Here's the latest I have on the Gulfstream G500 and the Falcon 7X (8 pax, ISA, NBAA 200 nm Reserves):
Gulfstream G500
Falcon 7x
Normal Cruise: Mach 0.85.....Range 5,100 nm
Normal Cruise: Mach 0.85.....Range 5,100 nm
LRC: Mach 0.80.....Range 5,800 nm
LRC: Mach 0.80.....Range 5,700 nm
Takeoff Dist. MGTOW: 5,150 ft.
Takeoff Dist. MGTOW: 5,200 ft.
Landing Dist. MLW (75,300 lbs): 2,770 ft
Landing Dist. Typical - 37,100 lbs (BOW + 8 pax +2400 lbs fuel): 2,350 ft.
Cabin: 43'11" L x 6'2" H x 7'4" W
Cabin: 39'01" L x 6'2" H x 7'8" W
Cabin Volume: 1,669 sq. ft.
Cabin Volume: 1,500 sq. ft.
MGTOW: 85,100 lbs
MGTOW: 67,300 lbs
Baggage Area: 226 sq. ft.
Baggage Area: 157 sq. ft.
Max Fuel: 35,200 lbs.
Max Fuel: 28,900 lbs.
Max Payload: 6,500 lbs.
Max Payload: 6,000 lbs.
Max Payload Full fuel: 2,300 Lbs.
Max Payload Full Fuel: 1,900 lbs.
Engines: Two Rolls Royce BR710C4-11 rated at 15,385 lbs thrust each
Engines: (3)PWC-PW307A rate at 6,100 lbs thrust each
Thrust to Weight Ratio: 1 to 2.77
Thrust to Weight Ratio: 1 to 3.68
Acquisition Cost: $38 million
Acquisiton Cost: $35.8 million
Direct Operating Cost: $1,886 hr.
Direct Operating Cost: $1,644 hr.
Although not ETOPS certified (ETOPS applies only to aircraft operating under FAA Part 121, FAA Part 129 Foreign Carrier Operations and so forth), the G500/G550 meets double ETOPS 180 requirements.
GV
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