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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.
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.
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
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
A typical light aircraft: the Cessna 172 With a maximum gross takeoff weight of 12,500 lbs, the DHC-6 Twin Otter is an example of the upper limit of the light aircraft category. A Robinson R44 light helicopter. A light aircraft is an aircraft that has a maximum gross takeoff weight of 12,500 lb (5,670 kg) or less. [1]
Air traffic control may assist in navigation by assigning pilots specific headings ("radar vectors"). The majority of IFR navigation is given by ground- and satellite-based systems, while radar vectors are usually reserved by ATC for sequencing aircraft for a busy approach or transitioning aircraft from takeoff to cruise, among other things.
In discussions of the takeoff performance of military aircraft, the term V ref stands for refusal speed. Refusal speed is the maximum speed during takeoff from which the air vehicle can stop within the available remaining runway length for a specified altitude, weight, and configuration. [ 19 ]
The facility includes classroom and briefing spaces; an advanced simulator bay with multiple flight training devices (FTDs); an FAA-certified Level 6 Cessna 172 FTD; and a new maintenance facility. [13] Other ATP schools in the Dallas area can be found at McKinney National Airport (KTKI) and Addison Airport (KADS). [13]