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===Dimensions===
===Dimensions===
Span 9.55 m
*Wing span 9.55 m
Wing area 14.00 m2
*Wing area 14.00 m2
Length 5,70 m
*Length 5.70 m
Height ground attitude 2,11 m
*Height ground attitude 2.11 m
Height flight attitude 2.17 m
*Height flight attitude 2.17 m


===Engine Plant===
===Engine Plant===
====Engine====
====Engine====
Manufacturers Bombardier Rotax GmbH, Austria
*Manufacturers Bombardier Rotax GmbH, Austria
Engine type: Rotax 912 UL
*Engine type: Rotax 912 UL
*Liquid- and air-cooled 4-cylinder four-stroke engine.
Maximum 80 hp @ 5800 RPM
*2 pcs flottörförgasare fitted with the choke knob.
Gearbox with a 2.43:1 reduction ratio
*Ignition: Dual Ignition system with CDI ignition.
*Starting system: Electric Starter Motor. *Maximum 80 hp @ 5800 RPM
*Gearbox with a 2.43:1 reduction ratio


=====Labeling of engine instruments=====
Liquid- and air-cooled 4-cylinder four-stroke engine.
*Green arc (normal area) 1400-5500 RPM
2 pcs flottörförgasare fitted with the choke knob.
*Yellow arc (non-continuous power) 5500-5800 RPM
Ignition: Dual Ignition system with CDI ignition.
*Red line (max power) 5800 RPM
Starting system: Electric Starter Motor.

Labeling of engine instruments
Green arc (normal area) 1400-5500 RPM
Yellow arc (non-continuous power) 5500-5800 RPM
Red line (max power) 5800 RPM


====Propeller====
====Propeller====
Manufacturer: Warp Drive Inc., USA.
*Manufacturer: Warp Drive Inc., USA.
Type Ivo Prop 3-blade carbon fiber laminate with duralnav adjustable on the ground.
*Type Ivo Prop 3-blade carbon fiber laminate with duralnav adjustable on the ground.
Default 12.5 degrees. at the propeller tip. Disk 68 ".
*Default 12.5 degrees. at the propeller tip. Disk 68 ".


====Fuel====
====Fuel====
Type: Non-alcoholic petrol RON 95 PREMIUM max 100LL.
*Type: Non-alcoholic petrol RON 95 PREMIUM max 100LL.
Wing Tank 82 liters. A fuel tank of 41 liters is mounted in each wing.
*Wing Tank 82 liters. A fuel tank of 41 liters is mounted in each wing.
Wing Tank utnyttjningsbart 78 liters.
*Wing Tank utnyttjningsbart 78 liters.


===Electrical===
===Electrical===
Line 56: Line 54:


===Trunk===
===Trunk===
Volume 20 liters.
*Volume 20 liters.
Max load 18 kg.
*Max load 18 kg.





Revision as of 13:28, 24 October 2009

Lamco Eurocub
Role Fixed wing ultralight aircraft
Manufacturer Danex Engineering Kft

The Lamco Eurocub is an ultralight aircraft with fixed gear (taildragger), general aviation airplane, manufactured in Hungary by Danex Engineering Kft. It is used primarily for flight training, touring, and personal flying.

General Description

The Lamco Eurocub is a single-engined high-wing monoplane with the two seats placed side-by-side. The Eurocub is manufactured with either an 80 hp (60 kW) Rotax 912 UL engine or a 100 hp (75 kW) Rotax 912 ULS 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 2.43:1 reduction ratio.

Specifications

These specifications relate to the Lamco Eurocub Mk IV fitted with a Rotax 912 UL engine (80 hp)[1].

Dimensions

  • Wing span 9.55 m
  • Wing area 14.00 m2
  • Length 5.70 m
  • Height ground attitude 2.11 m
  • Height flight attitude 2.17 m

Engine Plant

Engine

  • Manufacturers Bombardier Rotax GmbH, Austria
  • Engine type: Rotax 912 UL
  • Liquid- and air-cooled 4-cylinder four-stroke engine.
  • 2 pcs flottörförgasare fitted with the choke knob.
  • Ignition: Dual Ignition system with CDI ignition.
  • Starting system: Electric Starter Motor. *Maximum 80 hp @ 5800 RPM
  • Gearbox with a 2.43:1 reduction ratio
Labeling of engine instruments
  • Green arc (normal area) 1400-5500 RPM
  • Yellow arc (non-continuous power) 5500-5800 RPM
  • Red line (max power) 5800 RPM

Propeller

  • Manufacturer: Warp Drive Inc., USA.
  • Type Ivo Prop 3-blade carbon fiber laminate with duralnav adjustable on the ground.
  • Default 12.5 degrees. at the propeller tip. Disk 68 ".

Fuel

  • Type: Non-alcoholic petrol RON 95 PREMIUM max 100LL.
  • Wing Tank 82 liters. A fuel tank of 41 liters is mounted in each wing.
  • Wing Tank utnyttjningsbart 78 liters.

Electrical

Rotax 912 UL engine is equipped with a generator on the motor shaft, from 13.5 to 14.2 V / 250 W.

Trunk

  • Volume 20 liters.
  • Max load 18 kg.


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

References

Media related to Lamco Eurocub at Wikimedia Commons

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