The Aviation DataBase: Service Information: Solo Kleinmotoren
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Drawings
NameRevisionLangSubjectDate
en 2625-01i06/04/2018
Installation Instructions
NameRevisionLangSubjectDate
en Inspection of Engine Starter and if Necessary, Replacement of Part07/20/2015
en Inspection of Axle 20 31 216 for Cracks & if necessary Replacement of Part03/26/2015
Maintenance Instructions
NameRevisionLangSubjectDate
en SOLO 2 350: After 5 Years of Operation06/19/2001
Manuals (General)
NameRevisionLangSubjectDate
Iss 4 en 10/17/2014
4 en 10/22/2014
Iss 3 en 10/22/2014
Iss 4 en 10/17/2014
Iss 4 en 01/20/2022
en 10/07/1998
Iss 2 en 01/05/2001
Iss 2 en 12/11/2018
en 04/16/2019
Iss 2 en 01/05/2001
en 04/16/2019
en 03/25/2023
Parts Catalogs
NameRevisionLangSubjectDate
Ed 3 en 2350 Mounted in Schleicher Airplanes01/18/2019
Ed 3 en 2350 Mounted in Schempp-Hirth Airplanes01/18/2019
Ed 3 en 2350 Mounted in LAK Airplanes01/18/2019
Ed 6 en 05/17/2019
Ed 6 en 01/27/2022
Ed 5 en 11/30/2018
en 2625 01i & 2625 01i neo08/05/2019
en 2625 02i & 2625 02i neo08/05/2019
Ed 3 en 01/12/2017
Ed 2 en 12/03/2018
Ed 3 en 01/12/2017
Service (Technical) Bulletins
NameRevisionLangSubjectDate
en Limitation of Belt – Tension if Propeller is Driven by Belt. Use of an Additional Bearing. Increase of Max. Belt – Tension for Engines: 2 625 01 (from No. 124) & 2 625 02 (from No. 20)10/03/1999
en Optional Use of a Slip-Clutch on Engines 2 625 01 & 2 625 0202/06/2004
3 en Change of Slip-Clutch on Engines 2 625 01 & 2 625 0203/22/2007
Iss 2 en Check and Modification of Slip-Clutch on Engines 2 625 01 and 2 625 0201/03/2007
Iss 3 en Change of 2 625 02 from Version with Carburetors to Version with Electronic Engine Management for Fuel Injection & Ignition. Change of Type to 2 625 02 I with New S/N Consisting of Present Number Plus Number of Changed Engine12/18/2014
en Change of Throttle System with Improved Connection Profiles and Changed Holder for Bowden Cable in Order to Avoid Cracks on Profiles. Creating More Space for Throttle Sensor in Order to Avoid Damage to Sensor12/12/2012
en Change of Injector Mounts for Redundancy System and Securing of Connection of Lower to Upper Mount11/24/2014
Iss 2 en Change of Injector Mounts for Redundancy System and Securing of Connection of Lower to Upper Mount12/12/2014
en Change of Ignition Mapping11/16/2016
en Change of Engine 2 625 01 from Version with Carburetors to Version with Electronic Engine Management for Fuel Injection & Ignition. Change of Type to 2 625 01i with New S/N Consisting of Present Number Plus Number of Changed Engine03/05/2018
en a) Change of Material of Connecting Strips from Aluminum to CFK-Composite; b) Alternative Use of a Different Throttle Position Sensor02/23/2018
Iss 3 en Introduction of a New Throttle Body Assembly 06/26/2019
en Optional Use of a New Engine Controller with Redundant Functions in Conjunction with TM 4600-9 Throttle Valve System, a Fuel Pumps Electronics Unit & a New Speed Sensor. Designation of Engines as 2625 02i neo & SOLO 2625 01i neo09/18/2019
en ECU-Firmware Update08/19/2019
en Cross-Section Reduction of Exhaust Out-Put Pipe02/06/1984
en Hub for Propeller OE-FL 5.83/83 a 5, v 92 for Engine 235008/05/1987
de Exhaust Muffler 25 00 615 with Integrated Rear Silencer for Engine 235002/02/1988
de Propeller Bearing Block 2350 B Engine Crankcase
de Modification to Carburetor Cover of Mikuni BN 38 Carburetor for 2350 C06/19/1990
de Inspection of All 2350 B Engines for Piston Seizure07/31/1990
1 de Fuel Mixture for Engine 2350B. Instructions for Taxiing09/05/1990
2 en Cancellation of Service Bulletin TM 4603 6/1 Under Use of SB TM 4603 9. Use of Unleaded Fuel- with Minimal- 95 Octane in 235O B06/13/1994
de Conversion of 2350B Engines to New Version 2350BS02/06/1992
de Modification of Carburetors on Engine 2 35004/30/1993
en Unleaded Fuel for Engines 35O, Z 350 B, 2 35O BS and 204/21/1994
en Maintenance of Engine - "SOLO 2 350"07/19/2001
en Reinforcement of Propeller Bearing Block04/15/2002
en Check of Carburetor Housing of Front Cylinder in Flight Direction and if Necessary, Replacement of Part07/26/2011
Iss 2 en Check of Carburetor Housing of Front Cylinder in Flight Direction and if Necessary, Replacement of Part12/15/2011
en Check of Axle 20 31 211 for Cracks and if Necessary, Replacement of Part09/24/2012
en Change of Axle 20 31 211 by Axle 20 31 216 and Introduction of New Bearings if a Fixed Propeller is Mounted. Introducing Change Immediately in Production of Engines 2 350 C Beginning from S/N 217204/28/2014
en Introduction of New Fuel-Pump for all Engines 2350 Listed in EASA TCDS No. EASA.E.21908/12/2014
en Change of Engine 2350 into a Version with Electric Starter which is Connected Directly to Crankshaft. Change of Sales Designation to 2350 E05/19/2015
en Change of Axle 20 31 216 by Axle 20 31 211 V2 and Introduction of New Bearings Combined with Execution of SB 1000/26 of DG Flugzeugbau. Introducing Change Immediately in Production of Engines 2 350 C for DG Flugzeugbau and Exchange of Axles in All DG 1000T07/15/2015
Iss 2 en a) Nut with Flange at Excentric Axle; b) Lifetime Limit of 15 Years of Operation for Ball Bearings at Bearing Block of Reduction Gear01/22/2019
en Eccentric Shaft at Reduction Gear01/31/2022
Service Manuals
NameRevisionLangSubjectDate
Ed 5 en 2625 01, 2625 02 & 2625 02i12/10/2018
Ed 2 en 2625 01i12/04/2018
en 2625 01i neo & 2625 02i neo11/26/2020
Miscellaneous
NameRevisionLangSubjectDate
en Summary Fuel and Oil06/01/2016
en Spare Parts List07/01/1996
en Technical information: Spark-Plugs09/12/2019