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Cessna - Citation Bravo
1999
Rate of Climb
Single Engine 1,133 fpm (345 mpm)
Two Engine 3,195 fpm (974 mpm)
Ceiling
45,000 ft (13,216 m) maximum certified;
27,750 ft (8,458 m) single engine
Stall Speed
86 knots CAS (159 km/hr) in landing configu-
ration at 13,500 lbs (6,123 kg)
Airspeed Limits
Vmo at Sea Level 8,000 ft (2,438 m) to
27,900 ft (8,504 m)……….275 KCAS (510 km/hr)
Mmo at 27,900 ft (8,504 m) and above ……….0.70
Mach
Pressurization
Nominal pressure differential is 8.9 psi
(61.4 kP)
Outside dimensions
Wingspan 52'2" (15.90 m)
Overall height 15'0" (4.57 m)
Overall length 47'2" (14.39 m)
Range
1,900 nautical miles (3,519 km) with four
passengers and full fuel, and 45-minute
reserves.
Engine
Pratt & Whitney PW530A Takeoff thrust
2,885 lbs (12.83 kN) Bypass ratio 3.5
Cabin Dimensions
(with typical interior installed)
Height 4'8" (1.43 m)
Width 4'10" (1.48 m)
Length (forward pressure bulkhead to aft
pressure bulkhead) 20'8" (6.31 m)
Maximum Cruise Speed
401 KTAS (743 km/hr), 31,000 ft (9,449 m),
11,850 lbs (5,375 kg) cruise weight
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