The Light Weight Engine Houtekietstraat 11
B-8540 Deerlijk, Belgium
EFFECTIVITY
page 17
ALL
19-3-2019
Due to the side valve design of the motor, some motor failures normally found with OHV engines (for
example valve tearing will not stop the motor from functioning). Inflight even the loss of one or two
cylinders can be compensated for and the motor continues to run with less power, which allows time
for a safety landing.
The electrical supply is very important for a safe operation of the motor, should the generator fail and
the battery is not charged sufficiently , the motor will continue to run only until the minimum power
supply voltage of 8V is reached. Installation in the electric system of a sufficiently sized capacitor will
ensure continued operation of the engine in the case of a battery failure.
Short specification list
•
Type
: D- motor LF26
•
Class
: Microlight aircraft
•
Engine
: Four cylinder, four stroke, liquid cooled
•
Displacement
: 2690 cc
•
Stroke
: 80 mm
•
Compression ratio
: 8/1
•
Max power
: 69 kW (94hp)
at 3000 RPM
•
Max continuous power
: 65.3KW (88.8 hp) at 2800 RPM
•
Used fuel
: 91, 93, 95. 98 octane or avgas
•
Fuel consumption
: see fuel consumption table
•
Maximum torque
: 220 Nm (162 ft/lbs)
at 2500 RPM
•
Intake
: Multipoint sequential fuel injection
•
Alternator
: 25 Amp integrated
•
Electric starter
: 1.1 KW integrated
•
Ignition
: Double