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The service ceiling is the maximum altitude of an aircraft during normal operations. Specifically, it is the density altitude at which flying in a clean configuration , at the best rate of climb airspeed for that altitude and with all engines operating and producing maximum continuous power, will produce a given rate of climb.
V x increases with altitude and V Y decreases with altitude until they converge at the airplane's absolute ceiling, the altitude above which the airplane cannot climb in steady flight. The Cessna 172 is a four-seat aircraft. At maximum weight it has a V Y of 75 kn (139 km/h) indicated airspeed [4] providing a rate of climb of 721 ft/min (3.66 m/s).
Service ceiling: 5,500 m (18,000 ft) (absolute ceiling) Rate of climb: 6.32 m/s (1,245 ft/min) Take-off run to 15 m (50 ft): 436 m (1,430 ft)
In service Produced ... costs of the project is 568 million crowns, ... Absolute ceiling: 8,230 m (27,000 ft) Rate of climb: 8.5 m/s ...
Data from Cirrus SR20 Specifications Webpage General characteristics Crew: 1 Capacity: 3 Length: 26 ft 0 in (7.92 m) Wingspan: 38 ft 4 in (11.68 m) Height: 8 ft 11 in (2.72 m) Empty weight: 2,126 lb (964 kg) Gross weight: 3,050 lb (1,383 kg) Powerplant: 1 × Continental IO-360-ES six cylinder, horizontally-opposed piston aircraft engine, 200 hp (150 kW) Propellers: 3-bladed Performance Cruise ...
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