Gulfstream G150

Jet • twin engine • Low Wing • Retractable gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

Endorsements & ratings:
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument
459
KTAS
Cruise Speed
8
Occupants
3000
nm
Max Range
752
lbs
Wet Payload

Estimated Ownership Costs

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About the Gulfstream G150

The Gulfstream G150 was produced by Gulfstream Aerospace (manufactured by Israel Aerospace Industries). It is a wide-cabin evolution of the G100/Astra SPX, noted for its speed (Mach 0.85 max) and ability to fly coast-to-coast in the US. The G150 features a wider fuselage than its predecessor, offering improved passenger comfort. It is powered by two Honeywell TFE731-40AR engines and uses Rockwell Collins Pro Line 21 avionics. Production ran from 2005 to 2017.

Key Features for GA Buyers

  • Performance Leader: The G150 was marketed as the fastest mid-size business jet, capable of reaching Mach 0.85 and cruising comfortably at Mach 0.80.
  • Transcontinental Range: With a range of nearly 3,000 nm, it can easily fly coast-to-coast in the US (e.g., New York to Los Angeles) or connect London to Moscow non-stop.
  • Cabin Comfort: It features a wider, oval-shaped fuselage compared to its predecessor (the G100), offering significantly more seated headroom and shoulder room (seating 6-8 passengers comfortably).
  • Avionics: Equipped with the Rockwell Collins Pro Line 21 avionics suite, which is highly regarded for its reliability and situational awareness features.

Trade-offs

  • Out of Production: Production ended in 2017 (superseded by the G280), which may factor into long-term depreciation and support considerations compared to current production models.
  • Runway Requirements: While decent for its class, its takeoff distance (5,000 ft at MTOW) requires longer runways than some lighter jet competitors, limiting access to smaller general aviation airfields.
  • Cabin Height: While wider than the G100, the cabin height (5 ft 9 in) is not fully “stand-up” for taller passengers compared to super-midsize jets.

Technical Specifications

Dimensions

Wingspan
55.6 ft
Length
56.75 ft
Height
19.1 ft
Parking area (ft2)
4050.8 ft2

Weights

Max Takeoff Weight
26,100 lbs
Max Landing Weight
21,700 lbs
Useful Load
11,050 lbs
Fuel Capacity
1537 gal

Performance

Cruise Speed
459 KTAS
Never-Exceed (Vne)
330 KIAS
Max Structural Cruise (Vno)
470 KIAS
Approach Speed
115 KIAS
Stall, Clean (Vs1)
89 KIAS
Range
3000 NM
Service Ceiling
45,000 ft
Rate of Climb
3340 fpm
Takeoff over 50 ft obstacle
5,000 ft
Landing ground roll
2,880 ft

Engines

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