The GEMINI CH 620 is a light twin-engine 
            kit aircraft. The sleek low-wing design has a wide performance 
            envelope, making it easy to fly (low landing speed), yet it 
            outperforms most other light aircraft in its weight and power class. 
            The aircraft features a simple retractable gear system, available in 
            either standard taildragger or optional tricycle gear configuration.
            Basic features of the GEMINI include a high 
            useful load, large cabin area, and ample baggage space, making the 
            light twin aircraft suitable for extensive cross-country trips, yet 
            simple and sporty for local recreational flights.
            The GEMINI provides comfortable two-place 
            side-by-side seating in a spacious 44-inch wide cabin. Access to the 
            cabin is easy from both sides of the aircraft, facilitated with 
            20-inch wide reinforced wing walkways on either side of the 
            fuselage. The large bubble canopy provides outstanding visibility, 
            including superior forward-downward visibility that only a 
            twin-engine aircraft can offer.
            The large cabin area is equipped with a 
            full-size instrument panel for basic flight and engine instruments. 
            There is plenty of clearance behind the panel to accommodate full 
            custom avionics packages. 
            DUAL CONTROLS: The GEMINI features a 
            centre-mounted 
            control stick accessible from both the left and right hand seats. 
            The unique "Y" control column is a Heintz design feature that pilots 
            fall in love with - it leaves the occupants lap area unencumbered - 
            unlike dual yoke or stick controls - leaving room for charts or 
            other navigation aids on the pilot’s or co-pilot’s lap. The centre 
            stick also does not restrict visibility and access to the instrument 
            panel. 
            The engine controls quadrant is situated on 
            the left hand side of the cabin for easy access to the pilot. The 
            dual rudder pedals also provide steering for the nosewheel (in 
            tricycle gear configuration) or the tailwheel (in conventional 
            configuration). Standard toe-brakes provide differential braking to 
            the hydraulic disk brakes. 
            DESIGNED FOR EASE OF CONSTRUCTION
            The GEMINI CH 620 is designed not only to 
            provide excellent performance and flight characteristics, but 
            importantly, also for quick and easy assembly from Zenith Aircraft’s 
            complete kit. The aircraft uses single-curvature sheet-metal skins 
            fastened over structural members, such as the factory-manufactured 
            spar, wing ribs, longerons, and fuselage bulkheads. Parts are 
            fastened using the proven Avex blind rivets, which are as easy to 
            set as ‘pop’ rivets. The corrosion-resistant Avex rivets provide a 
            permanent structural bond and tight low-profile domed finish formed 
            by the custom riveter head. 
            Blind riveting does not require the special 
            skills or tools that conventional "bucked" riveting calls for, 
            making it well suited for first-time builders. Additionally, as the 
            name implies, riveting is performed only from one side, with access 
            to the ‘blind’ side not required. Because the Avex rivets are so 
            easy to set, construction time is minimized. 
            MODULAR CONSTRUCTION: The GEMINI is 
            assembled one section at a time to minimize space requirements while 
            building. Typically, the wings and tail section are built first. 
            Once assembled, these sections may easily be stored until they’re 
            ready to be joined to the fuselage. Even the fuselage is built in 
            two sections to minimize the space needed to build the GEMINI. The 
            modular building sequence allows the builder to "buy-as-he-builds" 
            rather than buying the complete kit at once. 
            The GEMINI CH 620 wings are made of a 
            carry-through cantilevered main spar. The wing centre-section has a 
            thick 18-percent constant chord airfoil, with tapered outboard wing 
            sections. The outboard wing panels are made for quick and easy 
            removal from the centre section, and are fitted with full-length 
            ailerons at the trailing edge. A sophisticated factory-welded 
            chrome-moly steel device acts as an integrated engine mount and 
            retractable landing gear assembly, attached at each end of the 
            centre wing section. 
            The rear fuselage is made up of a simple 
            rectangular section with a rounded top, formed with single-curvature 
            skins with internal longeron and bulkhead reinforcements. The cabin 
            area is built around the centre wing section, and rounds at the 
            front to join the sleek fibreglass nose cone. 
            The conventional horizontal tail has a 
            fixed stabilizer and large elevator, equipped with a standard 
            electric trim tab. Fiberglas fairings round the ends of the 
            horizontal tail. The full-flying vertical tail (rudder) is all 
            moving to provide maximum cross-wind capability. 
            The rugged retractable landing gear may be 
            configured either as a taildragger (conventional) or tricycle 
            (optional). The main gear is equipped with large 16-inch wheels and 
            the sturdy retractable gear mechanism uses dual ‘bungee’ shock 
            absorbers to provide rough field capability. The main gear is 
            mechanically retracted by a lever located in the cabin. The 
            low-profile tailwheel is fixed (non-retractable), and is linked to 
            the rudder pedals for effective ground handling and steering. 
            
