SOLO^® Aircraft Engine 2350 BS

Description of construction

In-line-two-cylinder-two-stroke engine
Air-cooling
Mixture control via one float type carburetor
CDI ignition
Propeller mounted on belt drive
Electric engine starter
AC generator 12 V, 180 W

Operational data and limitations

Take-off-speed, power and Max. cont. speed, power	17 kW (23 HP) at 5,500 1/min.
Max rpm	5,500 1/min.
Recommended rpm	5,300 1/min.
Idle rpm	2,000 1/min.
Cylinder head temp.	Max. 275°C
Fuel consumption	Max. speed approx 2.38 US gal./hr. (9.0 l/hr.) Cruising speed approx. 1.85 US gal./hr. (7,0 l/hr.) at 5,300 1/min.

Engine Displacement	430 ccm, cyl. bore 70 mm, stroke 56 mm
Compression Ratio	10 : 1
Ignition Unit	Magneto SOLO, ignition coil BOSCH or PVL
Ignition Plugs	BOSCH W 5 AC heat range 225 or Champion L82 C, Gap 0,5 mm
Carburetor	BING
Direction of rotation	Counterclockwise, seen in direction of flight
Fuel	2-Stroke mix, AVGAS 100LL, premium gas (min. 95 ROZ)
Mixture	Mixture ratio 1 : 40 , 2-stroke Castrol mineral oil or synthetic oil, or other oils with specification according to JASO FC oder FD
Dry Weight	26 kg
Starter	Fa. SJCE Tyep: 102 or UNITED TECHNOLOGIES Tyep: 1077-28-Mo 30 sM
Belt Drive	Ratio 1:2,1

SOLO Profi 2T engine oil 1 litre

SOLO 2350 BS Technical Drawing

PDF File

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Engine Manual 2350 BS

english version

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Engine Manual 2350 BS

german version

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TM 4603-15

Use of a new petrol pump (12.08.14 )

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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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TM 4603-7

Change of the engine 2350B to the new version 2350BS german version (06.02.92)

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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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