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The companies named the design the Cirrus Airframe Parachute System (CAPS), and, as of April 2023, made it standard equipment on all 9,000+ Cirrus SR aircraft. In 2002, BRS received a supplemental type certificate to install their parachute system in the Cessna 172, followed by the Cessna 182 in 2004 and the Symphony SA-160 in 2006. [1]
Developed as a collaboration between Cirrus and Ballistic Recovery Systems (BRS), [3] it was adapted from the GARD (General Aviation Recovery Device) initially released for the Cessna 150. [4] As in other BRS systems, a small solid-fuel rocket housed in the aft fuselage is used to pull the parachute out from its housing and deploy the canopy ...
This technique is widely used in the kit-plane industry and in construction of larger aircraft, but would be Cessna's first use in its single-engine line. On 9 October 2007 Cessna announced that a Ballistic Recovery Systems airframe ballistic parachute system would be a factory-installed option on the Cessna 162. [35] [36]
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 ...
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.
The following other wikis use this file: Usage on ba.wikibooks.org Балалар өсөн буяу китабы; Балалар өсөн буяу китабы/Plane
Cessna never offered a civil model directly analogous to these aircraft, but Cessna licensee Reims Aviation in France sold similar IO-360-powered models as the R172 Rocket and Hawk XP. [10] T-41A United States Air Force version of the Cessna 172F, 172G, and 172H for undergraduate pilot training, powered by 145 hp Continental O-300.
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