Read this description of a single engine light plane and answer the questions. the stol ch 701 aircraft is built of semi- monocoque stressed-skin all-metal construction, irframe sections are designed and built so that with internal supports (ribs, bulkheads and just like modern factory-built planes. the the outer surface skin is part of the structure, longerons) to distribute the loads. the parts are fastened together permanently with rivets. sturdy and low-fatigue aluminium alloys make the stol ch 701 airframe very rugged and corrosion resistant. the modern 6061-t6 aluminium alloy used in the construction is durable, corrosion resistant, and very easy to repair and maintain in the field. the owner of a stol ch 701 is assured of a long airframe life, with minimum required maintenance, as, unlike fabric and composites, metal is not adversely affected by ultra-violet (uv) light and temperature changes. the sheet-metal skins, main wing spar, structural ribs, longerons, stiffeners and bulkheads are fastened together with zenith's proven riveting method using textron avex blind rivets, which are as easy to set as pop rivets, requiring only a simple hand rivet puller. the corrosion-resistant avex rivets provide a permanent structural bond and tight low-profile dome finish, formed by the custom riveter head. the ivet stem becomes locked in after being set to provide a water-tight seal. the '/s-inch and 's2-inch vex rivets used are very sturdy and durable fasteners, and may be used over a wide grip area. the sturdy main wing spar is a built up l-beam, with cap extrusions buck-riveted to the spar web. in the kit, the spar comes completely pre-assembled and finished (drilled and riveted, with flanged lightening holes). the rib stations on the spar are even pre-drilled-ready for final wing assembly. the ructural aluminium wing ribs and fuselage bulkheads are supplied ready-to-install (pre-formed and finished at the factory with fanged lightening holes). the semi-monocoque rear fuselage requires the same type of simple assembly as the wings. the square rear fuselage is easily assembled by assembling cach side on a flat workbench and then simply boxing the four sides together. the forward fuselage (cabin) is made up of factory-riveted lower side frames, and a welded 4130 chromium-molybdenum steel top frame. fuselage and cabin parts are supplied ready for assembly as standard components of the complete kit the horizontal stabilizer tail is built up of two spars and internal ribs, covered with the pre-formed aluminium alloy skin. the elevator is fabricated like the ailerons, and attached to the stabiliser with pins at each end. the pre-formed vertical tail skins cover the internal spar and ribs 1 the plane is built in a factory 2 the skin is supported by the frame. 3 the aircraft doesn't need regular maintenance. 4 composites and fabries are affected by temperature change true false ue false false nae false ruc false rue false the rivets can be removed easily. 6 the main wing spar has holes for the lighting c cables 7 wing assembly is the last stage of constructin t true false the cabin frame is strengthened with steel. true false the horizontal stabilizer tail has three parts. 0 the ailerons and elevator are made the same way true false