Lamco Eurocub
| Lamco Eurocub | |
|---|---|
| |
| Role | Fixed wing microlight aircraft |
| Manufacturer | Danex Engineering Kft |
| First flight | 1996 |
| Number built | 650+ |
The Lamco Eurocub is an ultralight aircraft two-seat, fixed tricycle gear, general aviation microlight airplane, manufactured in Hungary by Danex Engineering Kft. It is used primarily for flight training, touring, and personal flying.
Design and development
The Lamco Eurocub is a single-engined high-wing monoplane with side-by-side seats for two in a 1.22 m (48 in) wide cabin. The Eurocub is manufactured with either an 80 hp (60 kW) Rotax 912 engine or a 100 hp (75 kW) Rotax 912s engine. The Rotax engine has a low fuel consumption and relatively low noise. The engine drives the propeller, which has ground-adjustable pitch, through a gearbox with a 2.273:1 reduction ratio.
The aircraft is structurally supported by a 'backbone' of large diameter aluminium tube which runs the length of the aircraft. The cabin and fuselage shell is a composite material and, being non-structural, can be removed for inspection and repair.
The wings are constructed of tubular front and rear spars. The wings and flying control surfaces are covered in Kevlar/Mylar/Polyester laminate. The wings can be removed or folded (if an optional folding kit is installed) for storage and transportation. The wing tips are of composite construction which reduces drag and improves low speed handling. Access to the cabin is provided by two Gull-wing doors.
Controls
A single centre stick controls the ailerons and elevators. Electrical pitch trim is controlled by two buttons on the top of the stick, operated by the thumb. A push to talk button is on the front of the stick, operated by the index finger, together with a vertical hand operated brake lever similar to a motorcycle front brake lever.
Rudder pedals are dual control. The distance from the seat to the pedals is fixed because the seat position is not adjustable.
The dual control throttle levers are situated between the legs, and pivot from side to side so can be folded out of the way making entry and exit of the aircraft easier.
The flaps are controlled by a centrally-mounted lever on the roof of the cabin. The relatively short lever does make the operation of lowering flaps quite physical when combined with holding the centre control stick at the same time.
Specifications
These specifications relate to the Lamco Eurocub Mk IV fitted with a Rotax 912 UL engine (80 hp)[1].
Speed restrictions
Where a single speed appears, it is applicable to the aircraft at maximum gross weight of 1,040 pounds (470 kg). Where a range appears, the lower speed is applicable at empty weight of 572 pounds (259 kg), while the higher speed is applicable at maximum gross weight.
- VNE (never exceed): 110 Knots
- VNO (max cruise): 95 Knots
- VA (maneuvering): 68 Knots
- VS0 (stall, dirty): 33 Knots
- VY (best rate of climb): 62 Knots
General characteristics
- Crew: 1
- Capacity: 1 passenger
Performance
See also
Aircraft of comparable role, configuration, and era
External links
Media related to Lamco Eurocub at Wikimedia Commons
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