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LCA LH 212 Delta helicopter

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Specifications Comment this helicopter
Picture LH_212_Delta
General
Manufacturer LCA
Type LH 212 Delta
Introduced 7/1/2012
In production? Yes
Units produced
Price US $ 165,000.00
Dimensions
Overall Length 20.29 ft
Length 0 ft
Height 7.67 ft
Width 0 ft
   
   
Description

The LH 212 Delta is an ultralight helicopter produced by the Italian LCA Srl company. It first took flight in 2010.

The LH 212 was in development for eight years and bears a striking resemblance to the DF334. However, there is no evidence that the two craft are directly-related.

The Delta has a conventional pod-and-boom design and has two side-by-side seats. The forward transparency is fully clear, giving both occupants good visibility. Tandem controls are fitted as standard, making it a good training craft.

Power is provided by a single 113 horsepower Rotax 914 turbocharged engine. It’s a liquid-cooled flat-four design power plant with radiators mounted behind the seats.

The landing system is a simple skid design with a skid track of 1.585 m.

By 2012 eleven units had been built at a cost of 165 000 Euros. A kit version is planned, but it is unclear if or when it will be available.

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Design features
  • Titanium frame
  • Carbon composite cabin
  • Carbon composite rotor blades
  • Cyclic with T-bar
  • Skid type landing gear
  • Mechanical governor
Description

The LH 212 Delta is an ultralight helicopter produced by the Italian LCA Srl company. It first took flight in 2010.

The LH 212 was in development for eight years and bears a striking resemblance to the DF334. However, there is no evidence that the two craft are directly-related.

The Delta has a conventional pod-and-boom design and has two side-by-side seats. The forward transparency is fully clear, giving both occupants good visibility. Tandem controls are fitted as standard, making it a good training craft.

Power is provided by a single 113 horsepower Rotax 914 turbocharged engine. It’s a liquid-cooled flat-four design power plant with radiators mounted behind the seats.

The landing system is a simple skid design with a skid track of 1.585 m.

By 2012 eleven units had been built at a cost of 165 000 Euros. A kit version is planned, but it is unclear if or when it will be available.

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Design features:
  • Titanium frame
  • Carbon composite cabin
  • Carbon composite rotor blades
  • Cyclic with T-bar
  • Skid type landing gear
  • Mechanical governor
Performance
Persons 2
Max. Range 280 mi
Cruise Speed 99 mph
Max. Speed 124 mph
Max. rate of Climb 1476 ft/min
HOGE ceiling 8202 ft
Service Ceiling 16404 ft
Gross Weight 992 lb
Empty Weigt 606 lb
Useful Load 386 lb
Dynamic system
Fuel Capacity 17 gallons
Number of Engines 1
Engine Type Piston
Engine Code Rotax 914
Horse Power 115
Rotorhead Teetering
Number of rotorblades 2
Rotor Diameter 21.92 ft
Number of tail rotorblades 2
Tailrotor Diameter 0 ft
Blueprints & model
Manufacturer Website manufacturer..
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