SOLO Aircraft Engine 2350 C View larger

SOLO® Aircraft Engine 2350 C

Description of construction

  •   In-line-two-cylinder-two-stroke engine
  •   Air-cooling
  •   Mixture control
  •   Two diaphragm carburetors with additional fule pump
  •   CDI ignition
  •   Propeller mounted on belt drive
  •   Electri engine starter 12 V, 400 W

Operational data and limitations

Take-off-speed, power22 kW (30 HP) at 6,500 1/min.
Max cont. speed, power20 kW (27 HP) at 6,100 1/min.
Recommended rpm6,500 1/min.
Idle rpm3,000 1/min.
Cylinder head temp.Max. 275°C
Fuel consumption100% cont. speed approx 3.96 US gal./hr. (15.0 l/hr.)
75% cont. speed approx. 3.7 US gal./hr. (14.0 l/hr.)
Engine Displacement430 ccm, cyl. bore 70 mm, stroke 56 mm
Compression Ratio12 : 1
Ignition UnitMagneto SOLO, ignition coil BOSCH or PVL
Ignition PlugsBOSCH W 5 AC heat range 225 or Champion L82 C, Gap 0,5 mm
CarburetorMIKUNI BN 38
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 Weight25 kg
StarterFa. SJCE type: 101
Belt DriveRatio 1:2,3

SOLO 2350 C Technical Drawing

PDF File

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Inspection Instruction 4603-1

Engine type: Solo 2350C Subject Inspection of the axle 20 31 216 for cracks and if necessary replacement of the part. Installed in aircrafts DG 1000 T

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AIRWORTHINESS DIRECTIVE

AD20150052-R1 (19.11.15)

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Spare parts list SOLO 2350 C

Ed. 6

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Engine Manual 2350 C

english version

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Engine Manual 2350 C

german version

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TM 4603-5

Change of the carburetor cover of the carburetor BN 38 for the engine 2350C

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TM 4603-15

Use of a new petrol pump (12.08.14 )

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TM 4603-17

Service Bulletin - Change of the axle (15.07.15)

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TM 4603-9

21.04.94 Unleaded fuel for the use in the engines 2350, 2350B, 2350BS and 2350C 21.04.94

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Summary Fuel and Oil

Summary Fuel and Oil for SOLO Aircraft Engines

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TM 4603-18

a) Introduction of a nut with flange at the excentric axle. b) Intoduction of a lifetime limit of 15 years of operation for the ball bearings at the bearing block of the reduction gear.

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Techn. Information Spark plugs

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Airworthiness Directive

ATA 72 – Engine – Propeller Reduction Gear Excentric Axle Bearings – Replacement

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