Cessna - Citation VII
1999
Rate of Climb
Single Engine 1,080 fpm (329 mpm)
Two Engine 4,442 fpm (1,354 mpm)
Ceiling
51,000 ft (15,545 m) maximum certified;
23,000 ft (7,010 m) single engine
Maximum Cruise Speed
476 KTAS (882 km/hr), 37,000 ft (10,668m);
18,000 lbs (8,165 kg)
Airspeed Limits
Vmo at Sea Level to 8,000 ft (2,438 m) - 275
KCAS (509 km/hr)
Vmo at 8,000 ft (2,438 m) - 336 KCAS
(640 km/hr)
Vmoat 34,275 ft (10,497m) - 293 KCAS
(542 km/hr)
Mmo- 0.851 (Indicated Mach)
Stall Speed
97 knots CAS (180 km/hr) in landing configu-
ration at 20,000 lbs (9,072 kg)
Pressurization
Nominal pressure differential is 9.3 psi
(61.4 kP), providing an 8,000 foot cabin
altitude at 51,000 feet
Range
2,220 nautical miles (4,113 km) with full
fuel, 22,450 lbs. takeoff weight, 45-minute
holding fuel reserves.
Outside dimensions
Wingspan 53' 6" (16.34 m)
Overall height 16' 9" (5.11 m)
Overall length 55' 6" (16.92 m)
Engine
Garrett AiResearch TFE-731-4R-2S
Takeoff thrust 4,080 lbs (18.15 kN)
Dry weight 822 lbs (373 kg)
Cabin Dimensions
(with typical interior installed)
Height 5'8" (1.74 m)
Width 5'6" (1.67 m)
Length (pressure vessel) 23'8" (7.22 m)
Length (cockpit divider aft) 18'5" (5.62 m)
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