Rotax 582 UL series Manuale utente

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.

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.

Effectivity: 582 UL

Edition 3 / Rev. 0

BRP-Rotax Page Content-1

January 01/2018

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

Page Notes-2

January 01/2018

BRP-Rotax Effectivity: 582 UL

Edition 3 / Rev. 0

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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Edition 3 / Rev. 0

BRP-Rotax Page INTRO-1

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Page Notes-2

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Edition 3 / Rev. 0

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

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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

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3 Jan. 01 2018

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7 Jan. 01 2018

8 Jan. 01 2018

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5 1 Jan. 01 2018

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7 1 Jan. 01 2018

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8 1 Jan. 01 2018

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3 Jan. 01 2018

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9 1 Jan. 01 2018

2 Jan. 01 2018

10 1 Jan. 01 2018

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Edition 3 / Rev. 0

BRP-Rotax Page LEP-1

January 01/2018

Chapter Page Date

2 Jan. 01 2018

Chapter Page Date

rear

page

Page LEP-2

January 01/2018

BRP-Rotax Effectivity: 582 UL

Edition 3 / Rev. 0

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

all Jan. 01 2018 DOA*

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Edition 3 / Rev. 0

BRP-Rotax Page TOA-1

January 01/2018

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

Page TOA-2

January 01/2018

BRP-Rotax Effectivity: 582 UL

Edition 3 / Rev. 0

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