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https://en.wikipedia.org/wiki/Cessna_195
The Cessna 190 and 195 Businessliner are a family of light single radial engine powered, conventional landing gear equipped, general aviation aircraft which were manufactured by Cessna between 1947 and 1954. The 195 model was also used by the United States Air Force, United States Army, and Army National Guard as a light transport and utility aircraft under the designations LC-126/U-20. The Cessna 190 and 195 were Cessna's only postwar radial-engined aircraft. The first prototype flew in 1945, after the end of World War II and both the 190 and 195 entered production in 1947. The 195 was the first Cessna airplane to be completely constructed of aluminum and features a cantilever wing, similar to the pre-war Cessna 165 from which it is derived. The wing differs from later Cessna light aircraft in that it has a straight taper from root chord to tip chord and no dihedral. The airfoil employed is a NACA 2412, the same as used on the later Cessna 150, 172 and 182. The 190/195 fuselage is large in comparison to other Cessna models because the 42" diameter radial engine had to be accommodated in the nose. There are two rows of seats: two individual seats in the first row, with a comfortable space between them and up to three passengers can be accommodated on a bench seat in the second row. The 190/195 has flat sprung-steel landing gear legs derived from Cessna's purchase of the rights to Steve Wittman's Big X. Many have been equipped with swiveling crosswind landing gear which allows landing with up to 15 degrees of crab. While the crosswind gear simplifies the actual landing, it makes the aircraft difficult to handle on the ground. The 195 is equipped with a retractable step that extends when the cabin door is opened, although some have been modified to make the step a fixed unit. The aircraft was expensive to purchase and operate for private use and Cessna therefore marketed them as mainly as a business aircraft under the name "Businessliner". The engines fitted to the 190 and 195 became well known for their oil consumption. The aircraft has a 5-US-gallon (19 L) oil tank, with 2 US gallons (7.6 L) the minimum for flight. Typical oil consumption with steel cylinder barrels is 2 US quarts (1.9 L) per hour. A factory-produced floatplane version was equipped with a triple tail for improved yaw stability. The tail resembles that of the Lockheed Constellation. The Cessna 195 produces a cruise true airspeed of 148 knots (274 km/h) (170 MPH) on a fuel consumption of 16 US gallons (61 L) per hour. It can accommodate five people. Including the LC-126s, a total of 1180 190s and 195s were built. Role Light personal and business aircraft National origin United States Manufacturer Cessna Aircraft Company First flight 1945 Introduction 1947 Primary users United States Army United States Air Force Produced 1947-1954 Number built 1,180 Unit cost USD$12,750 (1947) Developed from Cessna 165 The Cessna 190 and 195 are considered "one of the finest classics ever built" by pilots and collectors and are much sought after on the used aircraft market. Brazilian-registered Cessna 195 at Marte airfield, Sao Paulo in 1975 On July 24, 2017 the number of 190s and 195s still registered in the USA we 86 Cessna 190 225 Cessna 195 125 Cessna 195A 126 Cessna 195B In February 2014 there were three Cessna 190s, eleven Cessna 195s, two Cessna 195As and two Cessna 195Bs registered in Canada. Other Cessna 190 and 195 aircraft have been purchased by private pilot owners resident in Brazil and the United Kingdom. Specifications (Cessna 195) General characteristics Crew: one Capacity: four passengers Length: 27 ft 4 in (8.33 m) Wingspan: 36 ft 2 in (11.02 m) Height: 7 ft 2 in (2.18 m) Empty weight: 2,100 lb (953 kg) Gross weight: 3,350 lb (1,520 kg) Fuel capacity: 75 US gallons (280 l; 62 imp gal) Powerplant: 1 × Jacobs R-755 radial engine, 300 hp (220 kW) Propellers: 2-bladed Hamilton Standard constant speed propeller Performance Maximum speed: 178 mph (286 km/h; 155 kn) Cruise speed: 170 mph (274 km/h; 148 kn) at 70% power Stall speed: 62 mph (100 km/h; 54 kn) power off, flaps 45° Never exceed speed: 200 mph (322 km/h; 174 kn) Range: 800 mi (695 nmi; 1,287 km) at 70% power Service ceiling: 18,300 ft (5,600 m) Rate of climb: 1,200 ft/min (6.1 m/s) Wing loading: 15.36 lb/sq ft (75.0 kg/m2) * |
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Miloch wrote in
