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            Hawk Classic Two Place 
      
      
        
      
            
             
      
            
            CGS Hawk Classic Two Seat  
             
            The Hawk Classic Two Seat was designed for those who wanted the 
            excellent flight and handling characteristics of our Hawk Classic 
            Single Seat, but needed to carry a passenger or give flight 
            instruction. The Hawk Classic Two Seat easily fits the requirements 
            of Part 103-7 Waiver for Two Seat Instruction. With an empty weight 
            of 395 lbs. equipped with a Rotax 503 and 440 lbs. equipped with a 
            Rotax 582 (electric start and brakes), we are well under the weight 
            limit of 490 lbs. 
             
            The Hawk Classic Two Seat incorporates tandem seating rather than 
            side by side. This allows a student to feel as if he is flying in a 
            single place during his all important instructional phase because 
            the instructor is out of sight and behind him. When it is time to 
            solo, the student pilot experiences more confidence and less stress 
            with this seating arrangement. He is not suddenly dealing with an 
            empty seat next to him. With tandem seating, turns to the left or 
            right are equally comfortable because you don't have to look across 
            a seat to check behind you. In addition, since most ultralight 
            aircraft are pushers, the tandem configuration allows for better 
            inflow to the propeller, and much less drag. Centre of gravity 
            changes are also much less pronounced when flying solo vs. with a 
            passenger. In a tandem set up, the front pilot balances the engine, 
            and the passenger sits on the centre of gravity, so it makes no 
            difference if you have a passenger or not. The centre of gravity 
            changes very little. In a side by side arrangement, however, when 
            the passenger exits the plane, the centre of gravity makes a drastic 
            shift to the rear, and must be compensated for in some way.  
             
            On the Hawk Classic Two Seat the rear seat is designed to sit 
            slightly higher than the front seat so the field of vision of the 
            passenger or instructor in the rear seat is not obstructed. Other 
            design features of the Hawk Classic Two Seat include: the wing 
            design has a double surface flat bottomed airfoil for stable flight 
            characteristics. The nose is rounded on the bottom and the 
            windshield has a flatter angle than the CGS Hawk Arrow models. Flaps 
            (not flaperons) are standard equipment on all Hawks and are very 
            effective in increasing climb rate and decreasing landing distance. 
            At the heart of the Hawk's unique design is its curved boom tube 
            (which has never been successfully copied by any other ultralight 
            manufacturer). The curved boom allows the horizontal stabilizer to 
            be placed up and above the down wash of the wing, especially when 
            flaps are deployed. Another benefit of the curve is shorter landing 
            gear legs making it easier to get in and out of your plane. The 
            curved boom also is stronger in torsion than a straight boom, and 
            allows the airplane to rotate for take offs and landings in a normal 
            fashion without banging the boom on the ground. It is also 
            aesthetically pleasing to look at. 
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                ROTAX 503 52 hp 
                x 
                
                x 
                
                x 
                34' 
                159 
                square feet 
                2 
                395 Ibs. 
                x 
                950 lbs. 
                
                x 
                
                x | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                600-1100 
                fpm 
                x 
                
                55-75 mph 
                x 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                
                100 mph 
                
                30-35 mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
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