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 part has been then tested and released by BRP-Rotax, but it might not be certified for the relevant engine type. In such a case the correct function in conjunction with the entire system is the responsibility of the aircraft manufacturer and must be carried out jointly with the aircraft.
SERVICE INSTRUCTION PAC
1.8) Mass data
Change of weight none.
Moment of inertia unaffected.
1.9) Electrical load data
In addition to this technical information refer to current issue of in general Illustrated Parts Catalog (IPC) and in particular:
- Chapter 76-10-00
- in general Operators Manual (OM)
- in general Installation Manual (IM)
- in general Maintenance Manual Line (MML) and in particular:
- Chapter 12-20-00
- in general Maintenance Manual Heavy (MMH) and in particular:
- Chapter 76-10-00
Price and availability will be provided on request by ROTAX® Authorized Distributors or their independent Service Centers.
2.2) Company support information
- Any possible support by BRP-Rotax will be provided on request by ROTAX® Authorized Distributors or their independent Service Centers
2.3) Material requirement per engine
ROTAX® reserves the right to make any amendments to existing documents, which might become necessary due to this standardization, at the time of next revision or issue.
NOTE: Before maintenance, review the entire documentation to make sure you have a complete understanding of the procedure and requirements.
Illustrated Parts Catalog - related information
See current Installation Manual (IM) for the respective engine type.
|2||Allen screw M5x16||901253|
|4||Lock nut M5||842033|
Installation - related information
Non-compliance with these instructions could result in engine damag- es, personal injuries or death. Danger of damage to engine! There is a risk of short circuits and cable fires during work on the electric system. All installation work on the electric system should be carried out with the engine switched “OFF” and the battery (negative terminal) disconnected. Ignition main and LANE selector switches must be “OFF”.