-Performance-
Maximum Range * (Mach 0.85, 8 passengers, 4 crew and NBAA IFR reserves) 7,000 nm High-Speed Mach 0.90
Long-Range Mach 0.85
MMO (Maximum Operating Mach Number) Mach 0.925
Takeoff Distance (SL, ISA, MTOW) 5,858 ft
Initial Cruise Altitude 41,000 ft
Maximum Cruise Altitude 51,000 ft
* NBAA IFR theoretical range. Actual range will be affected by ATC routing, operating speed, weather, outfitting options and other factors.
-Weights-
Maximum Takeoff 99,600 lb
Maximum Landing 83,500 lb
Maximum Zero Fuel 60,500 lb
Basic Operating (including 4 crew **) 54,000 lb
Maximum Payload ** 6,500 lb
Payload with Maximum Fuel ** 1,800 lb
Maximum Fuel 44,200 lb
** Stated weights are based on theoretical standard outfitting configurations. Actual weights will be affected by outfitting options and other factors.
-External Dimensions-
Length 99 ft 9 in Overall Span 99 ft 7 in Height 25 ft 8 in
-Interior-
Total Interior Length 53 ft 7 in
Cabin Length (excluding baggage) 46 ft 10 in
Cabin Height 6 ft 5 in
Cabin Width 8 ft 6 in
Cabin Volume 2,138 cu ft
Baggage Compartment (usable volume) 195 cu ft
Design Standards
Avionics Gulfstream PlaneView™ II
Engines Two Rolls-Royce BR725 A1-12
Rated Takeoff Thrust (each) 16,900 lb
Passengers (Typical Outfitting)
Charly W. Karl 