            The all-metal airframe design is based on 
            the ZODIAC CH 601 kit series and other Heintz designs which have 
            proven themselves exhaustively over the past 22 years. 
            
            THE GEMINI CH 620 KIT
            Developed for the novice builder, the 
            GEMINI kit draws on Zenair’s vast aircraft design and manufacturing 
            experience. Over the past twenty two years, Zenair has excelled in 
            the light aircraft industry, successfully bringing to market more 
            than 12 new kit designs and a type-certificated production aircraft. 
            Being the latest Zenair development, the GEMINI CH 620 kit brings 
            forward the ZODIAC CH 601’s tried and proven kit building technology 
            developed for novice builders. 
            The main wing spar is made up of three 
            sections: A fuselage centre section and the outboard wing panels. 
            The three sections are bolted together for easy disassembly. 
            The sturdy wing spar is a built-up C-beam with spar cap angle 
            extrusions buck riveted to the shear web. Spar cap doublers are 
            added at the top and bottom of the web at the wing root. The spar 
            sections are joined by dual splice plates that set the 6½-degree 
            wing dihedral. In the kit, the spar sections are 
            factory-manufactured and jigged together. 
            WING ASSEMBLY: Building the wing 
            sections is easily done on a flat workbench (about 12’ x 4’). The 
            nose and rear wing ribs are positioned to the pre-drilled stations 
            along the spar. The pre-formed wing ribs are supplied 
            ready-to-install (hand finished with flanged lightening holes). A 
            rear spar "Z" angle is attached to the ends of the rear ribs. Once 
            the wing "skeleton" (internal assembly) is put together, top and 
            bottom rear wing skins are fitted to the assembly. The pre-formed 
            leading edge skin is then simply wrapped around the nose ribs and 
            fastened together with the rear skins and spar. 
            Welded aluminum wing tanks are installed 
            behind the main wing spar in the outer wing panels. The ailerons are 
            made up of a single pre-formed sheet-metal skin, with internal 
            reinforcement ribs. The top aileron skin is fastened to the rear 
            wing, providing a unique and simple ‘hingeless’ gap-sealed pivoting 
            system. 
            TAIL SECTIONS: The horizontal 
            stabilizer structure is made up of two spar sections with eight 
            internal ribs. A single pre-formed skin is then wrapped around the 
            assembly for final covering. The elevator uses a single pre-formed 
            skin with several internal rib supports. The elevator is hinged to 
            the stabilizer with a convention piano-hinge. A standard electric 
            trim servo is mounted inside the elevator. 
            The tapered rudder (vertical tail) consists 
            of a main spar that runs the length of the rudder, with nose and 
            rear rib supports. A single rear skin is overlapped by a pre-formed 
            nose skin, riveted together at the spar. 
            FUSELAGE CONSTRUCTION: The fuselage 
            is assembled in two manageable sections: the rear fuselage and the 
            forward fuselage / cabin area. 
            The rear fuselage is built up on a flat 
            workbench, by first attaching longerons, stiffeners, and support 
            brackets to the pre-formed bottom fuselage skin. The flat side walls 
            are also built up from a flat workbench, and then joined to the 
            fuselage bottom. The top rounded bulkheads are then attached to the 
            bottom-half assembly and the top fuselage skins are placed around 
            the bulkheads. 
            The forward fuselage / cabin area is built 
            up around the wing centre section, positioning the cabin side skins, 
            cabin floor, and nose cone bulkhead. The instrument panel and cabin 
            frame are then attached to the section. The two fuselage halves are 
            then fitted and joined together. 
            Once the major airframe sections are 
            assembled, the landing gear is installed: the integrated engine 
            mount and retractable landing gear assembly is bolted to each end of 
            the centre wing section (fuselage), and the wheel assemblies are 
            bolted to the bottom of the landing gear struts. The tailwheel 
            assembly is bolted to the end of the rear fuselage. 
            
