Rotax 582 UL series User manual

AIRCRAFT ENGINES
ref. no.: OM-582 UL | part no.: 899122
OPERATORS MANUAL
FOR ROTAX® ENGINE TYPE 582 UL SERIES
ROTAX® 582 UL DCDI Mod. 99 WITH OPTIONS
ROTAX® 582 UL DCDI Mod. 17 WITH OPTIONS
picture: ROTAX® 582 UL DCDI Mod. 99 with options

Before starting the engine, read the Operators Manual, as it contains
important safety relevant information. Failure to do so may result in per-
sonal injuries including death. Consult the original eq uipment
manufactur-ers handbook for additional instructions!
WARNING
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.
Copyright 2018 © - all rights reserved.
ROTAX® is a trade mark 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.
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.

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Table of Content
Chapter INTRO – Introduction
Chapter LEP – LIST OF EFFECTIVE PAGES
Chapter TOA – Table of amendments
Chapter 1 – General note
Chapter 2 – Operating instructions
Chapter 3 – Standard operation
Chapter 4 – Abnormal operation
Chapter 5 – Performance and Fuel consumption
Chapter 7 – System Description
Chapter 8 – Checks
Chapter 9 – Supplement
Chapter 10 – Proper disposal

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NOTES

INTRO) Introduction
Topics in this chapter
Foreword BRP-Rotax GmbH & Co KG (hereinafter “BRP-Rotax”) provides
“Instructions of Continued Airworthiness”, which are based on
the design, the tests and certification of the engine and its
components. These instructions apply only to engines and
components supplied by BRP-Rotax.
Before operating the engine, read this Operators Manual
carefully. If any passages of the Manual are not clearly
understood or in case of any questions, please contact our
ROTAX® Authorized Distributors or their independent Service
Centers.
This Operators Manual contains important information about
safe operation of the engine together with descriptions of the
systems, technical data, operating media and the operational
limits of the engine.
The specified information and procedures apply only to the
engine and not to specific applications in particular aircraft. The
aircraft manufacturers Operators Manual is therefore definitive
in terms of the operation of the engine, as it contains all of the
aircraft-specific instructions
BRP-Rotax wishes you much pleasure and satisfaction flying
your aircraft powered by this ROTAX® aircraft engine.
Document
structure
The structure of the Manual follows whenever it is possible the
structure of the „GAMA Specification #1 for Pilot’s Operating
Handbook“.
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NOTES

LEP) LIST OF EFFECTIVE PAGES
Chapter Page Date
cover
page
INTRO 1 Jan. 01 2018
2 Jan. 01 2018
LEP 1 Jan. 01 2018
2 Jan. 01 2018
TOA 1 Jan. 01 2018
2 Jan. 01 2018
1 1 Jan. 01 2018
2 Jan. 01 2018
3 Jan. 01 2018
4 Jan. 01 2018
5 Jan. 01 2018
6 Jan. 01 2018
7 Jan. 01 2018
8 Jan. 01 2018
9 Jan. 01 2018
10 Jan. 01 2018
11 Jan. 01 2018
12 Jan. 01 2018
13 Jan. 01 2018
14 Jan. 01 2018
15 Jan. 01 2018
16 Jan. 01 2018
17 Jan. 01 2018
18 Jan. 01 2018
2 1 Jan. 01 2018
2 Jan. 01 2018
3 Jan. 01 2018
4 Jan. 01 2018
Chapter Page Date
5 Jan. 01 2018
6 Jan. 01 2018
3 1 Jan. 01 2018
2 Jan. 01 2018
3 Jan. 01 2018
4 Jan. 01 2018
5 Jan. 01 2018
6 Jan. 01 2018
7 Jan. 01 2018
8 Jan. 01 2018
4 1 Jan. 01 2018
2 Jan. 01 2018
3 Jan. 01 2018
4 Jan. 01 2018
5 1 Jan. 01 2018
2 Jan. 01 2018
7 1 Jan. 01 2018
2 Jan. 01 2018
3 Jan. 01 2018
4 Jan. 01 2018
5 Jan. 01 2018
6 Jan. 01 2018
8 1 Jan. 01 2018
2 Jan. 01 2018
3 Jan. 01 2018
4 Jan. 01 2018
9 1 Jan. 01 2018
2 Jan. 01 2018
10 1 Jan. 01 2018
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Chapter Page Date
2 Jan. 01 2018
Chapter Page Date
rear
page
Page LEP-2
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TOA) Table of amendments
Approval*
The technical content of this document is approved under the authority of
DOA ref. EASA.21J.048.
cur-
rent
no.
chap-
ter
page date of
change
remark
for
appro-
val
date of
approval
from
authori-
ties
date of
inclusion
sig-
na-
ture
0 INTRO all Jan. 01 2018 DOA*
0 LEP all Jan. 01 2018 DOA*
0 TOA all Jan. 01 2018 DOA*
0 1 up to
10
all Jan. 01 2018 DOA*
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Summary of amendments
Summary of the relevant amendments in this context, but without any claim to
completeness.
current no. chapter page date of
change
comments
0 1 up to 10 all Jan. 01 2018 new layout and change of
company name
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