news ![]() https://en.wikipedia.org/wiki/Cessna_195 The Cessna 190 and 195 Businessliner are a family of light single radial engine powered, conventional landing gear equipped, general aviation aircraft which were manufactured by Cessna between 1947 and 1954. The 195 model was also used by the United States Air Force, United States Army, and Army National Guard as a light transport and utility aircraft under the designations LC-126/U-20. The Cessna 190 and 195 were Cessna's only postwar radial-engined aircraft. The first prototype flew in 1945, after the end of World War II and both the 190 and 195 entered production in 1947. The 195 was the first Cessna airplane to be completely constructed of aluminum and features a cantilever wing, similar to the pre-war Cessna 165 from which it is derived. The wing differs from later Cessna light aircraft in that it has a straight taper from root chord to tip chord and no dihedral. The airfoil employed is a NACA 2412, the same as used on the later Cessna 150, 172 and 182. The 190/195 fuselage is large in comparison to other Cessna models because the 42" diameter radial engine had to be accommodated in the nose. There are two rows of seats: two individual seats in the first row, with a comfortable space between them and up to three passengers can be accommodated on a bench seat in the second row. The 190/195 has flat sprung-steel landing gear legs derived from Cessna's purchase of the rights to Steve Wittman's Big X. Many have been equipped with swiveling crosswind landing gear which allows landing with up to 15 degrees of crab. While the crosswind gear simplifies the actual landing, it makes the aircraft difficult to handle on the ground. The 195 is equipped with a retractable step that extends when the cabin door is opened, although some have been modified to make the step a fixed unit. The aircraft was expensive to purchase and operate for private use and Cessna therefore marketed them as mainly as a business aircraft under the name "Businessliner". The engines fitted to the 190 and 195 became well known for their oil consumption. The aircraft has a 5-US-gallon (19 L) oil tank, with 2 US gallons (7.6 L) the minimum for flight. Typical oil consumption with steel cylinder barrels is 2 US quarts (1.9 L) per hour. A factory-produced floatplane version was equipped with a triple tail for improved yaw stability. The tail resembles that of the Lockheed Constellation. The Cessna 195 produces a cruise true airspeed of 148 knots (274 km/h) (170 MPH) on a fuel consumption of 16 US gallons (61 L) per hour. It can accommodate five people. Including the LC-126s, a total of 1180 190s and 195s were built. Role Light personal and business aircraft National origin United States Manufacturer Cessna Aircraft Company First flight 1945 Introduction 1947 Primary users United States Army United States Air Force Produced 1947-1954 Number built 1,180 Unit cost USD$12,750 (1947) Developed from Cessna 165 The Cessna 190 and 195 are considered "one of the finest classics ever built" by pilots and collectors and are much sought after on the used aircraft market. Brazilian-registered Cessna 195 at Marte airfield, Sao Paulo in 1975 On July 24, 2017 the number of 190s and 195s still registered in the USA we 86 Cessna 190 225 Cessna 195 125 Cessna 195A 126 Cessna 195B In February 2014 there were three Cessna 190s, eleven Cessna 195s, two Cessna 195As and two Cessna 195Bs registered in Canada. Other Cessna 190 and 195 aircraft have been purchased by private pilot owners resident in Brazil and the United Kingdom. Specifications (Cessna 195) General characteristics Crew: one Capacity: four passengers Length: 27 ft 4 in (8.33 m) Wingspan: 36 ft 2 in (11.02 m) Height: 7 ft 2 in (2.18 m) Empty weight: 2,100 lb (953 kg) Gross weight: 3,350 lb (1,520 kg) Fuel capacity: 75 US gallons (280 l; 62 imp gal) Powerplant: 1 × Jacobs R-755 radial engine, 300 hp (220 kW) Propellers: 2-bladed Hamilton Standard constant speed propeller Performance Maximum speed: 178 mph (286 km/h; 155 kn) Cruise speed: 170 mph (274 km/h; 148 kn) at 70% power Stall speed: 62 mph (100 km/h; 54 kn) power off, flaps 45° Never exceed speed: 200 mph (322 km/h; 174 kn) Range: 800 mi (695 nmi; 1,287 km) at 70% power Service ceiling: 18,300 ft (5,600 m) Rate of climb: 1,200 ft/min (6.1 m/s) Wing loading: 15.36 lb/sq ft (75.0 kg/m2) * One of my favoritss, thanks. I have flown Beavers but never the 195, but always wanted to. |
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In article , Mitchell Holman
says... Miloch wrote in news ![]() https://en.wikipedia.org/wiki/Cessna_195 The Cessna 190 and 195 Businessliner are a family of light single radial engine powered, conventional landing gear equipped, general aviation aircraft which were manufactured by Cessna between 1947 and 1954. Maximum speed: 178 mph (286 km/h; 155 kn) Cruise speed: 170 mph (274 km/h; 148 kn) at 70% power Stall speed: 62 mph (100 km/h; 54 kn) power off, flaps 45° Never exceed speed: 200 mph (322 km/h; 174 kn) Range: 800 mi (695 nmi; 1,287 km) at 70% power Service ceiling: 18,300 ft (5,600 m) Rate of climb: 1,200 ft/min (6.1 m/s) Wing loading: 15.36 lb/sq ft (75.0 kg/m2) * One of my favoritss, thanks. I have flown Beavers but never the 195, but always wanted to. In the VNam war, my aviation company had both UH-1s and Beavers. Flew down to Ca Mau (tip of the delta in a U-6 and we left at midnight...as the junior officer (1st lieutenant & only rated for helicopters) the pilot (a captain) had me take the controls and do the flying back to Saigon while he dozed. As there was no electricity in those days in the small villages, it was pitch black with no horizon and the only lights to focus on were the city lights of Saigon...way off in the distance. Flew it on instruments most of the way back. I remember them as no frills-simple and noisy!! * |
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