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Product Name: Mission M212 Aircraft Description
Product Description

The Mission M212 is a single engine light aircraft of conventional
configuration. It has an unswept straight-tapered low wing. The fuselage
provides side-by-side seating and has sufficient room to accommodate four
adults. In the initial design stages, significant attention was paid to
visibility, comfort and ergonomics. The single piece forward hinging canopy
provides excellent visibility in level flight as well as in turns. In addition,
the clean arrangement ensures a good and water proof seal and keeps aerodynamic
noise low. Both the seats and rudder pedals are adjustable. Elevator and aileron
control is by sticks. The aircraft is standard equipped with full dual controls.
Control surfaces are conventional with single slotted flaps and an all-moving
horizontal tail. The main landing gear consists of a cantilever leaf spring and
the steerable nosewheel is of the telescopic oleo-pneumatic type. The airframe
is all composite. Construction is mainly of glass fibre and epoxy. Carbon
reinforcements are used in spars and longerons where additional stiffness is
required
Company Details
Founded in 1996, Lambert Aircraft Engineering is a specialist in the design
and prototype construction and production of light aircraft having an
all-composite airframe. Lambert Aircraft Engineering is fully equipped to
design, develop,... more
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Avionics shop, Mission M106 Aircraft Description, Pilot shop |
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