G150 Specifications Sheet G150規(guī)格表
Wide-cabin  high-speed

PERFORMANCE
Maximum Range* 3,000 nm / 5,556 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

55 ft 7 in / 16.94 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   Two Honeywell TFE 731 40AR
Rated Takeoff Thrust (each) 4,420 lb / 19.66 kN
Passengers: Typical Outfitting 6 8
56 ft 9 in / 17.30 m

INTERIOR
Total Interior Length 17 ft 8 in / 5.38 m
Cabin Length (excluding baggage) 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
11 Large Oval Windows