Trade.Information

Product Name: Mission M106 Aircraft Description

Product Description

The Mission M106 is a single engine light aircraft in Microlight/Ultralight/ULM category of conventional configuration. It has an unswept untapered high wing. The fuselage provides comfortable side-by-side seating. Two upwards hinging doors provide access to the cabin. The large transparent areas of the cabin provide excellent visibility in level flight as well as in turns. Both the seats and rudder pedals are adjustable. Elevator and aileron control is by sticks. The aircraft is standard equipped with full dual controls.

The fuselage is a welded space frame, which is fabric covered. High strength steel tubing is used throughout. The wings are of aluminium construction and also fabric covered.
Control surfaces are conventional with single slotted flaps, pushrod operated elevator and cable operated rudder and ailerons. The main landing gear consists of composite cantilever leaf springs. The Mission M106 is available as either a tailwheel or a nosewheel version.

The front mounted UL260i engine produces 82 HP at 2800 rpm and drives either a two blade fixed pitch propeller, or three blade ground adjustable propeller. The four stroke four cylinder engine is air cooled and features FADEC (Full Authority Digital Engine Control).

A \'glass cockpit\' is standard in the Mission M106. All flight instruments are integrated in the EFIS. Engine instruments are displayed on the EMS. We offer a choice of three instrument panel layouts with displays of different sizes. Optionally, these avionics can be complemented with navigation and communication equipment, such as a GPS with moving map, VHF radio and ATC transponder.

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