Performance Database
 |
|
GLOBAL 5000 |
|
Engines |
|
| Make | Rolls Royce |
| Model | BR710A2-20 |
| HP/Thrust lbs per engine | 14,750 |
Fuselage Dimension |
|
| Length (ft) | 96.8 |
| Height (ft) | 25.5 |
| Wing Span (ft) | 94 |
| Passengers | 15 + 3 Crew |
| Pressurization (psi) | 10.3 |
Weights (lbs) |
|
| Max Ramp | 87,950 |
| Max Takeoff | 87,700 |
| Zero Fuel | 56,000 |
| Basic Operating | 50,830 |
| Max Landing | 78,600 |
Fuel Capacity |
|
| Standard lbs/gal | 35,733/5,333 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 5,540 |
| 5000 +20C BFL (ft) | 6,650 |
Landing Performance (ft) |
|
| FAA Field Length | 2,670 |
Range (NM) |
|
| Max Range | 5,200 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 2,255 |
| Engine Out (fpm) | 701 |
Speeds (Knots) |
|
| Normal Cruise TAS | 513 |
| Vmo (Max Operating) IAS | 340 |
Ceiling (ft) |
|
| Certified Ceiling | 51,000 |
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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