 lb / 4,672 kg
DESIGN STANDARDS
Avionics Rockwell Collins Pro Line 21
Engines (2) Honeywell TFE 731-40AR
Rated Takeoff Thrust (each) 4,420 lb / 19.66 kN Passengers: Typical Outfitting 6-8
INTERIOR
Cabin Length 17 ft 8 in / 5.38 m Cabin Height 5 ft 9 in / 1.75 m Cabin Width 5 ft 9 in / 1.75 m Cabin Volume 465 cu ft / 13.17 cu m
Total Baggage Volume (Internal & External) 80 cu ft / 2.27 cu m
COMFORT
Window 11 Large Oval Windows Galley Forward Galley
Lavatories Aft Lavatory
Cabin Configurations 3 Select Floorplans
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G 200 PERFORMANCE
*Maximum Range 3,400 nm / 6,301 km (Mach 0.75, 4 passengers, 2 crew and NBAA IFR reserves)
Long-Range Cruise Speed Mach 0.75 / 430 ktas / 796 km/h Normal Cruise Speed Mach 0.80 / 459 ktas / 850 km/h Mmo (Maximum Operating Mach Number) Mach 0.85 Takeoff Distance (SL, ISA, MTOW) 6,083 ft / 1,854 m Landing Distance (SL, ISA, MLW) 3,280 ft / 1,000 m Initial Cruise Altitude 39,000 ft / 11,887 m Maximum Cruise Altitude 45,000 ft / 13,716 m
WEIGHTS
Maximum Takeoff Weight 35,450 lb / 16,080 kg Maximum Landing Weight 30,000 lb / 13,608 kg Maximum Zero Fuel Weight 24,000 lb / 10,886 kg **Basic Operating Weight (including 2 crew) 19,950 lb / 9,049 kg **Maximum Payload 4,050 lb / 1,837 kg **Payload with Maximum Fuel 650 lb / 295 kg Maximum Fuel Weight 15,000 lb / 6,804 kg
DESIGN STANDARDS
Avionics Rockwell Collins Pro Line 4
Engines (2) Pratt & Whitney Canada 306A
Rated Takeoff Thrust (each) 6,040 lb / 26.9 kN Passengers: Typical Outfitting 8-10
INTERIOR
Cabin Length 24 ft 5 in / 7.44 m Cabin Height 6 ft 3 in / 1.91 m Cabin Width 7 ft 2 in / 2.18 m Cabin Volume 868 cu ft / 24.6 cu m
Total Baggage Volume (Internal & External) 150 cu ft / 4.2 cu m
COMFORT
Window 15 Large Oval Windows Galley Forward Galley
Lavatories Aft Lavatory
Cabin Configurations 3 Select Floorplans
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G 250 PERFORMANCE
* Maximum Range 3,400 nm / 6,300 km (Mach 0.80, 4 passengers, 2 crew and NBAA IFR reserves)
Long-Range Cruise Speed Mach 0.80 / 459 ktas / 850 km/h High Speed Cruise Mach 0.82 / 470 ktas / 870 km/h Mmo (Maximum Operating Mach Number) Mach 0.85 Takeoff Distance (SL, ISA, MTOW) 4,960 ft / 1,512 m Landing Distance (SL, ISA, MLW) 3,180 ft / 969 m Initial Cruise Altitude 41,000 ft / 12,497 m Maximum Cruise Altitude 45,000 ft / 13,716 m
WEIGHTS
Maximum Takeoff Weight 39,600 lb / 17,962 kg Maximum Landing Weight 32,700 lb / 14,832 kg Maximum Zero Fuel Weight 28,200 lb / 12,791 kg **Basic Operating Weight (including 2 crew) 24,150 lb / 10,954 kg **Maximum Payload 4,050 lb / 1,837 kg ** Payload with Maximum Fuel 1,000 lb / 454 kg Maximum Fuel Weight 14,600 lb / 6,622 kg
DESIGN STANDARDS
Avionics Gulfstream PlaneView250™
Engines (2) Honeywell HTF7250G
Rated Takeoff Thrust (each) 7,445 lb / 33 kN Passengers: Typical Outfitting 8-10
INTERIOR
Cabin Length (excluding baggage) 25 ft 10 in / 7.87 m Cabin Height 6 ft 3 in / 1.91 m Cabin Width 7 ft 2 in / 2.18 m Cabin Volume 935 cu ft / 26.5 cu m
Total Baggage Volume (interior and exterior) 154 cu ft / 4.4 cu m
COMFORT
Cabin Altitude Maximum 7,000 ft at FL450
Windows 19 Large Oval Windows Galley Forward Galley
Lavatories Aft Lavatory
Cabin Configurations 3 Select Floorplans
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G II PERFORMANCE
Cabin Height: 6.1 Ft.
