SOLO Aircraft Engine 2350 D View larger

SOLO® Aircraft Engine 2350 D


Description of construction

  •   In-line-two-cylinder-two-stroke engine
  •   Air-cooling
  •   Mixture control via two diaphragm carburetors
  •   CDI ignition
  •   Propeller mounted on belt drive
  •   No engine starter
  •   Crank-case-pressure operated fuel pump

Operational data and limitations

Take-off-speed, power and Max. cont. speed, power22 kW at 6,500 1/min.
Max rpm6,600 1/min.
Idle rpmNot available - no throttle control
Cylinder head temp.Max. 275°C (measured at spark plug)
Fuel consumption at cruiseApprox 3.7 US gal./hr (14 l/hr.)
Engine Displacement430 ccm, cyl. bore 70 mm, stroke 56 mm
Compression Ratio12 : 1
Ignition UnitMagneto SOLO, ignition coil Ducati
Ignition PlugsBOSCH W 5 AC heat range 225 or Champion L82 C, Gap 0,5 mm
CarburetorSOLO, metering-device WALBRO
Fuel PumpBING
Direction of rotationCounterclockwise, seen in direction of flight
Fuel2-Stroke mix, AVGAS 100LL, premium gas (min. 95 ROZ)
MixtureMixture ratio 1 : 40 , 2-stroke Castrol mineral oil or synthetic oil, or other oils with specification according to JASO FC oder FD
Dry WeightApprox. 23,5 kg, complete with muffler, without propeller
Belt DriveRatio 1:1,56

AIRWORTHINESS DIRECTIVE

AD 2002-130/2 (27.04.02) Engine: Solo 2350 D Subject: Reinforcement of the propeller bearing block on the engine 2350D english version

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AIRWORTHINESS DIRECTIVE

AD 2002-130/2 (27.04.02) Engine: Solo 2350 D Subject: Reinforcement of the propeller bearing block on the engine 2350D german version

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TM 4603-12

Check of the carburetor housing (26.07.11)

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TM 4603-11

Reinforcement of the propeller bearing block on the engine 2350D (15.04.02)

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Summary Fuel and Oil

Summary Fuel and Oil for SOLO Aircraft Engines

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