Tu-134 (according to NATO codification: Crusty - "Sharp") - a Soviet passenger aircraft for 76-80 passengers for short and medium-haul airlines, developed in the early 1960s at the OKB im. Tupolev.
The Tu-134 is made according to the scheme of an all-metal cantilever low-wing aircraft with a swept wing (sweep angle - 35 °), placed in the rear fuselage by two D-30 engines of various series. Wing mechanization - double-slotted flaps and spoilers produced only on the ground; slats are absent. The wing area is 127.3 m². The fuselage is "borrowed" from the Tu-124 and lengthened by 7 meters. Plumage - T-shaped. Chassis - retractable, tricycle. The front support retracts into a niche in the fuselage, the main ones - into special gondolas on the wing. The main supports have two axes.
