Performance Database
 |
|
FALCON 200 |
|
Engines |
|
| Make | Garrett |
| Model | ATF3-6A-4C |
| HP/Thrust lbs per engine | 5.200 |
Fuselage Dimension |
|
| Length (ft) | 56.30 |
| Height (ft) | 17.50 |
| Wing Span (ft) | 53.50 |
| Passengers | 9 + 2 Crew |
| Pressurization (psi) | 8.5 |
Weights (lbs) |
|
| Max Ramp | 32.000 |
| Max Takeoff | 32.000 |
| Zero Fuel | 22.500 |
| Basic Operating | 19.200 |
| Max Landing | 28.880 |
Fuel Capacity |
|
| Standard lbs/gal | 10.687 / 1.595 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 5.260 |
| 5000 +20C BFL (ft) | 8.750 |
Landing Performance (ft) |
|
| FAA Field Length | 2.860 |
Range (NM) |
|
| Max Range | 2.204 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 3.065 |
| Engine Out (fpm) | 830 |
Speeds (Knots) |
|
| Vso (Landing) | 89 |
| Normal Cruise TAS | 435 |
| Vmo (Max Operating) IAS | 380 |
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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