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A pilot of a DC-10 consulting his checklist. In aviation, a preflight checklist is a list of tasks that should be performed by pilots and aircrew prior to takeoff. Its purpose is to improve flight safety by ensuring that no important tasks are forgotten. Failure to correctly conduct a preflight check using a checklist is a major contributing ...
The first production Cessna R172E operating as a T-41B Mescalero with the US Army. In 1964, the US Air Force (USAF) decided to use the commercial off-the-shelf Cessna 172F as a lead-in aircraft for student pilots rather than starting them out in the T-37 jet aircraft. The USAF ordered 237 T-41As from Cessna.
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.
Deicing an Airbus A330 Deicing a Cessna 172, Edmonton, Canada. In aviation, ground deicing of aircraft is the process of removing surface frost, ice or frozen contaminants on aircraft surfaces before an aircraft takes off. This prevents even a small amount of surface frost or ice on aircraft surfaces from severely impacting flight performance.
This list of accidents and incidents involving general aviation is grouped by the years in which the accidents or incidents occurred. "General aviation" here includes private as well as corporate aircraft operating under general aviation rules, i.e. not flights of airliners, commuter or military aircraft.
Steady initial climb speed. The all engines operating take-off climb speed used to the point where acceleration to flap retraction speed is initiated. Should be attained by a gross height of 400 ft (120 m). [10] V A: Design maneuvering speed. This is the speed above which it is unwise to make full application of any single flight control (or ...
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