Cabin Width: 7.3 Ft.
Cabin Length: 39.3 Ft.
Total Passenger Cabin Volume : 1269 Cu. Ft.
Baggage Internal: 157 Cu. Ft.
Baggage External: 0 Cu. Ft.
Typical Passenger Seating: 12
Maximum Take-off Weight: 62,000 lb
Maximum Landing Weight: 58,500 lb
Basic Operating Weight Weight: 37,185 lb
Zero Fuel Weight: 42,000 lb
Maximum Payload: 4,815 lb
Payload Full Fuel: 2,190 lb
Usable Fuel: 23,125 lb
Range-Seats Full (NBAA IFR Reserves): 2,625 nm
Normal Cruise Speed (KTAS): 475
Long Range Cruise Speed (KTAS): 450
Service Ceiling: 42,500
One Engine Inoperative Ceiling: 24,500
Rate of Climb: 4,350
Single Engine Rate of Climb: 1,500
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G IISP PERFORMANCE
Cabin Height: 6.1 Ft.
Cabin Width: 7.3 Ft.
Cabin Length: 39.3 Ft.
Total Passenger Cabin Volume : 1269 Cu. Ft.
Baggage Internal: 157 Cu. Ft.
Baggage External: 0 Cu. Ft.
Typical Passenger Seating: 12
Maximum Take-off Weight:
62,000 lb
Maximum Landing Weight: 58,500 lb
Basic Operating Weight Weight: 37,450 lb
Zero Fuel Weight: 42,000 lb
Maximum Payload: 4,550 lb
Payload Full Fuel: 1,925 lb
Usable Fuel: 23,125 lb
Range-Seats Full (NBAA IFR Reserves): 2,790 nm
Normal Cruise Speed (KTAS): 475
Long Range Cruise Speed (KTAS): 430
Service Ceiling: 42,500
One Engine Inoperative Ceiling: 24,500
Rate of Climb: 4,350
Single Engine Rate of Climb: 1,500
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G IIB PERFORMANCE
Cabin Height: 6.1 Ft.
Cabin Width: 7.3 Ft.
Cabin Length: 39.3 Ft.
Total Passenger Cabin Volume : 1270 Cu. Ft.
Baggage Internal: 157 Cu. Ft.
Baggage External: 0 Cu. Ft.
Typical Passenger Seating: 12
Maximum Take-off Weight: 69,700 lb
Maximum Landing Weight: 58,500 lb
Basic Operating Weight Weight: 38,150 lb
Zero Fuel Weight: 44,000 lb
Maximum Payload: 5,850 lb
Payload Full Fuel: 3,964 lb
Usable Fuel: 28,086 lb
Range-Seats Full (NBAA IFR
Reserves): 3,560 nm
Normal Cruise Speed (KTAS): 460
Long Range Cruise Speed (KTAS): 430
Service Ceiling: 43,000
One Engine Inoperative Ceiling: 23,400
Rate of Climb: 4,049
Single Engine Rate of Climb: 1,403
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G III PERFORMANCE
Cabin Height: 6.1 Ft.
Cabin Width: 7.3 Ft.
Cabin Length: 41.3 Ft.
Total Passenger Cabin Volume : 1345 Cu. Ft.
Baggage Internal: 157 Cu. Ft.
Baggage External: 0 Cu. Ft.
Typical Passenger Seating: 12
Maximum Take-off Weight: 69,700 lb
Maximum Landing Weight: 58,500 lb
Basic Operating Weight Weight: 39,500 lb
Zero Fuel Weight: 44,000 lb
Maximum Payload: 4,500 lb
Payload Full Fuel: 2,610 lb
Usable Fuel: 28,090 lb
Aircraft Performance
Range-Seats Full (NBAA IFR Reserves): 3,460 nm
Normal Cruise Speed (KTAS): 478
Long Range Cruise Speed (KTAS): 427
Service Ceiling: 43,000
One Engine Inoperative Ceiling: 27,000
Rate of Climb: 4,210
Single Engine Rate of Climb: 1,470
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G IV PERFORMANCE
Cabin Height: 6.1 Ft.
Cabin Width: 7.3 Ft.
Cabin Length: 45.1 Ft.
Total Passenger Cabin Volume : 1513 Cu. Ft.
Baggage Internal: 169 Cu. Ft.
Baggage External: 0 Cu. Ft.
