d0
65
1
5
.f
m
08 February 2019
24-30-00
Initial Issue
Page 20 of 21
Copyright - BRP-Rotax GmbH & CO KG. All rights reserved.
SI-PAC-001
SERVICE INSTRUCTION -
PAC
Dynamic propeller balance
Dynamic propeller balancing is required after external alternator set installation. Max tolerated
imbalance is 0.5 gram (0.0011 lb) or industry standard of max. 0.05 IPS.
-
Restore aircraft to original operating configuration.
-
Connect negative terminal of aircraft battery.
3.6) Test run
Conduct test run. See Chapter 12-20-00 of the latest Maintenance Manual Line for the respective
engine type.
3.7) Summary
The execution of the Service Instruction - PAC
must be confirmed in the logbook.
A revision bar outside of the page margin indicates a change to text or
graphic.
Translation into other languages might be performed in the course of language localization but
does not lie within ROTAX
®
scope of responsibility.
In any case the original text in English language and the metric units are authoritative.
3.8) Inquiries
Inquiries regarding this Service Instruction - PAC
should be sent to the ROTAX
®
Authorized Dis-
tributor of your area.
A list of all ROTAX
®
Authorized Distributors or their independent Service Centers is provided on
www.flyrotax.com
.
m
WARNUNG
NOTICE
Engine vibrations can be caused by an improperly balanced propeller.
Operation without dynamic propeller balancing may cause engine dama-
ge.