Performance Database
 |
|
GULFSTREAM G-200 |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | PW306A |
| HP/Thrust lbs per engine | 6,040 |
| TBO (hours) | 6,000 |
Fuselage Dimension |
|
| Length (ft) | 62.3 |
| Height (ft) | 21.5 |
| Wing Span (ft) | 58.1 |
| Passengers | 10 + 2 Crew |
| Volume Interior (cu.ft) | 25 cu ft |
| Volume Baggage (cu.ft) | 150 cu ft |
| Pressurization (psi) | 8.8 |
Weights (lbs) |
|
| Max Ramp | 35,600 |
| Max Takeoff | 35,450 |
| Zero Fuel | 24,000 |
| Basic Operating | 19,950 |
| Max Landing | 30,000 |
| Maximum Payload | 4,050 |
| Payload with full fuel | 650 |
Fuel Capacity |
|
| Standard lbs/gal | 15,000/2,127 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 6,083 |
| 5000 +20C BFL (ft) | 8,804 |
Landing Performance (ft) |
|
| FAA Field Length | 3,280 |
Range (NM) |
|
| Max Range | 3,400 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 1,947 |
| Engine Out (fpm) | 395 |
Speeds (Knots) |
|
| Vmc | 130 |
| Vso (Landing) | 96 |
| Normal Cruise TAS | 459 |
| Vmo (Max Operating) IAS | 360 |
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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