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      Messerschmitt-Blohm - 209 Monsun performance and specifications 
                        
            
                                        
                                         
            
                                        
                                        History and 
                                        Notes
                                        
                                        
                                        In 1965 
                                        Bolkow Apparatebau's technical director, 
                                        Dr. Hermann Mylius, began work on the 
                                        design of a light all-metal two-seater 
                                        training, aerobatics and glider towing 
                                        aircraft, under the designation MHK-101. 
                                        Clearly owing much to be Bo 208 Junior, 
                                        with some commonality of components new 
                                        wing and a winder fuselage to provide 
                                        more room in the cabin. The prototype 
                                        took off on its maiden flight on 22 
                                        December 1967, powered by a 115-hp 
                                        (86-kW) Lycoming, developed as the 
                                        Bolkow 209 Monsun and manufacturing of a 
                                        wider fuselage to provide more room in 
                                        the cabin. The prototype took off on its 
                                        maiden flight on 22 December 1967 
                                        Powered by a 115-hp (86 kW) Lycoming 
                                        O-235-C2A engine. It was developed as 
                                        the Bolkow 209 Monsun and Manufacturing 
                                        of a prototype began in January 1969, 
                                        this making its first flight on 28 of 
                                        May.  
                                         
                                        The main production variants were the Bo 
                                        209-150, powered  by a 150 hp (112 
                                        kW) Avco Lycoming )-320-E1C engine 
                                        driving a McCauley fixed pitch or 
                                        optional Hartzell constant speed 
                                        propeller, and the Bo 209-160 with a 
                                        160-hp (119-kW) AVCO Lycoming IO-320-DIA 
                                        fuel injection equipped engine fitted 
                                        with the Hartzell propeller as standard. 
                                        Both models had folding wings to reduce 
                                        hangar space requirements and to 
                                        facilitate towing of the aircraft behind 
                                        a car; they also had retractable 
                                        nosewheels and fixed main wheels. The 
                                        Monsun was also available as the Bo 209S 
                                        two-seat trainer, with non-folding wings 
                                        and non-retraceable landing gear. 
                                        Production of all models totalling 102. 
                                        creasing in 1971.  
                                        
                                        Specification
                                        Type:
                                        
                                        two-seater light monoplane
                                        
                                        Powerplant:
                                        one 
                                        160-hp (119-kW) Avco Lycoming IQ-320-D1A 
                                        flat four piston engine.
                                        
                                        Performance:
                                        Maximum 
                                        speed 170mph (127 km/h) at sea level; 
                                        economic cruising speed 151 mph (113 
                                        km/h) at 8,100 ft (2440 m); service 
                                        ceiling 18,100 ft (556 km/h)
                                        
                                        Weights: 
                                        empty 1,067 lb (484 kg); maximum 
                                        take-off 1,807 lb (820 kg)
                                        
                                        The MBB Bo 
                                        209 Monsun is an interesting design, of 
                                        which relatively few were built in three 
                                        versions. The Two Lycoming-engine models 
                                        featured an optionally retractable 
                                        nosewheel leg.
                                        
                                        Dimensions:
                                        span 27 
                                        ft 6 3/4 in (8,40 m); 21ft 7 3/4 in 
                                        (6,60 m); height 7 ft 2 1/2 in (2,20 m); 
                                        wing area 110 sq ft (10,20 m2) | 
        
      
    
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