
        
            
            
            CGS 
            Hawk "Plus" Single Seat
        
        The 
        Hawk "Plus" is basically a revised version of the 1983 Two Place Hawk, 
        with two place cargo area combined into a single seat.  While the 
        Classic and Arrow single seat models have a large baggage area behind 
        the seat, it can be difficult to place large bulky items back there.  
        The "Plus" was designed to accommodate the requests of customers needing 
        a larger cargo capacity.  The Hawk "Plus" has larger passenger doors 
        coupled with a two place fuselage.  This combination allows for easy 
        access to the baggage area while keeping the space large enough for a 
        jump seat to be installed.  We have put 4 large filled duffle bags on 
        board and still had room for the small stuff.  Wing tanks are standard 
        on the "Plus" leaving the rear compartment available for optimal use of 
        the space.  It can be used for storage or additional fuel tanks.  With 
        the larger engine options offered, up to 250 lbs. can be carried in the 
        rear baggage area. 
        
        Another 
        feature of the Hawk "Plus" are the wing spars, which are stronger than 
        those found on standard single seat models.  They are 2 1/4" dia. X .083 
        (instead of .049) wall thickness to provide the same load factors as the 
        single place models.  The Hawk "Plus" is based on the Hawk Arrow 
        design.  It has the same forward fuselage pod as the Two Place Arrow, 
        which is 2" wider than the single place models. The Hawk "Plus" also has 
        the semi symmetrical wing, streamline struts, reinforced boom, wing 
        tanks, fibreglass nose cone, folding tail, curved overhead and 
        windshield as standard equipment.
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                ROTAX 447 40 hp 
                x 
                
                x 
                
                x 
                28' 10" 
                135 
                square feet 
                1 
                350 Ibs. 
                x 
                800 lbs 
                
                x 
                
                x | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                x 
                800-1100 
                fpm 
                x 
                
                60-80 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 
                
                35-40 mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
   |