Performance Database
 |
|
CITATION 501 |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | JT15D-1A OR-1B |
| HP/Thrust lbs per engine | 2.200 |
| TBO (hours) | 3.500 |
Fuselage Dimension |
|
| Length (ft) | 43.50 |
| Height (ft) | 14.30 |
| Wing Span (ft) | 47.10 |
| Passengers | 6 |
| Pressurization (psi) | 8.5 |
Weights (lbs) |
|
| Max Ramp | 12.000 |
| Max Takeoff | 11.850 |
| Zero Fuel | 8.400 |
| Basic Operating | 6.670 |
| Max Landing | 11.350 |
Fuel Capacity |
|
| Standard lbs/gal | 3.780 / 565 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 2.930 |
| 5000 +20C BFL (ft) | 5.280 |
Landing Performance (ft) |
|
| FAA Field Length | 2.270 |
Range (NM) |
|
| Max Range | 1.325 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 2.680 |
| Engine Out (fpm) | 800 |
Speeds (Knots) |
|
| Vso (Landing) | 82 |
| Normal Cruise TAS | 352 |
| Vmo (Max Operating) IAS | 275 |
Ceiling (ft) |
|
| Certified Ceiling | 41.000 |
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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