Performance Database
 |
|
CITATION EXCEL |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | PW545A |
| HP/Thrust lbs per engine | 3,804 |
| TBO (hours) | 5.000 |
Fuselage Dimension |
|
| Length (ft) | 51.80 |
| Height (ft) | 17.20 |
| Wing Span (ft) | 55.70 |
| Passengers | 8 + 2 Crew |
| Pressurization (psi) | 8.9 |
Weights (lbs) |
|
| Max Ramp | 20.200 |
| Max Takeoff | 20.000 |
| Zero Fuel | 15.000 |
| Basic Operating | 12.550 |
| Max Landing | 18.700 |
Fuel Capacity |
|
| Standard lbs/gal | 6.740 / 1.006 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 3.590 |
| 5000 +20C BFL (ft) | 4.730 |
Landing Performance (ft) |
|
| FAA Field Length | 2.327 |
Range (NM) |
|
| Max Range | 1.581 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 3.090 |
| Engine Out (fpm) | 728 |
Speeds (Knots) |
|
| Vso (Landing) | 82 |
| Normal Cruise TAS | 373 |
| Vmo (Max Operating) IAS | 290 |
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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