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Flaps 39
- GV/G550 170 KTS/.60M
- G450 180 KTS/.60M
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Turbulence Penetration
- GV/G550 270 KTS/.80M
- G450 270 KTS/.75M
- All Types Below 10,000 FT: 240 KTS
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Ceiling
- GV/G550 51,000 FT
- G450 45,000 FT
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Maximum Fuel Imbalance
- GV/G550 2000 LBS
- G450 2000 LBS @ 55K/400 LBS @ 60.5K
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Maximum Fuel Imbalance Takeoff
- GV/G550 1000 LBS
- G450 See Maximum Fuel Imbalance
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Maximum Demonstrated Crosswind
- GV/G550 28 KTS
- G450 24 KTS
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Speed Brakes
Not approved for extension with flaps at 39 degrees or with landing gear extended in flight.
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Minimum Altitude for Autopilot on Departure
500 FT AGL
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Minimum Altitude for Autopilot on ILS
- GV 50 FT AGL
- G450/550 60 FT AGL
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Minimum Altitude for Autopilot on LNAV/VNAV Approach
- GV 300 FT AGL or 50 FT below MDA, whichever is higher.
- G450/550 50 FT Below MDA
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Minimum Altitude for Autopilot on other than ILS or LNAV/VNAV Approach
50 FT Below MDA
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Coupled Go-Around Single Engine
Not Authorized
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Max Start TGT (Ground)
700 C
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Max Ramp Weight GV
90,900 LBS
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Max Ramp Weight G550
91,400 LBS
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Max Ramp Weight G450
75,000 LBS
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Max Takeoff Weight GV
90,500 LBS
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Max Takeoff Weight G550
91,000 LBS
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Max Takeoff Weight G450
74,600 LBS
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Max Landing Weight GV/G550
75,300 LBS
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Max Landing Weight G450
- 66,000 LBS Cat D
- 58,500 LBS Cat C
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Max Zero Fuel Weight GV/G550
53,500 LBS
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Max Zero Fuel Weight G450
48,000 LBS
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