Rotax SI-912 i-004R3 Скачать руководство пользователя страница 5

 d

068

92.

fm

SI-916 i-003R1 / SI-915 i-003R2
SI-912 i-004R3 / SI-912-018R4 /
SI-914-020R4

SERVICE INSTRUCTION

02 July 2021

79-00-00

Revision

Page 5 of 15

Copyright - BRP-Rotax GmbH & Co KG. All rights reserved.

3.3) Operation - related information

In general all operating limits as per current Operators Manual (OM) have to be observed. In par-
ticular the limits which have influence to induce air into the oil system like e.g. acceleration and 
static roll angle.

Pre-flight check and oil level check

.

3.4) Maintenance - related information

3.4.1) Purging of oil system

See 

Fig. 1

 to 

Fig. 4

.

-

Verify that oil tank connections are connected correctly and secured, and that the oil cooler (if 
fitted) is in the suction line (pos. 1 on Fig. 1) between the oil tank and the oil pump inlet. Verify 
that the oil tank is filled up to the maximum level (to the top of the flat portion of the dipstick). 
Additional oil (up to 0.5 liter) may be added to the tank for the purpose of this procedure.

NOTE:

Consult appropriate engine Installation Manual for diagrams to identify oil tank and oil
pump connections. Older engines may be equipped with oil tanks that have oil ports in
different locations.

See Chapter 3 section 3.2, current Operators Manual (OM) for the respective engine 
type. In particular make sure that the oil level in the oil tank is between the two
marks (max./min.) on the oil dipstick, but must never fall below the min. mark.

All work has to be performed in accordance with the relevant ROTAX

®

 Instructions for 

Continued Airworthiness (ICA) of the respective engine type.

m

WARNUNG

NOTICE

Incorrectly connected oil lines to the oil tank or to the engine will result in 
severe engine damage.

Step

Procedure

1

Disconnect oil return line(s) (pos. 2 on Fig. 1) from the oil tank (915 i and 916 i: two return 
lines).

NOTE:

Do not disconnect the turbo scavenge return line.

2

Place the free end (915 i and 916 i with two free ends) (pos. 3 on Fig.1) of the return oil 
line into a suitable container (pos. 4 on Fig. 1) below the engine.

NOTE:

This step is a cleanliness precaution. Typically, during the purging pro-
cedure, oil does not come out from the hoses.

3

Plug open connection (pos. 7 on Fig. 1) (915 i and 916 i with two connections) on oil tank 
with suitable air tight cap or plug.

4

Remove all of the spark plug connectors from the spark plugs.

5

For easier rotation of engine remove one spark plug from each cylinder.

Содержание SI-912 i-004R3

Страница 1: ...ice Instructions must be observed and complied with in general all relevant Alert Service Bulletins ASB Service Bulletins SB Service Instructions SI Service Letters SL Service Instruction Parts and Ac...

Страница 2: ...maintenance events retrofitting repair and overhaul 1 6 Approval The technical content of this document is approved under the authority of the DOA ref EASA 21J 048 1 7 Labor time Estimated labor hour...

Страница 3: ...Not affected 2 Material Information 2 1 Material Price and availability will be provided on request by ROTAX Authorized Distributors or their inde pendent Service Centers 2 2 Company support informati...

Страница 4: ...el minimum 9 Series Service are entitled to carry out this work Persons with type specific training General Further material on general inspection maintenance and repair can be found also in relevant...

Страница 5: ...may be equipped with oil tanks that have oil ports in different locations See Chapter 3 section 3 2 current Operators Manual OM for the respective engine type In particular make sure that the oil lev...

Страница 6: ...t the air line pressure is between 0 4 5 8 psi and 1 bar 15 psi Do not exceed 1 bar 15 psi m WARNUNG mWARNING Non compliance can result in serious injuries or death Do not remove oil tank or cover bef...

Страница 7: ...Observe to bury no oil Dispose of oil in an environmentally friendly manner Step Procedure m WARNUNG mWARNING Non compliance can result in serious injuries or death Observe the appropriate safety pre...

Страница 8: ...up period the following job tasks need to be performed Step Procedure 1 Ensure that all engine and actuation systems such as carburetor actuation cooling system ignition switch and propeller are inst...

Страница 9: ...irection of normal rotation so that cylinder 1 is set to top dead center both valves are closed 3 Push down the rocker arm on the push rod side with a force F of around 70 N 15 74 lb force for about 3...

Страница 10: ...uction must be confirmed in the logbook NOTE Work on EASA certified parts might affect the EASA Form 1 and does require appro priate documentation by authorized persons Repairs must be entered into th...

Страница 11: ...Page 11 of 15 Copyright BRP Rotax GmbH Co KG All rights reserved 4 Appendix The following drawings should convey additional information Fig 1 Purging of oil system 916 i and 915 i Series 1 Suction oil...

Страница 12: ...ll rights reserved SI 916 i 003R1 SI 915 i 003R2 SI 912 i 004R3 SI 912 018R4 SI 914 020R4 SERVICE INSTRUCTION Fig 2 Purging of oil system 912 i Series 1 Suction line 2 Oil return line 3 Free end 4 Sui...

Страница 13: ...erved Fig 3 Purging of oil system 912 Series IN O U T 6 2 5 8 7 AE 912_0039a 1 4 3 Pressure max 1bar 15 psi Pressure max 1bar 15 psi Relevant plug Relevant plug Direction of rotation on propeller shaf...

Страница 14: ...020R4 SERVICE INSTRUCTION Fig 4 05449 05451 Purging of oil system 914 Series 7 IN O U T 7 4 3 1 2 5 appropriate cap or plug direction of rotation on propeller shaft counterclockwise viewed from the fr...

Страница 15: ...t Fig 6 Valve spring support NOTE The illustrations in this document show the typical construction They may not repre sent full detail or the exact shape of the parts which have the same or similar fu...

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