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Data from The Complete Guide to the Single-Engine Cessnas, AOPA Pilot, and Aircraft Specification No. A-768. General characteristics Crew: one Capacity: one passenger Length: 21 ft 6 in (6.55 m) Wingspan: 33 ft 4 in (10.16 m) Height: 6 ft 3 in (1.91 m) Wing area: 159.3 sq ft (14.80 m 2) Empty weight: 890 lb (404 kg) Gross weight: 1,450 lb (658 kg) Fuel capacity: 25 US gallons (95 liters), of ...
The Cessna Citation V (company designation Model 560) is a business jet built by Cessna that was in production from 1989 until 2011. During that time, 774 such craft were made. The first Model 560 prototype, a stretched version of the Citation S/II, flew in August 1987 and was certified on December 9, 1988.
This is the speed at which drag is minimised. For jet aircraft, "long-range cruise" speed (LRC) is defined as the speed which gives 99% of the maximum range, for a given weight. This results in a 3–5% increase in speed. [8] It is also a more stable speed than maximum range speed, so gives less autothrottle movement. [9]
Cessna Model A: 1927 70 Single piston engine monoplane utility airplane Cessna Model BW: 13 Single piston engine monoplane utility airplane Cessna CG-2: Glider Cessna CH-1: 1953 ~50 Single piston engine utility helicopter Cessna CH-4: Single piston engine utility helicopter Cessna CR-1: 1 Single piston engine monoplane racer Cessna CR-2: 1930 1
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 ...
The Cessna Citation Longitude is a business jet produced by Cessna, part of the Cessna Citation family. It remains the largest business jet by Cessna. It remains the largest business jet by Cessna. Announced at the May 2012 EBACE , the Model 700 made its first flight on October 8, 2016, with certification obtained in September 2019.
Data from Jane's All The World's Aircraft 1982–83 General characteristics Crew: 1 or 2 pilots Capacity: 8–10 passengers Length: 39 ft 0 in (11.89 m) Wingspan: 49 ft 4 in (15.04 m) Height: 13 ft 2 in (4.01 m) Wing area: 253.6 sq ft (23.56 m 2) Aspect ratio: 9.6:1 Airfoil: NACA 23018 at root, NACA 23019 at tip Empty weight: 5,682 lb (2,577 kg) Gross weight: 9,850 lb (4,468 kg) Powerplant: 2 ...
Typical missions are 2.0–2.7 hours and with 400 kn (740 km/h) block speeds and most operators can fly 5–6 hours at Mach 0.72–0.76 for a 2,000–2,400 nmi range, with short takeoff requirements and good hot and high performance. A first hour fuel burn of 2,000–2,500 lb (910–1,130 kg) followed by 1,600–1,900 lb (730–860 kg) the ...