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| The Bravo features new P&WC PW530A turbofans, modern Honeywell Primus EFIS avionics suite, a revised interior based on that introduced in the Citation Ultra and other improvements such as trailing link main undercarriage. The Bravo first flew on April 25 1995 and was granted certification in August 1996. First delivery was in February 1997. |
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| Seating (normal) |
7 |
Max Takeoff (lbs) |
14,800 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
45,000 |
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| Engines |
2 P&WC PW530A |
To (Sealevel, ISA Temp) (ft) |
3,600 |
| Output lbs ea. Flat Rating |
2,887/ISA+8 |
Landing Distance (ft) |
2,493 |
| Maximum Mach No. |
0.70 |
Max Range (fuel) (nm) |
1,614 |
| High Speed Cruise (Kts) |
400 |
Max Range (payload) (nm) |
907 |
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| Flight Time 300nm |
0 + 53 |
Flight Time 1000nm |
2 + 49 |
| Flight Time 600nm |
1 + 42 |
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| External |
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Internal |
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| Length (ft) |
47.20 |
Length (ft) |
15.70 |
| Height (ft) |
15.00 |
Height (ft) |
4.70 |
| Span (ft) |
51.70 |
Width: Max floor (ft) |
4.80 |
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