Cabin
Cockpit
Weight / Powerplant / Dimension
Performance / Specification
 
 
  Beechcraft Bonanza BE-E33C  
     
 

The Beechcraft E33C

    
 
   
   
  Weights / Powerplant / Dimension                
Dimension
Weight
 
 
Gross Weight ...3300 lb
Empty Weight Equipped (w/full oil) ... 2844 lb
Fuel (84 gal) ...504 lb
Passengers and Baggage w/stnd fuel ... lb		        
                 
Powerplant            
           
One Teledyne Continental Motors Corporation engine model IO-520-BA. It is a fuel injected, direct-drive, air-cooled, horizontally-opposed, 6-cylinder, 520-cubic inch-displacement, 285-horsepower rated engine.
        
               
                           
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Performance / Specification            

Bonanza BE-E33C
Performance / Specification  
 
       
  Design Weights
Max. Ramp Weight ......................................................................... 3,312 lbs.
Max. Takeoff Weight....................................................................... 3,300 lbs.
Max. Landing Weight ...................................................................... 3,300 lbs.
Max. Zero Fuel Weight ........................................................ No Sructural Limit
Max. Weight in Baggage Compartment ................................................ 270 lbs.
   
   
Cabin and Entry Dimensions    
Length................................................................................................ 8 ft. 6 in.
Height ............................................................................................... 4 ft. 2 in.
Width ................................................................................................ 3 ft. 6 in.
Cabin Door ................................................................. 37 in. wide by 36 in. high		  
   
Baggage Space and Entry Dimensions
Compartment Volume ......................................................................... 16 cu. ft.
With Utility Shelf ................................................................................. 22 cu. ft.
Door Width (Minimum) ........................................................................ 18.5 in.
Door Height (Minimum)......................................................................... 22.5 in.
   
Specific Loadings (Maximum Take-Off Weight)
Wing Loading at gross weight .............................................................. 16 cu. ft.
Power Loading at gross weight ............................................................. 22 cu. ft.
   
Oil Capacity
Oil Capacity......................................................................................... 12 quarts
 
Oil Pressure
Minimum Pressure (Red Radial) ............................................................ 30 psi
Operating Range (Green Arc) ............................................................... 30 to 60 psi
Maximum RPM (Red Radial) ................................................................. 100 psi		            
       
Maneuver (3300 pounds)      
Chandelle ................................................................................... 132 kts/152 mph
Steep Turn .................................................................................. 132 kt/152 mph
L azy Eight .................................................................................. 132 kts/152 mph
Stall (Except Whip)............................................................... Use slow deceleration
   
Flight Load Factor (3300 pounds)  
Positive maneuvering Load Factors
Flaps Up ................................................................................................. 4.4G
Flaps Down ............................................................................................. 2.0G
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