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

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

Download (71.47k)

TM 4603-5

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

Download (71.03k)

TM 4603-15

Use of a new petrol pump (12.08.14 )

Download (125.13k)

TM 4603-17

Service Bulletin - Change of the axle (15.07.15)

Download (303.24k)

TM 4603-9

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

Download (56.84k)

Summary Fuel and Oil

Summary Fuel and Oil for SOLO Aircraft Engines

Download (90.91k)

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.

Download (245.36k)

Airworthiness Directive

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

Download (501.53k)
Please wait...