Rotax 912 i series Manual de usuario

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.

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

OM Edition 1/Rev. 0 January 01/2012

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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

Effectivity: 912 i Series BRP-Powertrain page LEP-1

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LEP) List of effective pages

Chapter Page Date

cover page

INTRO INTRO-1

INTRO-2

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

04 01 2014

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

01 01 2012

04 01 2014

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

04 01 2014

10 01 2013

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

04 01 2014

01 01 2012

55-1

5-2

5-3

5-4

5-5

5-6

01 01 2012

04 01 2014

66-1

6-2

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

04 01 2014

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

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

LEP

TOA

LEP-1

TOA-1, 3

1-11, 11-12

2-2, 2-3

4-2

07 01 2012

DOA*

LEP

TOA

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

DOA*

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NOTES

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OM Edition 1/Rev. 2 April 01/2014

d05693.fm

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

1-11

1-12

2-2

2-3

4-2

07 01 2012

Standard version corrected

Certification supplemented

Oil pressure

Ambient temperature

Available landing site

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

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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d05693.fm

NOTES

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