Rotax SI-912 i-004R3 Скачать руководство пользователя страница 8

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02 July 2021

79-00-00

Revision

Page 8 of 15

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

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

SERVICE INSTRUCTION

-

Restore aircraft to original operating configuration.

3.5) Warming up period

NOTE:

At a new installation or modifications to installation do not start the engine before all
installation checks are finished.

3

Observe oil pressure and oil flowing out of the disconnected hose.

NOTE:

If oil is not flowing out of detached hose within 10 seconds, stop
the engine immediately and find the trouble. repeat the previous
steps until proper oil flow is observed. The engine must not be
returned to service before rectification

4

Fit the turbo oil return hose (pos. 2 on Fig. 1) on oil tank. See latest Maintenance Man-
ual Heavy (MMH) for the respective engine type or instruction of aircraft manufacturer 
for ROTAX

®

 914, 916 i and 915 i Series.

Step

Procedure

m

WARNUNG

NOTICE

Before commencing with the warming 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 installed and tested O.K. according to spec-
ifications of aircraft manufacturer.

Step

Procedure

2

Connect negative terminal of aircraft battery.

3

Start engine and observe oil pressure.

m

WARNUNG

NOTICE

If oil pressure does not raise within 5 sec. after engine start, shut engine 
off. Do not start engine before lubrication system is checked and purging 
procedure is repeated.
Repeated test starts with no indicated oil pressure will severely damage 
the engine.

Step

Procedure

4

Run engine for about 7 min. at approx. 2500 rpm. Then warm up engine at 2200 to 
2500 rpm depending on ambient temperature until an oil temperature of 50 °C (122 
°F) is reached.

5

Check oil temperature and pressure values.

6

Stop engine and secure aircraft against unauthorized operation.

7

Check oil level as per operators manual and refill as necessary. Refill oil level in the 
tank to max. mark. Do not overfill, otherwise oil would exit through vent hole during 
operation. At oil level check the max. mark must not be exceeded.

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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