Rotax 912 i series User manual

AIRCRAFT ENGINES
ref. no.: OM-912 i | part no.: 898740

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 equipment manufactur-
ers handbook for additional instructions!
WARNING
These technical data and the information embodied therein are the property of BRP-Powertrain
GmbH&Co KG, Austria, acc, BGBI 1984 no. 448, and shall not, without prior
written permission of BRP-Powertrain 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 2014© - all rights reserved.
ROTAX®is a trade mark of BRP-Powertrain GmbH&Co KG. In the following document the
short form of BRP-Powertrain GmbH&Co KG = BRP-Powertrain 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.
Approval of translation has been done to best knowledge and judgement - in any case
the original text in german language is authoritative.

Effectivity: 912 i Series BRP-Powertrain page INTRO-1
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d05270.fm
Introduction
Foreword BRP-Powertrain provides “Instructions of Continued Airworthi-
ness”, 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-Powertrain.
This Operator Manual contains important information about safe
operation of the engine, together with descriptions of the system
and its layout, technical data, operating media and the operational
limits of the engine.
The specified data apply only to the engine and not to specific ap-
plications in particular aircraft. The aircraft manufacturers Opera-
tors Manual is therefore definitive in terms of the operation of the
engine, as it contains all of the aircraft-specific instructions.
Chapter structure The structure of the Manual follows whenever it is possible the
structure of the „GAMA Specification #1 for Pilot’s Operating
Handbook“. The Operators Manual is subdivided into the following
chapters:
Subject Chapter
Introduction Chapter INTRO
List of effective pages Chapter LEP)
Table of amendments Chapter TOA)
General note Chapter 1)
Operating instructions Chapter 2)
Standard operation Chapter 3)
Abnormal operation Chapter 4)
Performance data Chapter 5)
Weights Chapter 6)
Description of systems Chapter 7)
Checks Chapter 8)
Supplements Chapter 9)

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NOTES

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d05692.fm
LEP) List of effective pages
Chapter Page Date
cover page
INTRO INTRO-1
INTRO-2
01 01 2012
01 01 2012
LEP LEP-1
LEP-2
04 01 2014
01 01 2012
TOA TOA-1
TOA-2
TOA-3
TOA-4
04 01 2014
01 01 2012
04 01 2014
01 01 2012
11-1
1-2
1-3
1-4
1-5
1-6
1-7
1-8
1-9
1-10
1-11
1-12
1-13
1-14
01 01 2012
01 01 2012
01 01 2012
01 01 2012
01 01 2012
04 01 2014
01 01 2012
01 01 2012
01 01 2012
01 01 2012
04 01 2014
07 01 2012
01 01 2012
04 01 2014
22-1
2-2
2-3
2-4
2-5
2-6
2-7
2-8
01 01 2012
04 01 2014
04 01 2014
01 01 2012
04 01 2014
01 01 2012
01 01 2012
01 01 2012
33-1
3-2
3-3
3-4
3-5
3-6
3-7
3-8
3-9
3-10
3-11
3-12
3-13
3-14
3-15
3-16
04 01 2014
01 01 2012
01 01 2012
01 01 2012
01 01 2012
04 01 2014
10 01 2013
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
44-1
4-2
4-3
4-4
4-5
4-6
4-7
4-8
4-9
4-10
01 01 2012
07 01 2012
01 01 2012
01 01 2012
01 01 2012
01 01 2012
01 01 2012
04 01 2014
04 01 2014
01 01 2012
55-1
5-2
5-3
5-4
5-5
5-6
01 01 2012
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
66-1
6-2
01 01 2012
01 01 2012
77-1
7-2
7-3
7-4
7-5
7-6
7-7
7-8
7-9
7-10
7-11
7-12
01 01 2012
01 01 2012
01 01 2012
01 01 2012
04 01 2014
04 01 2014
01 01 2012
01 01 2012
01 01 2012
01 01 2012
01 01 2012
01 01 2012
88-1
8-2
04 01 2014
01 01 2012
99-1
9-2
9-3
9-4
9-5
9-6
9-7
9-8
01 01 2012
01 01 2012
01 01 2012
01 01 2012
01 01 2012
01 01 2012
01 01 2012
04 01 2014
rear page
Chapter Page Date

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NOTES

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d05693.fm
TOA) Table of amendments
Approval*
The technical content of this documents is approved
under the authority DOA ref. EASA.21J.048
current
no.
chapter page date of
change
remark
for
approval
date of
approvalfrom
authorities
date of
inclu-
sion
signa-
ture
01 up to 9 all 01 01 2012
1
1
1
1
1
LEP
TOA
1
2
4
LEP-1
TOA-1, 3
1-11, 11-12
2-2, 2-3
4-2
07 01 2012
07 01 2012
07 01 2012
07 01 2012
07 01 2012
DOA*
DOA*
DOA*
DOA*
DOA*
2
2
2
2
2
2
2
2
2
2
LEP
TOA
1
2
3
4
5
7
8
9
LEP-1
TOA-1, 3
1-6,1-11,1-14
2-2, 2-3, 2-5
3-1, 3-6,
3-8 to 3-16
4-8, 4-9
5-2 to 5-6
7-5, 7-6
8-1
9-8
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
DOA*
DOA*
DOA*
DOA*
DOA*
DOA*
DOA*
DOA*
DOA*
DOA*
DOA*

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NOTES

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TOA) Summary of amendments
Content Summary of the relevant amendments in this context, but without
requirement on completeness.
Current
No.
Chapter Page Date of change Comments
1
1
1
1
1
1
1
2
2
4
1-11
1-12
2-2
2-3
4-2
07 01 2012
07 01 2012
07 01 2012
07 01 2012
07 01 2012
Standard version corrected
Certification supplemented
Oil pressure
Ambient temperature
Available landing site
2
2
2
2
2
2
2
2
1
2
3
4
5
7
8
9
1-11,1-14
2-2, 2-3
2-5
3-8 to 3-16
4-8, 4-9
5-2 - 5-6
7-5, 7-6
8-1
9-8
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
04 01 2014
Standard version corrected, Note added
Notice added,EGT temperature changed,
[psi] values corrected
AVGAS description corrected
Engine Start-, Check-, Take-off-, Shut
down procedure changed/updated
Text corrected, step added
New charts + POWER/ECO description
General note: text added, new grafic
Note added
Distributor for Pakistan added

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NOTES