Performance Database
 |
|
GULFSTREAM G-II |
|
Engines |
|
| Make | Rolls Royce |
| Model | SPEY MK 511-8 |
| HP/Thrust lbs per engine | 11.400 |
| TBO (hours) | 8.000 |
Fuselage Dimension |
|
| Length (ft) | 79.90 |
| Height (ft) | 24.60 |
| Wing Span (ft) | 68.90 |
| Passengers | 11 + 2 Crew |
| Volume Interior (cu.ft) | 1.270 |
| Volume Baggage (cu.ft) | 157 |
| Pressurization (psi) | 9.5 |
Weights (lbs) |
|
| Max Ramp | 65.300 |
| Max Takeoff | 64.800 |
| Zero Fuel | 42.000 |
| Basic Operating | 36,944 |
| Max Landing | 58.500 |
| Useful Load | 25.950 |
| Maximum Payload | 5.450 |
| Payload with full fuel | 2.830 |
Fuel Capacity |
|
| Standard lbs/gal | 23.300 / 3.478 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 26,250 |
Landing Performance (ft) |
|
| FAA Field Length | 3.200 |
Range (NM) |
|
| Max Range | 2,592 |
| Full passengers | 2.600 (add 210 w.Winglets) |
| Two passengers (200 lbs each) | 2.700 (add 210 w.Winglets) |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 4.345 |
| Engine Out (fpm) | 1.520 |
| Initial Cruise Altitude | 39.000 |
| Time to Cruise Altitude (minutes) | 18 |
Speeds (Knots) |
|
| Vmc | 102 |
| Vso (Landing) | 108 |
| Normal Cruise TAS | 459 |
| Vmo (Max Operating) IAS | 367 |
Ceiling (ft) |
|
| Certified Ceiling | 45.000 |
Specifications are provided as introductory information only and
are subject to verification by the buyer during a prepurchase inspection
of the aircraft. The aircraft is offered subject to prior sale,
price changes and/or removal from the market without notice.
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