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The CJ series are powered by two Williams FJ44 engines; the design uses the Citation II's forward fuselage with a new carry-through section wing and a T-tail. The original CitationJet model has been updated into the CJ1/CJ1+/M2 variants; additionally, the CJ1 was stretched into the CJ2/CJ2+ which was built between 2000 and 2016.
[2] [3] [6] To further reduce drag, the fuselage and engine nacelle pylons were redesigned, and nacelle fairings were added. [ 2 ] [ 6 ] Fuel capacity was increased by 120 US gal (450 L). The result of the improvements was a cruise speed of 403 kn (746 km/h)—exceeding 400 kn, felt to be an important marketing benchmark by Cessna—and a range ...
Data from Jane's All The World's Aircraft 1969–70 General characteristics Crew: 1 Capacity: 5 passengers Length: 29 ft 9 in (9.07 m) Wingspan: 38 ft 09 in (11.81 m) Height: 9 ft 4 in (2.84 m) Wing area: 201 sq ft (18.7 m 2) Aspect ratio: 7.18:1 Airfoil: NACA 2412 at root, NACA 2409 at tip Empty weight: 2,655 lb (1,204 kg) Max takeoff weight: 4,400 lb (1,996 kg) Fuel capacity: 92 US gal (77 ...
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X-Plane is a flight simulation software initially launched by Laminar Research in 1995. Commercial desktop versions are sold for macOS , Windows , and Linux . In addition, Laminar Research also distributes FAA -certified versions for professional use.
Cessna Citation Mustang instrument panel A Mustang PW615F engine uncowled. Data from Cessna Aircraft Company [14] General characteristics. Crew: one or two pilots; Capacity: 4 to 5 passengers and 3130 lb (1420 kg) useful load; Length: 40 ft 7 in (12.37 m) Wingspan: 43 ft 2 in (13.16 m) Height: 13 ft 5 in (4.09 m) Empty weight: 5,600 lb (2,540 kg)
Data from Jane's all the world's aircraft 1976–77. General characteristics Crew: Two Capacity: four passengers Length: 36 ft 9.75 in (11.22 m) Wingspan: 49 ft 0.5 in (14.95 m) Height: 14 ft 6 in (4.42 m) Wing area: 255 sq ft (23.69 m 2) Aspect ratio: 9.45:1 Airfoil: NACA 23012 modified Empty weight: 4,635 lb (2,102 kg) Max takeoff weight: 6,750 lb (3,062 kg) Powerplant: 2 × Lycoming IO-540 ...
The L550E is an air-cooled horizontally-opposed 550cc four-cylinder two-stroke petrol engine developing 37 kW (50 hp) at 7500 rpm which can drive a propeller either directly or geared. It employs a single magneto ignition, four carburettors , and is lubricated by oil mixture lubrication with a fuel to oil ratio of 25:1 for mineral oil or 50:1 ...