Girish Mahajan (Editor)

MBB Bo 209

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Top speed
  
274 km/h

Length
  
6.6 m

Wingspan
  
8.4 m

MBB Bo 209 BO209 MonsunBOLKOW B209 L1P L

Manufacturers
  
Messerschmitt-Bölkow-Blohm, Bölkow

The MBB Bo 209 Monsun (originally the MHK-101) is a two-seat light aircraft that was developed in Germany in the late 1960s.

Contents

MBB Bo 209 MBB Bo209 Monsun Airspotru

Design and development

MBB Bo 209 Blkow Bo 209 Monsun Specifications Technical Data Description

The design started as a redesign of the Bo 208 under Bölkow technical director Dr Hermann Mylius but resulted in a vastly different aircraft with little commonality of parts with its predecessor. The fuselage was now wider and incorporated a retractable nose wheel. The wings were redesigned and relocated to a low-wing configuration (the Bo 208 was a high-wing aircraft) and made foldable for towing and storage. The aircraft was marketed with a choice of the fixed or retractable nose wheel, either a 150-hp or 160-hp Lycoming engine, and an optional variable-pitch propeller. A trainer version with dual controls was also manufactured.

MBB Bo 209 Boelkow Monsun Pilot Report

With this broad array of equipment options Bölkow displayed the aircraft at the Air Show in Hanover 1970: 57 orders of the new type were drawn in advance. A commercial success of the project seemed secured, but the fusion of the Bölkow GmbH into the MBB company 1968 led to the economic decision to stop building civil aircraft. Although there were 102 Monsun manufactured between 1969 and 1971. A United States businessman invested in the model, secured funding, and started shipping factory equipment to Georgia. Before completion of the transition, the investor committed suicide after losses in stock market speculation. MBB decided in February 1972 to stop production despite there still being 275 orders outstanding.

MBB Bo 209 httpsuploadwikimediaorgwikipediacommonsthu

In the late 90's Dr. Mylius's son, Albert Mylius, completed a totally revised version of his father's design under a new company "Mylius Flugzeugwerk GmbH & Co KG" based in Bitburg. Two models were produced: a single seat developed as a low cost aerobatic airplane (MY-102) and a two-seat (MY-103) Mylius Aircraft which has some variations over the original Bo 209 design, like wider cockpit, better handling characteristics and improved overall performance (including aerobatic rating) with a more powerful 200HP engine.

Variants

MBB Bo 209 MBB Bo 209 Monsun tourer trainer

  • MHK-101 prototype
  • Bo 209-150 - production version with Lycoming O-320-E1C engine
  • Bo 209-160 - production version with Lycoming O-320-D1A engine
  • Bo 209S - trainer version with dual controls, non-retracting nosewheel, and non-folding wings
  • Specifications (Bo 209-160)

    Data from Jane's All The World's Aircraft 1971-72

    General characteristics

    MBB Bo 209 MBB Bo209 Monsun

  • Crew: one pilot
  • Capacity: 1 passenger
  • Length: 6.60 m (21 ft 7¾ in)
  • Wingspan: 8.40 m (27 ft 6¾ in)
  • Height: 2.20 m (7 ft 2½ in)
  • Wing area: 10.2 m2 (110 ft2)
  • Empty weight: 484 kg (1,067 lb)
  • Gross weight: 820 kg (1,807 lb)
  • Powerplant: 1 × Lycoming O-320-D1A, 119 kW (160 hp)
  • Performance

  • Maximum speed: 274 km/h (170 mph)
  • Cruising speed: 243 km/h (150 mph)
  • Range: 1,200 km (745 miles)
  • Endurance: 5 hours  14 min
  • Service ceiling: 5,520 m (18,100 ft)
  • Rate of climb: 6 m/s (1,180 ft/min)
  • References

    MBB Bo 209 Wikipedia