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SI-916 i-003R1 / SI-915 i-003R2
SI-912 i-004R3 / SI-912-018R4 /
SI-914-020R4
Carry out further warm up and inspection of the hydraulic valve tappets in compliance with section
3.2 and 3.3 until all 8 hydraulic valve tappets are hard and the max. allowable distance is not
exceeded.
3.8) Test run
Conduct test run.
In case of uninstalled engines test run is accomplished with the mandatory test run after installa-
tion into aircraft.
3.9) Summary
These instructions (section 3) have to be followed in accordance with the deadlines specified in
section 1.5.
The execution of the Service Instruction must be confirmed in the logbook.
NOTE:
Translation into other languages might be performed in the course of language localization but
does not lie within ROTAX
In any case the original text in English language and the metric units are authoritative.
3.10) Inquiries
Inquiries regarding this Service Instruction should be sent to the ROTAX
of your area.
A list of all ROTAX
www.flyrotax.com.
02 July 2021
Revision
Copyright - BRP-Rotax GmbH & Co KG. All rights reserved.
See Chapter 12-20-00 of the latest Maintenance Manual Line (MML) for the respec-
tive engine type.
Work on EASA certified parts might affect the EASA Form 1 and does require appro-
priate documentation by authorized persons. Repairs must be entered into the engine
logbook and also do apply for the EASA Form 1.
A revision bar outside of the page margin indicates a change to text or
graphic.
scope of responsibility.
®
Authorized Distributors or their independent Service Centers is provided on
®
SERVICE INSTRUCTION
®
Authorized Distributor
79-00-00
Page 10 of 15
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