CMD19

Engine for Ultralight and General Aviation Aircrafts

Architecture

4-cylinder boxer

Bore

Stroke

Displacement

cm³

1795,1

Compression ratio

10.5:1

Gear RR

2.667:1

Induction type

Naturally aspirated

Fuel Injection Sys.

Indirect electronic injection system multi point

Fuel

Gasoline EN228 - RON 95

Min. BSFC

g/kWh

280

Cruise fuel consumption [cruise @ sea level]

l/h

EECS

SINGLE FADEC ECU

Alternator

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

Cooling System

Liquid-cooled

Dry weight

85 with Gearbox

Weight to fly

Dry weight + 5kg of liquids

Dimension (LxWxH)

588 x 617 x 470 with Gearbox

Take-Off power

kW/Hp

89/120 @ 5800 rpm

Maximum Continuous power

kW/Hp

75.5/102 @ 5500 rpm

Max Altitude

12,000