Typical Passenger Seating: 13
Maximum Take-off Weight: 73,200 lb
Maximum Landing Weight: 58,500 lb
Basic Operating Weight Weight: 43,100 lb
Zero Fuel Weight: 46,500 lb
Maximum Payload: 3,400 lb
Payload Full Fuel: 1,220 lb
Usable Fuel: 29,280 lb
Range-Seats Full (NBAA IFR Reserves): 3,800 nm
Normal Cruise Speed (KTAS): 476
Long Range Cruise Speed (KTAS): 445
Service Ceiling: 41,000
One Engine Inoperative Ceiling: 27,000
Rate of Climb: 4,219
Single Engine Rate of Climb: 1,068
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G 350 PERFORMANCE
*Maximum Range 3,800 nm / 7,038 km (Mach 0.80, 8 passengers, 3 crew and NBAA IFR reserves)
Normal Cruise Mach 0.80 / 459 ktas / 850 km/h High Speed Cruise Mach 0.85 / 488 ktas / 904 km/h Mmo (Maximum Operating Mach Number) Mach 0.88 Takeoff Distance (SL, ISA, MTOW) 5,050 ft / 1,539 m Landing Distance (SL, ISA, MLW) 3,260 ft / 994 m Initial Cruise Altitude 41,000 ft / 12,497 m Maximum Cruise Altitude 45,000 ft / 13,716 m
WEIGHTS
Maximum Takeoff Weight 70,900 lb / 32,160 kg Maximum Landing Weight 66,000 lb / 29,937 kg Maximum Zero Fuel Weight 49,000 lb / 22,226 kg **Basic Operating Weight (including 3 crew) 42,700 lb / 19,369 kg **Maximum Payload 6,300 lb / 2,858 kg **Payload with Maximum Fuel 2,600 lb / 1,179 kg Maximum Fuel Weight 26,000 lb / 11,796 kg
DESIGN STANDARDS
Avionics Gulfstream PlaneView®
Engines (2) Rolls-Royce Tay Mk 611-8C
Rated Takeoff Thrust (each) 13,850 lb / 61.6 kN Passengers: Maximum 19
Typical Outfitting 12-16
INTERIOR
Cabin Length 45 ft 1 in / 13.74 m Cabin Height 6 ft 2 in / 1.88 m Cabin Width 7 ft 4 in / 2.24 m Cabin Volume 1,525 cu ft / 43.2 cu m
Baggage Compartment Volume 169 cu ft / 4.8 cu m
COMFORT
Window 12 Gulfstream Signature Oval Windows Galley Forward or Aft Galley
Lavatories Aft Lavatory and Optional Forward
Cabin Configurations 6 Select Floorplans
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G 450 PERFORMANCE
*Maximum Range 4,350 nm / 8,061 km (Mach 0.80, 8 passengers, 3 crew and NBAA IFR reserves)
Normal Cruise Speed Mach 0.80 / 459 ktas / 850 km/h High Speed Cruise Mach 0.85 / 488 ktas / 904 km/h Mmo (Maximum Operating Mach Number) M ach 0.88 Takeoff Distance (SL, ISA, MTOW) 5,450 ft / 1,661 m Landing Distance (SL, ISA, MLW) 3,260 ft / 994 m Initial Cruise Altitude 41,000 ft / 12,497 m Maximum Cruise Altitude 45,000 ft / 13,716 m
WEIGHTS
Maximum Takeoff Weight 73,900 lb / 33,521 kg Maximum Landing Weight 66,000 lb / 29,937 kg Maximum Zero Fuel Weight 49,000 lb / 22,226 kg **Basic Operating Weight (including 3 crew) 43,000 lb / 19,504 kg **Maximum Payload 6,000 lb / 2,722 kg **Payload with Maximum Fuel 1,800 lb / 816 kg Maximum Fuel Weight 29,500 lb / 13,381 kg
DESIGN STANDARDS
Avionics Gulfstream PlaneView®
Engines (2) Rolls-Royce Tay Mk 611-8C
Rated Takeoff Thrust (each) 13,850 lb / 61.6 kN Passengers: Maximum 19
Typical Outfitting 12-16
INTERIOR
Cabin Length 45 ft 1 in / 13.74 m Cabin Height 6 ft 2 in / 1.88 m Cabin Width 7 ft 4 in / 2.24 m Cabin Volume 1,525 cu ft / 43.2 cu m
Baggage Compartment Volume 169 cu ft / 4.8 cu m
COMFORT
Window 12 Gulfstream Signature Oval Windows Galley Forward or Aft Galley
Lavatories Forward and Aft Lavatory
Cabin Configurations 6 Select Floorplans or Tailored Floorplans
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GV PERFORMANCE
Cabin Height: 6.2 Ft.
Cabin Width: 7.3 Ft.
Cabin Length: 50.1 Ft.
Total Passenger Cabin Volume : 1669 Cu. Ft.
Baggage Internal: 226 Cu. Ft.
Baggage External: 0 Cu. Ft.
