SERVICE INSTRUCTION. Optimizing of mixture distribution SI Repeating symbols: 1) Planning information. 1.1) Engines affected

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Optimizing of mixture distribution Repeating symbols: Please, pay attention to the following symbols throughout the Service Bulletin emphasizing particular information. WARNING: Identifies an instruction, which if not followed, may cause serious injury or even death. ATTENTION:Denotes an instruction which if not followed, may severely damage the engine or could lead to suspension of warranty. NOTE: Information useful for better handling. 1) Planning information 1.1) Engines affected All versions of the engine type: 914 F (Series) from S/N 4,420.002 to S/N 4,420.118 Commencing with engine no. 4.420.119 the carburetor calibration has been verified in serial production in accordance with this Service Instruction. 914 UL (Series) from S/N 4,417.503 to S/N 4,417.717 Commencing with engine no. 4.417.718 the carburetor calibration has been verified in serial production in accordance with this Service Instruction. pre-series engines 914 all 1.2) Concurrent ASB/SB/SI und SL further to this service instruction the following additional technical bulletin and service information must be observed: Technical bulletin no. 914-03 current issue Service information 7 UL 97 D/E current issue 1.3) Reason At repair or renewal of the airbox and when encountering mixture distribution problems a matching carburetor calibration will be required to achieve the best possible mixture distribution and consumption values. d00533 page 1 of 6

1.4) Subject Replacement of the main jet 162 ( 268.990). 1.5) Compliance RECOMMENDED for technical reasons it is recommended to Change the main jet to 160 on carburetor 1/3 and to main jet 164 on carburetor 2/4, in accordance with the following instructions a) At replacement of the airbox b) At mixture distribution problems (rough engine run, vibrations etc.) 1.6) Approval not required 1.7) Manpower estimated man-hours: engine installed in the aircraft - - - manpower, depending on installation and therefore no statement is feasible from the engine manufacturer. 1.8) Mass data - change of weight - - -. - moment of inertia - - - unaffected. 1.9) Electrical load data no change 1.10) Software accomplishment summary no change page 2 of 6

1.11) References In addition to this technical information refer to - current issue of the Operator s Manual (OM) - engine data sheet - power, torque and fuel consumption curves - current issue of the Illustrated Parts Catalog (IPC) - Installation Manual (IM) and Check List - all relevant Service Information - all relevant Technical Bulletins - all relevant Service Bulletins (SB) - all relevant Service Instructions (SI) - all relevant Service Letters (SL) - Maintenance Manual (MM) 1.12) Other publications affected 1.13) Interchangeability of parts All parts are interchangeable page 3 of 6

2) Material Information 2.1) Material - cost and availability cost and availability will be supplied on request by our authorized distributors 2.2) Company support information 2.3) Material volume per engine parts volume: For the modification/optimizing of the carburetor jetting the following parts are required: item no. New Qty. Description Old remarks 268.985 1 main jet 160 carb assy. 1/3 268.993 1 main jet 164 carb assy. 2/4 2.4) Material volume per spare part 2.5) Rework of parts 2.6) Special tooling - Price and availability Price and availability will be supplied on request by our Authorized Distributors or their Service Center. parts volume: For the modification/optimizing of the carburetor jetting the following parts are required: item no. New Qty. Description Old remarks as required safety wire attachment screw page 4 of 6

3) Accomplishment / Instructions Accomplishment All the measures must be taken and confirmed by the following persons or facilities: - ROTAX -Distributors or their Service Center - Persons with the respective Aviation Authority - Persons with type-specific training (applicable only for non-certified engines) WARNING: Proceed with this work only in a non-smoking area and not near open flames. Switch off ignition and secure engine against unintentional operation. - Secure aircraft against unauthorized operation. - Disconnect minus pole of aircraft battery. WARNING: Carry out work on a cold engine only. 3.1) Replacement of the airbox (if required) Exchange the airbox assembly as per the current Maintenance Manual 914 F, section 13.1. 3.2) Removal of the main jet 162 ( 268.990) Remove the main jet 162 from the carburetor 1/3 and 2/4 as per the current Maintenance Manual 914 F, section 13.1. 3.3) Installation of the new main jet in the respective carburetor Fitting of the following main jets as per the current Maintenance Manual 914 F, section 13.1: a) on carburetor 1/3 ( 887.091 or 887.092) fit the main jet 160 (part no. 268.985) b) on the carburetor 2/4 ( 887.096 or 887.097) fit the main jet 164 ( 268.993) NOTE: For easy distinguishing of the two carburetors use the throttle potentiometer which is installed only on the carburetor 2/4. Reconnect minus pole of aircraft battery page 5 of 6

3.4) Carburetor synchronisation Synchronize the carburetors as per the current Maintenance Manual 914 F, section 13.1. 3.5) Verification/calibration of the mixture enrichment jet (if airbox was changed) Verify or recalibrate if necessary the mixture enrichment jet for correct position and CO-values as per Technical Bulletin 914-03 or Service Information 7 UL 97 D/E. 3.6) Test run Conduct engine test run inclusive leakage test and ignition check, as per the current Maintenance Manual 914 F, section 12.3.22): 3.7) Summary WARNING: Non-compliance with these recommendations could result in engine damage, personal injury or death! page 6 of 6