Performance Database
| |
 |
| |
GLOBAL EXPRESS |
Engines |
| Make |
Rolls Royce |
| Model |
BR710A2-20/BR710-48-C2 |
| HP/Thrust lbs per engine |
14.750 |
Fuselage Dimension |
| Length (ft) |
99.40 |
| Height (ft) |
25.5 |
| Wing Span (ft) |
94.00 |
| Passengers |
15 + 2 Crew |
| Volume Interior (cu.ft) |
1.815 |
| Volume Baggage (cu.ft) |
325 |
| Pressurization (psi) |
9.6 |
Weights (lbs) |
| Max Ramp |
95.250 |
| Max Takeoff |
95.000 |
| Zero Fuel |
56.000 |
| Basic Operating |
50.300 |
| Max Landing |
78.600 |
Fuel Capacity |
| Standard lbs/gal |
43.170 / 6.470 |
Takeoff Performance (BFL) |
| SL ISA BFL (ft) |
5.820 |
| 5000 +20C BFL (ft) |
7.880 |
Landing Performance (ft) |
| FAA Field Length |
2.640 |
Range (NM) |
| Max Range |
6.395 |
Climb (SL ISA MTOW) |
| Normal (fpm) |
1.947 |
| Engine Out (fpm) |
226 |
Speeds (Knots) |
| Vso (Landing) |
129 |
| 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.
This website and all of its contents are owned and copyrighted by aircraftsales.com.
The use of any information without a written permission is strictly prohibited.