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Wings of more than 8 or 9 aspect ratio features other devices to complete the cuff effect, [17] for example stall strips (as used on the Cirrus SR22 and Cessna 400), "Rao slots" (as used on the Questair Venture), vortex generators or segmented droop (as used on a NASA modified Cessna 210). In the case of the high aspect ratio Cessna 210 wing ...
This model had a longer wing, giving it a lower landing speed. The name was a play on the name of a popular model of Cessna, the Cessna 172 , the idea being it is one better. Some flying Velocity planes experienced "deep stall" incidents, where the main wing stalled before the canard, causing an unrecoverable stall.
The aircraft experienced a mid-air collision with a Cessna 172, killing both occupants of the Cessna, while there were no injuries aboard the commercial flight and it made a successful landing in spite of loss of its right horizontal stabilizer. January 25, 1990 73 85 85 Avianca Flight 52: Cove Neck: New York: Boeing 707-320B
The Cessna 172 Skyhawk is an American four-seat, single-engine, high wing, fixed-wing aircraft made by the Cessna Aircraft Company. [2] First flown in 1955, [2] more 172s have been built than any other aircraft. [3] It was developed from the 1948 Cessna 170 but with tricycle landing gear rather than conventional landing gear.
Additional speed ranges are specified for other segments of the approach. [1]: Table II-5-1-2 Table II-5-1-2 Approach plates generally include visibility requirements up to category D. [ 1 ] : II-5-1-3 While ICAO specify a top speed of 391 km/h for Category E, there exist no aircraft with an approach speed above this.
Stall speed: 27 kn (31 mph, 50 km/h) out of ground effects, without assistance of engine power, with full flaps; 35 kn (65 km/h) without use of flaps. Never exceed speed : 123 kn (141 mph, 227 km/h) Vne, boundary between yellow and red on the airspeed indicator, achievable in powered flight pitched for dive with 1G wing loading in smooth air.
Data from Jane's All The World's Aircraft 1982-83 General characteristics Crew: 1 Capacity: 3 pax Length: 7.24 m (23 ft 9 in) Wingspan: 9.986 m (32 ft 9 in) Height: 2.77 m (9 ft 1 in) Wing area: 13.4 m 2 (144 sq ft) Aspect ratio: 7.45 Airfoil: NACA 63A515 Empty weight: 600 kg (1,323 lb) Max takeoff weight: 990 kg (2,183 lb) Fuel capacity: 162 L (43 US gal; 36 imp gal) fuel ; 7.5 L (2 US gal; 2 ...
Fuel capacity was increased to 213 US gallons (810 L). Even with the weight increase, single-engine performance improved and the stall speed decreased by a couple of knots. After this change, the plane was named the Cessna 402C. [4] [3] Production stopped after the 1985 model year.