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 operation. If any passages of the manual are not clearly understood or if you have any questions, please contact a ROTAX® authorized distributor or their independent Service Center for ROTAX® aircraft engines.
BRP-Rotax GmbH & Co KG (hereinafter “BRP-Rotax“) wishes you much pleasure and satisfaction flying your aircraft powered by this ROTAX® aircraft engine. The structure of the manual follows, whenever possible, the structure of the ATA (Air Transport Association) standards. The aim is the compatibility with the aircraft manufacturers documentation, which means they still must adapt or incorporate the documentation to their standard.
BRP-Rotax INSTALLATION MANUAL
The purpose of this Manual is to provide aircraft manufacturers with technical requirements (e.g. interface descriptions and limitations) that must be adhered to when installing this type of engine into an aircraft or certifying aircraft powered by this engine type. Furthermore it should allow independent ROTAX® Maintenance Technicians (iRMT) to install this engine into an airframe in compliance with the relevant installation and safety instructions provided by the engine manufacturer. For detailed information related to aircraft and aircraft/engine installation, maintenance, safety or flight operation, consult the documentation provided by the aircraft manufacturer and/or its dealer.
For additional information on engines, its maintenance or parts, you can also contact your nearest ROTAX® authorized Aircraft Engine Distributor or their independent Service Center.
AUXILIARY EQUIPMENT (OPTIONAL)
Any equipment not included as part of the standard engine version and thus not a fixed component of the engine is not in the volume of supply. Components especially developed and tested for this engine are readily available at BRPRotax.
Auxiliary equipment not certified
The following auxiliary equipment has been developed and tested, but NOT certified for this engine. Certification of auxiliary equipment is the responsibility of the aircraft manufacturer.
See relevant Illustrated Parts Catalog
The representation of components that are not within scope of the delivery is purely symbolic. It does not constitute the specification of the engine version and shall therefore only be seen functionally. The actual interpretation/selection of corresponding regulations is the aircraft manufacturer’s responsibility.
Engine operation
- The engine must always be operated according to the content of the latest Operators Manual
- To eliminate the risk of injury or damage, ensure any loose equipment or tools are properly secured before starting the engine
- The use of propellers and their fastenings which exceed the specified values of moment of inertia and imbalance is not allowed and releases the engine manufacturer from any liability
- Improper engine installation, use of unsuitable piping for fuel, cooling and lubrication system and use of unsuitable wiring for electric and engine management system releases the engine manufacturer from any liability
INSTRUCTION
Engines require instructions regarding their installation, application, use, operation, maintenance and repair. Technical documentation and regulations are useful and necessary complementary elements for trainings, but can by no means substitute for theoretical and practical instructions. These instructions should cover explanation of the technical context, advice for operation, maintenance, installation, use and operational safety of the engine.
Download Installation Manual ROTAX Engine Type: 915 iS A,915 iSc A,915 iS C24,915 iSc C24