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| Specification
& Weight
Bravo does everything its forerunners did, and does them better.
More power for less money. Longer endurance and faster speeds.
Short-field performance and high operating altitudes. In a Bravo,
you'll leave the competition far below and farther behind.
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Maximum Cruise Speed (± 3%) |
402 KTAS (745 km/hr), 33,000 ft (10,058 m), 12,500 lbs (5,670 kg)
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Ceiling |
45,000 ft (13,216 m) maximum certified
27,750 ft (8,458 m) single engine
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Airspeed Limits |
Vmo @ 8,000 ft (2,438 m) to 27,900 ft (8,504 m) 275 KIAS (510 km/hr)
Mmo at 27,900 ft (8,504 m) and above 0.70 (Indicated Mach)
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Climb Performance |
Single Engine 1,133 fpm (345 mpm)
Two Engine 3,190 fpm (972 mpm)
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Pressurization |
Nominal pressure differential is 8.9 psi (.61 Bar)
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Range (± 3%) |
1,744 nautical miles (3,232 km) fulle fuel and MTOW NBAA IFR Reserves (100 nm alternate)
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Engine |
Pratt & Whitney PW 530A
Takeoff thrust 2,887 lbs (12.84 kN)
3.4 bypass ratio
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Outside Dimensions |
Overall width 52.2 ft (15.90 m)
Overall height 15.0 ft (4.57 m)
Overall length 47.2 ft (14.39 m)
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Cabin Dimensions (with typical interior installed) |
Height 4.7 ft (1.45 m)
Width 4.8 ft (1.47 m)
Length (forward pressure blockhead to aft pressure blockhead) 20.8 ft (6.31 m)
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Design Weights & Fuel Capacity
| Maximum
ramp weight |
15,000
lbs (6,804 kg) |
| Maximum
takeoff weight |
14,800
lbs (6,713 kg) |
| Maximum
landing weight |
13,500
lbs (6,123 kg) |
| Maximum
zero fuel weight |
11,300
lbs (5,126 kg) |
| Maximum
fuel capacity (usable) |
4,824
lbs (2,188 kg) |
| Typical
empty weight * |
9,040
lbs (4,100 kg) |
| Two
pilots and furnishings |
400
lbs (181 kg) |
| Typical
basic operating weight |
9,440
lbs (4,282 kg) |
| Useful
payload and fuel at ramp weight (over crew) |
5,560
lbs (2,522 kg) |
| Payload
with full fuel |
736
lbs (334 kg) |
| Maximum
payload weight** |
1,860
lbs (843 kg) |
* Includes unusable fuel, oil, and standard equipment as listed in
Citation Bravo Specification and Description.
** Zero fuel weight limited.
Note: Performance conditions are based on the International Standard
Atmosphere. Takeoff and landing field lengths are based on level, hard-surface,
dry runways with no wind.
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