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      Rearwin Junior Aircraft history performance and specifications 
      
      
          
        
        
       
          
      With the market for everything starting to disappear during The Great 
      Depression, Rearwin, along with other airplane manufacturers, decided to 
      build a "flying flivver." The Junior was an attempt to fill that niche.
       
       
      Powered by a 3 cyl. 45 HP Szekely engine, the Junior enjoyed some market 
      success. The 3000, and the later 4000 version (with an Aeromarine AR-3 
      engine) sold nearly 30 copies.  
       
      The Szekely engine w as 
      notorious for spitting out its cylinders. So much so that the heads were 
      attached to one-another by a cable!
        
      
      
      
       
        | 
        Rearwin Junior | 
        
       
        | 
        Specifications | 
        
         
         3000 
         | 
        
          | 
        
         
         3100 
         | 
        
         
        
        4000   | 
        
       
        | 
         
         Aircraft Type Certificate  
  
         | 
        
         
         #434 
         (07-09-31) 
         
         | 
          | 
        
         
         #481 
         (05-06-32) 
         | 
        
         
         #469 
         (03-25-32) 
         
         | 
        
       
        | 
         
         Length  
         | 
        
         
         21 ft 11 in 
         | 
        
          | 
        
         
           
         | 
        
         
         22 ft 3 in 
         
         | 
        
          
           | 
            
            Height  
            | 
           
            
            7 ft 6 in 
            | 
           
             | 
           
            
              
            | 
           
            
             7 ft 6 in 
            
            | 
        
        
       
        | 
         
         Wing Span  
         | 
        
         
         36 ft 
         | 
        
          | 
        
         
           
         | 
        
         
          36 ft 
         
         | 
        
        
       
        | 
         
         Wing Area  
         | 
        
         
         179.5 sq ft 
         | 
        
          | 
        
         
           
         | 
        
         
          179.5 sq ft 
         
         | 
        
        
       
        | 
        Construction  | 
        
       
        | The fuselage 
        framework was built of welded chrome-moly and 1025 steel tubing, lightly 
        faired to shape and fabric covered. One elongated cockpit seated two in 
        tandem; there was a large windshield in front and a smaller windshield 
        for the rear seat. A detachable full enclosure was optional. A large 
        rectangular door offered easy entry into either seat. The wing framework 
        in two halves was built up of laminated spruce spar beams with spruce 
        and birch plywood truss-type wing ribs. The leading edges were covered 
        with plywood sheet and the completed framework was covered in fabric. 
        The centre section was mounted high above the cockpit on steel tube 
        struts and the wings were braced to the lower fuselage by streamlined 
        steel tube struts. The split-axle landing gear of 72 inch tread used a 
        spool of rubber shock-cord or Rusco rubber compression rings to absorb 
        the shock. 16x7-4 Goodyear airwheels w/o brakes were standard equipment. 
        Tail skid was of steel spring-leaf type. The fabric-covered tail group 
        was built up of welded steel tubing and channel sections. Horizontal 
        stabilizer was adjustable in flight. A wooden Aeromarine propeller, dual 
        joystick controls were standard equipment. A 12 lb. or 28 lb detachable 
        winter enclosure was optional. | 
        
       
        |   | 
        
       
        | Power 
        Plant | 
        
       
        | 
         
         Engine MFG  
  
         | 
        
         
         Szekely 
         | 
        
         
         Poyer 
         | 
        
         
         Szekely 
         
         | 
        
         
         Aeromarine 
         | 
        
       
        | 
         
         Model  
         | 
        
         
         SR-3-0 
         | 
        
         
  
         | 
        
         
         SR-3-55 
         | 
        
         
         AR-3 
         | 
        
       
        | 
         
         H.P.  
         | 
        
         
         45 
         | 
        
         
         40 
         | 
        
         
         50 
         | 
        
         
         40-50 
         | 
        
       
        | Fuel 
        Data | 
        
       
        | 
         
         Gasoline capacity (upper 
         wing)  
  
         | 
        
         
           
         | 
        
         
           
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         | 
        
         
         12 gal 
         | 
        
       
        | 
         
         Gasoline capacity (fuselage)  
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         - 
         | 
        
       
        | 
         
         Oil capacity  
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         6 qts 
         | 
        
       
        | 
        Equipment | 
        
       
        |   | 
        
       
        | Load | 
        
       
        | 
         
         Weight empty  
  
         | 
        
        569 lbs | 
        
         
           
         | 
        
         
           
         | 
        
         
          
         506 lbs /617 lbs* 
         | 
        
        
       
        | 
         
         Useful load   
         | 
        
         
         430 lbs 
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         433 lbs/423 lbs*  
         | 
        
       
        | 
         
         Payload  
         | 
        
         
         177 lbs 
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         180 lbs/170 lbs* 
         | 
        
       
        | 
         
         Gross weight loaded  
         | 
        
         
         999 lbs 
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         1038 lbs / 1040 lbs*  
         | 
        
       
        | 
        Performance | 
        
       
        | 
         
         High speed (full load)  
  
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         91 mph  
         
         | 
        
       
        | 
         
         High speed (pilot 
         alone)  
         
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
          - 
         | 
        
       
        | 
         
         Cruising speed (full load)  
         
         | 
        
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         76 mph 
         | 
        
       
        | 
         
         Landing speed (full 
         load)  
         
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
          30 mph 
         | 
        
       
        | 
         
         Cruising range (full 
         load)  
         
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         240 miles  
         | 
        
       
        | 
         
         Climb at sea level 
         (full load)  
         
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
          700 ft 
         | 
        
       
        | 
         
         Climb to 10,000 feet 
         (full load)  
         
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         - 
         | 
        
       
        | 
         
         Take off time (pilot 
         alone)  
         
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         - 
         | 
        
       
        | 
         
         Take off time (full 
         load)  
         
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         - 
         | 
        
       
        | 
         
         Absolute ceiling (full load)  
         | 
        
         
           
         | 
        
         
           
         | 
        
         
           
         | 
        
         
         16,000 ft  
         | 
        
       
        | 
        
        Cost | 
        
       
        | 
         
         Retail price from factory  
         | 
        
         
         $1,800 
         | 
        
         
  
         | 
        
         
  
         | 
        
         
         $1,880 
         | 
        
       
        | Comments | 
        
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          | 
          | 
          | 
        * 
        specifications shown with/without the removable cockpit enclosure | 
        
       
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