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 be used as instruction for the installation of a ROTAX® aircraft engine in a specific type of airframe or airplane. BRP-Rotax GmbH & Co KG does not assume any warranty or liability in this context.
In no event shall the Installation Manual be used without following the specific instructions and/or requirements of the manufacture of an airframe or airplane (“Manufacturer”). For verification and/or for release of the engine installation, the respective Manufacturer must be contacted. Any modifications or adaptations to the airframe or airplane shall be carried out and/or be verified and released by the Manufacturer only.
Improper use of the Installation Manual and/or non compliance with the installation requirements of the Manufacturers can cause personal injury or property damage. BRP-Rotax GmbH & Co. KG disclaims any liability for any and all damage and/or injuries (including death) resulting from the improper use of Installation Manual and non compliance with the installation requirements of the Manufacturer.
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 of BRP-Rotax GmbH & Co KG, be disclosed in whole or in part to third parties. This legend shall be included on any reproduction of these data, in whole or in part. The Manual must remain with the engine/aircraft in case of sale.
ROTAX® is a trademark of BRP-Rotax GmbH & Co KG. In the following document the short form of BRP-Rotax GmbH & Co KG = BRP-Rotax is used. Other product names in this documentation are used purely for ease of identification and may be trademarks of the respective company or owner.
Table of Content
- Chapter INTRO – GENERAL NOTE
- Chapter LEP – LIST OF EFFECTIVE PAGES
- Chapter TOA – TABLE OF AMENDMENTS
- Chapter 00–00–00 – GENERAL NOTE
- Chapter 10–10–00 – STORAGE AND INSTALLATION
- Chapter 24–00–00 – ELECTRICAL POWER
- Chapter 61–00–00 – PROPELLER DRIVE
- Chapter 72–00–00 – ENGINE
- Chapter 72–60–00 – AIR INTAKE SYSTEM
- Chapter 73–00–00 – ENGINE – FUEL AND CONTROL
- Chapter 75–00–00 – COOLING SYSTEM
- Chapter 76–00–00 – ENGINE CONTROLS
- Chapter 78–00–00 – EXHAUST SYSTEM
- Chapter 79–00–00 – LUBRICATION SYSTEM
- Chapter 80–00–00 – STARTING
In this Manual all ROTAX® 912 Series engines are described.
ROTAX® 912 Series includes 912 A, 912 F, 912 S, 912 UL, 912 UL and 912 ULS.
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.