            With the fuselage on its gear, the tail 
            sections and the outer wing panels are bolted to the fuselage, and 
            the controls are installed: The factory-welded rudder pedal 
            assemblies are bolted to the cabin floor, and the centre stick is 
            installed. Cable control lines are then run through the fuselage to 
            the tail sections and attached to the elevator and rudder control 
            bellcranks, and aileron control cables are brought to the aileron 
            bellcranks at the ends on the centre wing section. Pushrods connect 
            the bell cranks to the ailerons. 
            The formed Plexiglas bubble canopy and 
            frame is then assembled and fitted to the fuselage. The engines are 
            fastened to the airframe, and powerplant controls and systems are 
            installed. Finally, the fiberglass engine cowls and the nosebowl are 
            fitted to the completed aircraft. 
            The complete kit has been developed to meet 
            the "51% rule," making it eligible for "Experimental - Amateur 
            Built" registration in the United States. Contact the Federal 
            Aviation Administration (FAA) for details on kit aircraft 
            registration and operation. 
            Assembly time for the complete kit is 
            estimated at just 750 hours for the average novice builder. That 
            means that the average builder can expect to fly the completed 
            Gemini within just one year when averaging about two hours of 
            building time per day (or slightly more than three months 
            full-time). 
            WORKSHOP SPACE: A basement workshop 
            or single car garage provides plenty of room for most assemblies. 
            All the sections are built on a flat level workbench (12’ x 4’). No 
            requirement for temperature controlled workshop. 
            TOOLS: Only simple hand tools are 
            needed. This also means that no special building skills or 
            experience is needed, making this a good project for first-time 
            builders. Parts or processes that require special tools, jigs or 
            skills are pre-manufactured at the factory to minimize the 
            construction time. 
            
              
              
- Basic tools required for assembly 
              include: 
 
              
              - 
              
Hand (or pneumatic) blind riveter with 
              custom domed heads; 
 
              - 
              
Cleco temporary fasteners 
              
 
              - 
              
Sheet-metal snips 
 
              - 
              
Hand drill (electric or pneumatic)
              
 
              - 
              
Assorted hand tools such as files, 
              pliers, wrenches, etc. 
 
            
            No costly or specialized tools are 
            required, and importantly, no jigs or fixtures need to be made (that 
            means time is spent building the aircraft, and not making jigs).
            
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                  Jabiru 
                2200
                80 hp 
                
                
                fixed pitch 55-IN dia. ground adjustable 
                
      
                  19 
                ft 
                
                  
                  5 
                ft10 
                ins 
                
      
                  
                  27 
                ft 3 
                ins 
                
      
                  123 
                sq ft 
                2 
                
                  800 
                lbs 
                
                  650 
                lbs 
                
                  1450 
                lbs 
                
                  
                4 US gal 
                
      
                650 
                miles | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                
                450 
                ft 
                
      
                1280 
                fpm 
                
      
                155+ 
                mph 
                
      
                145 
                mph 
                
      
                450 
                ft 
                
      
                12,000+ 
                ft | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                x 
                x 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
   |