CMD19 TC

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Engine for Ultralight and General Aviation Aircrafts

APPLICATION

Ultralight Aircrafts
Tactital UAV
Recreational and Commercial purpose

ADDED VALUES

Lower Stress at same power condition
Less Strain components
Reduced engine wear
High technology
Lower maintenance costs
High Performances

Performance

Architecture

4-cylinder boxer

Bore

Stroke

Displacement

cm³

1795,1

Compression ratio

8.25:1

Gear RR

2.667:1

Induction type

Turbo charged

Fuel Injection Sys.

Indirect electronic injection system

Fuel

Gasoline EN228 - RON 95

Min. BSFC

g/kWh

280

Cruise fuel consumption [cruise @ sea level]

l/h

EECS

DUAL FADEC ECU

Alternator

1 x 14V 30A (Main) + 1 x 14V 20A (Cockpit)

Cooling System

Liquid-cooled

Dry weight

96 with Gearbox

Weight to fly

Dry weight + 5kg of liquids

Dimension_ (LxWxH)

588 x 617 x 665 with Gearbox

Take-Off power

kW/Hp

147/200 @ 5800 rpm

Maximum Continuous power

kW/Hp

125/170 @ 5500 rpm

Max Altitude

20,000