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| Major improvements were made to the design with the arrival of the Model S550 Citation S/II. Announced in October 1983, this improved version first flew on February 14 1984. Certification, including an exemption for single pilot operation, was granted that July. Improvements were mainly aerodynamic, including a new wing designed using supercritical technology developed for the Citation III (described separately), plus JT15D4B turbofans. The S/II initially replaced the II in production from 1984, but the II returned to the lineup from late 1985, and both variants remained in production until the introduction of the Bravo. |
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| Seating (normal) |
7 |
Max Takeoff (lbs) |
15,100 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
43,000 |
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| Engines |
2 P&WC JT15D-4B |
To (Sealevel, ISA Temp) (ft) |
3,240 |
| Output lbs ea. Flat Rating |
2,500 |
Landing Distance (ft) |
2,247 |
| Maximum Mach No. |
0.72 |
Max Range (fuel) (nm) |
1,847 |
| High Speed Cruise (Kts) |
402 |
Max Range (payload) (nm) |
1,342 |
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| Flight Time 300nm |
0 + 53 |
Flight Time 1000nm |
2 + 45 |
| Flight Time 600nm |
1 + 39 |
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| External |
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Internal |
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| Length (ft) |
47.20 |
Length (ft) |
16.00 |
| Height (ft) |
15.00 |
Height (ft) |
4.80 |
| Span (ft) |
52.20 |
Width: Max floor (ft) |
4.90 |
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