Performance Database
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FALCON 20F |
Engines |
| Make |
General Electric |
| Model |
CF700-2D2/CF-700-2D2-Q |
| HP/Thrust lbs per engine |
4.500 |
| TBO (hours) |
5.000 |
Fuselage Dimension |
| Length (ft) |
56.30 |
| Height (ft) |
17.50 |
| Wing Span (ft) |
53.50 |
| Passengers |
9 + 2 Crew |
| Volume Interior (cu.ft) |
700 |
| Volume Baggage (cu.ft) |
41 |
| Pressurization (psi) |
8.3 |
Weights (lbs) |
| Max Ramp |
28.660 |
| Max Takeoff |
28.660 |
| Zero Fuel |
22.000 |
| Basic Operating |
16.730 |
| Max Landing |
27.320 |
| Useful Load |
10.760 |
| Maximum Payload |
1.700 |
| Payload with full fuel |
1.660 |
Fuel Capacity |
| Standard lbs/gal |
9.119 / 1.361 |
Takeoff Performance (BFL) |
| SL ISA BFL (ft) |
4.950 |
| 5000 +20C BFL (ft) |
9.100 |
Landing Performance (ft) |
| FAA Field Length |
2.450 |
Range (NM) |
| Max Range |
1.610 |
| Full passengers |
1.300 |
| Two passengers (200 lbs each) |
1.400 |
Climb (SL ISA MTOW) |
| Normal (fpm) |
3.330 |
| Engine Out (fpm) |
715 |
| Initial Cruise Altitude |
35.000 |
| Time to Cruise Altitude (minutes) |
26 |
Speeds (Knots) |
| Vso (Landing) |
88 |
| Normal Cruise TAS |
410 |
| Vmo (Max Operating) IAS |
390 |
Ceiling (ft) |
| Certified Ceiling |
42.000 |
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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