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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.
Pages in category "Aircraft with fixed conventional landing gear" The following 200 pages are in this category, out of approximately 1,308 total. This list may not reflect recent changes .
A Boeing 747-400's main landing gear. Note the toes-up bias angle of the bogies on the wing gear, to ensure correct stowage upon retraction: 707, 720, 757, 767, 787: 10 wheels [1x2]+[2x4] A Boeing 757-200 from British Airways: 777: 14 wheels [1x2]+[2x6] A Boeing 777-200 from United Airlines.
Pages in category "Aircraft with skid landing gear" The following 112 pages are in this category, out of 112 total. This list may not reflect recent changes. A.
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.
Aircraft with retractable conventional landing gear (534 P) Pages in category "Aircraft with conventional landing gear" The following 27 pages are in this category, out of 27 total.
An oleo strut is a pneumatic air–oil hydraulic shock absorber used on the landing gear of most large aircraft and many smaller ones. [1] This design cushions the impacts of landing and damps out vertical oscillations.
Pages in category "Aircraft with retractable conventional landing gear" The following 200 pages are in this category, out of approximately 535 total. This list may not reflect recent changes .