Typical Passenger Seating: 13
Aircraft Weights
Maximum Take-off Weight: 90,500 lb
Maximum Landing Weight: 75,300 lb
Basic Operating Weight Weight: 48,400 lb
Zero Fuel Weight: 54,500 lb
Maximum Payload: 6,100 lb
Payload Full Fuel: 1,500 lb
Usable Fuel: 41,000 lb
Range-Seats Full (NBAA IFR Reserves): 6,250 nm
Normal Cruise Speed (KTAS): 488
Long Range Cruise Speed (KTAS): 459
Service Ceiling: 42,400
One Engine Inoperative Ceiling: 29,000
Rate of Climb: 3,610
Single Engine Rate of Climb: 820
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G 550 PERFORMANCE
*Maximum Range 6,750 nm / 12,501km
(Mach 0.80, 8 passengers, 4 crew and NBAA IFR reserves)
Normal Cruise Mach 0.80 / 459 ktas / 850 km/h High Speed Cruise Mach 0.87 / 500 ktas / 926 km/h Mmo (Maximum Operating Mach Number) Mach 0.885 Takeoff Distance (SL, ISA, MTOW) 5,910 ft / 1,801 m Landing Distance (SL, ISA, MLW) 2,770 ft / 844 m Initial Cruise Altitude 41,000 ft / 12,497 m Maximum Cruise Altitude 51,000 ft / 15,545 m
WEIGHTS
Maximum Takeoff Weight 91,000 lb / 41,277 kg Maximum Landing Weight 75,300 lb / 34,156 kg Maximum Zero Fuel Weight 54,500 lb / 24,721 kg **Basic Operating Weight (including 4 crew) 48,300 lb / 21,909 kg **Maximum Payload 6,200 lb / 2,812 kg **Payload with Maximum Fuel 1,800 lb / 816 kg Maximum Fuel Weight 41,300 lb / 18,733 kg
DESIGN STANDARDS
Avionics Gulfstream PlaneView®
Engines (2) Rolls-Royce BR710 C4-11
Rated Takeoff Thrust (each) 15,385 lb / 68.4 kN Passengers: Maximum 19 Typical Outfitting 14 - 18
INTERIOR
Cabin Length 50 ft 1 in / 15.27 m Cabin Height 6 ft 2 in / 1.88 m Cabin Width 7 ft 4 in / 2.24 m Cabin Volume 1,669 cu ft / 47.26 cu m
Baggage Compartment Volume 226 cu ft / 6.40 cu m
COMFORT
Window 14 Gulfstream Signature Oval Windows Galley Forward or Aft Galley
Lavatories Forward and Aft Lavatory Cabin Configurations 12 Select Floorplans or Tailored Floorplans
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G 650 PERFORMANCE
* Maximum Range 7,000 nm / 12,964 km (Mach 0.85, 8 passengers, 4 crew and NBAA IFR reserves)
Long-Range Cruise Speed Mach 0.85 / 488 ktas / 904 km/h Normal Cruise Speed Mach 0.90 / 516 ktas / 956 km/h Mmo (Maximum Operating Mach Number) Mach 0.925 Takeoff Distance (SL, ISA, MTOW) 6,000 ft / 1,829 m Landing Distance (SL, ISA, MLW) 3,000 ft / 914 m Initial Cruise Altitude 41,000 ft / 12,497 m Maximum Cruise Altitude 51,000 ft / 15,545 m
WEIGHTS
Maximum Takeoff Weight 99,600 lb / 45,178 kg Maximum Landing Weight 83,500 lb / 37,875 kg Maximum Zero Fuel Weight 60,500 lb / 27,442 kg ** Basic Operating Weight (including 4 crew) 54,000 lb / 24,494 kg ** Maximum Payload 6,500 lb / 2,948 kg ** Payload with Maximum Fuel 1,800 lb / 816 kg Maximum Fuel Weight 44,200 lb / 20,049 kg
DESIGN STANDARDS
Avionics Gulfstream PlaneView® II
Engines (2) Rolls-Royce BR725 A1-12
Rated Takeoff Thrust (each) 16,100 lb / 71.6 kN Passengers: Typical Outfitting 11-18
INTERIOR
Cabin Length 53 ft 7 in / 16.33 m Cabin Height 6 ft 5 in / 1.95 m Cabin Width 8 ft 6 in / 2.59 m Cabin Volume 2,138 cu ft / 60.54 cu m
Usable Baggage Volume 195 cu ft / 5.52 cu m
COMFORT
Cabin Altitude Maximum 4,850 ft at FL510
Windows 16 Large Gulfstream Panoramic Windows Galley Forward or Aft Galley
Lavatories Forward and Aft Lavatories
Cabin Configurations 12 Select Floorplans or Tailored Floorplans
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