Cessna Citation Mustang C-510

The Mustang is a low-wing cantilever monoplane with a tricycle retractable landing gear and two Pratt & Whitney Canada PW615F turbofan engines, mounted in pods on the rear aft fuselage.

The airframe is constructed primarily of aluminum alloys, with a three spar wing group. One main door is located in the forward left section of the aircraft, with an additional emergency exit on the center right section of the fuselage.

Capacity: 4 to 5 passengers
Length: 40'7" (12.37 m)
Wingspan: 43'2" (13.16 m)
Height: 13'5" (4.09 m)
Empty weight: 6750 lb (3062 kg)
Loaded weight: 8730 lb (3960 kg)
Useful load: 3180 lb (1442 kg)
Max takeoff weight: 8645 lb (3930 kg)

Maximum speed: Mach 0.63
Cruise speed: 340 ktas (630 km/h)
Range: 1167 nmi (at max. takeoff weight) (2161 km)
Service ceiling: 41000 ft (12500 m)
Rate of climb: 3010 fpm (917 mpm)
Thrust/weight: 0.169 (at max. takeoff weight)
Takeoff distance: 3,110 ft (948 m)
Landing distance: 2,380 ft (729 m)

Cessna C-510 - Performance

Single Pilot Certified	Yes
Maximum Cruise Speed	340 ktas (630 km/h)
Certified Ceiling	41,000 ft (12,497 m)
Airport Performance
Takeoff Distance	3,110 ft (948 m)
Landing Distance	2,380 ft (725 m)
Rate of Climb at Sea Level	3,010 fpm (917 mpm)
Range	1,150 nm (2,130 km)

Conditions:Take-off distances are over a 35 foot obstacle and landing distances are over a 50 foot obstacle.
Range Assumption:NBAA IFR Reserves (100 nm), HSC, Max Fuel, Max Takeoff Weight
Airport Performance:at Sea Level, ISA