Performance Database
 |
|
CITATION S II |
|
Engines |
|
| Make | Pratt & Whitney |
| Model | JT15D-4B/FJ44-3A |
| HP/Thrust lbs per engine | 2.500 |
| TBO (hours) | 3.500 |
Fuselage Dimension |
|
| Length (ft) | 47.20 |
| Height (ft) | 15.00 |
| Wing Span (ft) | 52.20 |
| Passengers | 8 + 2 Crew |
| Volume Interior (cu.ft) | 263 |
| Volume Baggage (cu.ft) | 76 |
| Pressurization (psi) | 8.7 |
Weights (lbs) |
|
| Max Ramp | 15.300 |
| Max Takeoff | 15.100 |
| Zero Fuel | 11.200 |
| Basic Operating | 8.459 |
| Max Landing | 14.400 |
| Useful Load | 6.300 (SB S550-11-1) |
| Maximum Payload | 2.200 (SB S550-11-1) |
| Payload with full fuel | 697 (SB S550-11-1) |
Fuel Capacity |
|
| Standard lbs/gal | 5.818/ / 862 |
Takeoff Performance (BFL) |
|
| SL ISA BFL (ft) | 3.430 |
| 5000 +20C BFL (ft) | 6.490 |
Landing Performance (ft) |
|
| FAA Field Length | 3.140 |
Range (NM) |
|
| Max Range | 1.970 |
| Full passengers | 1.400 |
| Two passengers (200 lbs each) | 1.800 |
Climb (SL ISA MTOW) |
|
| Normal (fpm) | 3.040 |
| Engine Out (fpm) | 860 |
| Initial Cruise Altitude | 37.000 |
| Time to Cruise Altitude (minutes) | 28 |
Speeds (Knots) |
|
| Vso (Landing) | 82 |
| Normal Cruise TAS | 410 |
| Vmo (Max Operating) IAS | 276 |
Ceiling (ft) |
|
| Certified Ceiling | 43.000 |
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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