Cessna - Citation Excel
1999
Ceiling
45,000 ft (13,216 m) maximum certified;
28,600 ft (8,717 m) single engine
Maximum Cruise Speed
429 KTAS (795 km/hr), 35,000 ft (10,668m)
Airspeed Limits
Vmo at Sea Level to 28,900 ft (8,809 m)…………
305 KCAS (565 km/hr)
Mmo ……….0.75 (Indicated Mach)
Stall Speed
90 knots CAS (167 km/hr) in landing configu-
ration at 18,700 lbs (8,482 kg)
Pressurization
Nominal pressure differential is 9.3 psi
(61.4 kP)
Rate of Climb
Single Engine 850 fpm (259 mpm)
Two Engine 3,790 fpm (1155 mpm)
Range
2,080 nautical miles (3,852 km) with four
passengers and two crew and 45-minute hold.
Engine
Pratt & Whitney PW545A
Takeoff thrust 3,805 lbs (1,726 kg)
Bypass ratio 4.0
Cabin Dimensions
(with typical interior installed)
Height 5.7 ft (1.74 m)
Width 5.6 ft (1.71 m)
Length (forward pressure bulkhead to aft
pressure bulkhead) 23.0 ft (7.0 m
Outside dimensions
Wingspan 55.7 ft (16.9 m)
Overall height 17.2 ft (5.25 m)
Overall length 51.8 ft (15.79 m)
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