SL-912 i-017_915 i-012_Conditions relating to the limited extended warranty under the ROTAX® Care program for ROTAX® Engine Types 912 i (Series) and 915 i (Series) ATA System: 00-00-00 General note…

The coolant radiator may be declared as part of the cooling system on air- craft-side and so might not be a part of the Engine Type Design. Such a PAC…

The optional oil system parts may be declared as part of the oil system on aircraft-side and so might not be a part of the Engine Type Design. Such a…

Congratulation on your decision to use a ROTAX® aircraft engine. Before starting with the engine installation, read this Installation Manual carefully. The Manual will provide you with basic information on…

Planning information To obtain satisfactory results, procedures specified in this publication must be accomplished with accepted methods in accordance with prevailing legal regulations. BRP-Rotax GmbH & Co KG cannot accept…

This Installation Manual for the ROTAX® aircraft engines Type 914 Series should only be used as a general installation guide for the installation of ROTAX® engines into airframes. It should…

The Illustrations in this Manual are stored in a graphic data base system and are provided with a consecutive irrelevant number. This number (e.g. AE 2St_001) is of no significance…

The aircraft related Certification Specification for Light Sport Aircrafts (CS-LSA) permits the usage and installation of an engine which complies with ASTM F2339. Under the above conditions (CS-LSA aircraft with…

Before starting any maintenance work, please read the Maintenance Manual completely as it contains important safety relevant information. Failure to do so may result in personal injuries including death. Consult…

Replacement of electrical fuel pump(s) for ROTAX® Aircraft Engines To obtain satisfactory results, procedures specified in this publication must be accomplished with accepted methods in accordance with prevailing legal regulations…

The electric starter relay assy. is on some ROTAX be a part of the Engine Type Design. Such a PAC part has been then test- ® Aircraft Engines not ed…

This Installation Manual for the ROTAX® aircraft engines type 582 UL Series should only be used as a general installation guide for the installation of ROTAX® engines into airframes. It…

The regulator connector bracket assemblies are not a part of the Engine Type Design. The regulator connector bracket assemblies have been tested and released by BRP-Rotax, but they are not…

This SI revises rotax SI-912-032 / SI-914-033 / SI-2ST-011 dated 20 February 2019 Running modifications of the Bing constant depression carburetor for ROTAX® Engine Type 912 and 914 (Series) and…

Planning information To obtain satisfactory results, procedures specified in this publication must be accomplished with accepted methods in accordance with prevailing legal regulations. BRP-Rotax GmbH & Co KG cannot accept…

The fuel pump service kit is part of the fuel system on aircraft-side and not a part of the Engine Type Design. The fuel pump service kit has been tested…

Technical documentation These documents form the instructions ensuring continued airworthiness of ROTAX® aircraft engines. The information contained herein is based on data and experience that are considered applicable for authorized…

Before carrying out engine installation related work on the engine, read this Installation Manual carefully. The manual will provide you with basic information on correct engine installation for safe engine…

Information about Storage and Storage Conditions of ROTAX Genuine Spare Parts for ROTAX Aircraft Engines. This SL revises SL-916 i-003, SL-915 i-003R1, SL-912 i-011R1, SL-912-022R1, SL-914-020R1, SL-2ST-014R1, dated 04 November…

This Installation Manual for the ROTAX® aircraft engines 912 Series, should only be used as a general installation guide for the installation of ROTAX® engines into airframes. It should not…

SERVICE INSTRUCTION B.U.D.S. Aircraft Installation Instructions and Update for ROTAX® Engine Types 916 i, 915 i, 912 i and 914 Series. This SI revises SI-916 i B-002 / 915 i-002…

Inspection and re-torquing of oil spray nozzle for ROTAX Engine Type 915 i A and 916 iSc B Series (ASTM). ALERT SERVICE BULLETIN For complete instructions and compliance to this…

The oil tank assy. BIG might not be a pa a PAC part has been then tested and released by BRP-Rotax, but it might rt of the Engine Type Design…

The optional accessory drive flange is not part of the Engine Type Design. Such a PAC part has been then tested and released by BRP-Rotax, but it might not be…

The optional fuel pressure adapter is not part of the Engine Type Design. Such a PAC part has been then tested and released by BRP-Rotax, but it might not be…

The optional cooling system parts may be declared as part of the cooling system on aircraft-side and so might not be a part of the Engine Type Design. Such a…

Optional mounting kit for AC-DC Converter for ROTAX® Aircraft Engines ATA System: 24-00-00 Electric Power Planning information: “PAC” Service Instruction Documents provide detailed information on ROTAX® Aircraft Engine Parts and…

This SL revises SL-916 i B-004/SL-915 i-004R1/SL-912 i-012R1/SL-912-004R4/SL-914-004R4 dated 04 November 2020. Documentation for ROTAX® Engine Type 916 i (Series), 915 i (Series), 912 i (Series), 912 and 914 (Series)…

ROTAX Engine Type 915 i A Training Whether you are a qualified pilot or a novice, complete knowledge of the aircraft, its controls and operation is mandatory before a solo…

The optional mounting brackets may be declared as part of the electric system on aircraft-side and so might not be a part of the Engine Type Design. Such a PAC…

These technical data and the information embodied therein are the property of BRP-Rotax GmbH & CO KG, Austria, acc, BGBI 1984 no. 448, and shall not, without prior written permission…

Information about third party after-market replacement piston kits The manufacturers of various modifications are suggesting that replacement of the parts in the ROTAX® engines can be easily undertaken by owners…

The governor flange cover ernor on by the aircraft OEM and so might not be a part of the Engine Type may be declared as part of the hydraulic govDesign…

The connector set may be declared as part of the wiring harness on air- craft-side and so might not be a part of the Engine Type Design. Such a PAC…

The shock mount set is not a part of the Engine Type Design. The mount has been tested and released by BRP-Rotax, but it is not certified. shock The correct…

The overflow bottle part of the Engine Type Design. The is part of the cooling system on aircraft-side and not a Overflow bottle has been tested and released by BRP-Rotax…

The information and components-/system descriptions contained in this Illustrated Parts Catalog are correct at the time of publication. BRP-Rotax, however, maintains a policy of continuous improvement of its products without…

SERVICE INSTRUCTION The 24 Volt electric starter assy. and its connectors may be declared as part of the starting system on aircraft-side and so might not be a part of…

The air filter may be declared as part of the air intake system on aircraft- side and so might not be a part of the Engine Type Design. Such a…

The oil radiator and so might not be a part of the Engine Type Design. Such a PAC part may be declared as part of the oil system on aircraft-side…

Fuel pump assembly for ROTAX® Aircraft Engines ATA System: 73-00-00 Fuel system “PAC” Service Instruction Documents provide detailed information on non-certified ROTAX® Aircraft Engine Parts and Accessories. Referenced parts and…

Replacement of fuel pump nipple fittings on ROTAX® Engine Type 912 (Series) Aircraft Engines To obtain satisfactory results, procedures specified in this publication must be accomplished with accepted methods in…

The fuel filter is part of the fuel system on aircraft-side and not a part of the Engine Type Design. The fuel filter has been tested and released by BRP-Rotax…