Power: 11.5 HP/ 7500RPM
Idle Speed: 1400rpm/min
Pulling Force: 25.8kg/100M Altitude, 28.3kg/1800M Altitude
Recommended Propeller: 26x12 27x12 28x10
Spark Plug Special: CM-6
Exhaust Amount: 112cm3
Cylinder Bore Stroke: 45.1mm x 35mm
Compression Ratio: 7.8.1
Lubrication Ratio: 30x1( Break in), 40-50x1(Normal Flying)
Weight: Main Engine-2485g, Exhaust Pipe-115g*2pcs, Ignition-160g
(lighter than the current DLE111)
Exhaust Amount: 56cm3 (DLE55=55.6cm3)
Ratio of Compression: 7.8:1 (7.6:1 for DLE55)
Ratio of Lubricating Capacity: 30:1
Total Weight: 3035g
Material of Muffler and crankcase: Aluminum Magnesium Alloy
(Aluminum Alloy for DLE111)
Machining: CNC processed while others are not.
Crank Case Material: the newest aero material make DLA112 engines
too hard to be damaged.
DLA 112 has its NSK bearing imported from Japan which makes the
life of engine longer while others have their bearing made in their
DLA112 is less weight than other gasoline engines in the same
The appearance of DLA112 is artistically and smooth and shinny,
while others are common.
DLA112used high quality Iridium plugs while others not; comes with
aluminum alloy mufflers.