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Introduced in November 1955 for the 1956 model year as a development of the Cessna 170B with tricycle landing gear, dubbed "Land-O-Matic" by Cessna. The 172 also featured a redesigned tail similar to the experimental 170C, "Para-Lift" flaps, and a maximum gross weight of 2,200 lb (998 kg) while retaining the 170B's 145 hp (108 kW) Continental O ...
A Cessna 150 converted to taildragger configuration by installation of an aftermarket modification kit. Conventional landing gear, or tailwheel-type landing gear, is an aircraft undercarriage consisting of two main wheels forward of the center of gravity and a small wheel or skid to support the tail. [1] [2] The term taildragger is also used. [2]
A Cessna 150 taildragger. The taildragger configuration has its own advantages, and is arguably more suited to rougher landing strips. The tailwheel makes the plane sit naturally in a nose-up attitude when on the ground, which is useful for operations on unpaved gravel surfaces where debris could damage the propeller.
Landing lights are lights, mounted on aircraft, that illuminate the terrain and runway ahead during takeoff and landing, as well as being used as a collision avoidance measure against other aircraft and bird strikes. Landing lights must be activated when the aircraft is under 10,000 feet in altitude. Landing light on a Cessna 172N
Dramatic video shows the moment the pilot of a small plane made a “textbook” emergency landing on just one wheel. Footage from Tuesday afternoon shows the Cape Air Cessna 402C heading back to ...
Cockpit controls and instrument panel of a Cessna 182D Skylane. Generally, the primary cockpit flight controls are arranged as follows: [2] A control yoke (also known as a control column), centre stick or side-stick (the latter two also colloquially known as a control or joystick), governs the aircraft's roll and pitch by moving the ailerons (or activating wing warping on some very early ...
The landing gear represents 2.5 to 5% of the maximum takeoff weight (MTOW) and 1.5 to 1.75% of the aircraft cost, but 20% of the airframe direct maintenance cost. A suitably-designed wheel can support 30 t (66,000 lb), tolerate a ground speed of 300 km/h and roll a distance of 500,000 km (310,000 mi) ; it has a 20,000 hours time between overhaul and a 60,000 hours or 20 year life time.
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