Rotax 915 i A SERIES User manual

AIRCRAFT ENGINES

ref. no.: OM-915 i A| part no.: 898851

OPERATORS MANUAL

FOR ROTAX® ENGINE TYPE 915 i A SERIES

picture: ROTAX® 915 iS 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: 915 i A Series

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BRP-Rotax Page Content-1

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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 – Preservation and storage

Chapter 9 – Supplement

Chapter 10 – Proper disposal

Page Notes-2

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BRP-Rotax Effectivity: 915 i A Series

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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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BRP-Rotax Page INTRO-1

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Page Notes-2

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NOTES

LEP) LIST OF EFFECTIVE PAGES

Chapter Page Date

cover

page

INTRO 1 Dec. 01 2017

2 Dec. 01 2017

LEP 1 Dec. 01 2017

2 Dec. 01 2017

TOA 1 Dec. 01 2017

2 Dec. 01 2017

1 1 Dec. 01 2017

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2 1 Dec. 01 2017

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8 Dec. 01 2017

Chapter Page Date

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BRP-Rotax Page LEP-1

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Chapter Page Date

3 Dec. 01 2017

4 Dec. 01 2017

7 1 Dec. 01 2017

2 Dec. 01 2017

3 Dec. 01 2017

4 Dec. 01 2017

5 Dec. 01 2017

6 Dec. 01 2017

7 Dec. 01 2017

8 Dec. 01 2017

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12 Dec. 01 2017

Chapter Page Date

13 Dec. 01 2017

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15 Dec. 01 2017

16 Dec. 01 2017

8 1 Dec. 01 2017

2 Dec. 01 2017

3 Dec. 01 2017

4 Dec. 01 2017

9 1 Dec. 01 2017

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10 1 Dec. 01 2017

2 Dec. 01 2017

Index

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.

chapter page date of

change

remark

for

appro-

val

date of

appro-

val

from

authori-

ties

date of

inclu-

sion

signa-

ture

0 INTRO all Dec. 01 2017 DOA*

0 LEP all Dec. 01 2017 DOA*

0 TOA all Dec. 01 2017 DOA*

0 1 up to

all Dec. 01 2017 DOA*

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BRP-Rotax Page TOA-1

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Summary of amendments

Summary of the relevant amendments in this context, but without any claim to

completeness.

current

no.

chap-

ter

page date of change comments

Page TOA-2

December 01 2017

BRP-Rotax Effectivity: 915 i A Series

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