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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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