Rotax SI-912 i-004R3 Скачать руководство пользователя страница 9

 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 9 of 15

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

3.6) Inspect the hydraulic valve tappet for correct purging

See 

Fig. 5

 and 

Fig. 6

.

The following check procedure describes the correct method for checking the hydraulic valve tap-
pets.

3.7) Replacement of components

If a hydraulic valve tappet still malfunctions after several engine runs, it must be replaced and the 
valve spring support must be inspected for wear.
All work has to be performed in accordance with the latest Maintenance Manual for the respective 
engine type.

If the valve spring support indicates wear, replace valve spring retainer, valve spring support, both 
valve cotters, valve and hydraulic valve tappet. Additionally perform a detailed visual inspection of 
relevant valve train components of push rod, rocker arm and valve spring for abnormal wear con-
dition.

m

WARNUNG

m

WARNING

Risk of burns and scalds.
Hot engine parts. Always allow engine to cool down to ambient tempera-
ture before starting work.

Step

Procedure

1

Remove valve cover on cylinder 1.

2

Turn crankshaft in direction 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 seconds. You can using a belt tester, for example, to check 
approximately how much force is being exerted. Repeat on other rocker arms.

4

Check distance between rocker arm and valve contact surface. Max. allowable distance 
0.5 mm (0.02 in.).

m

WARNUNG

NOTICE

If it is possible to push the valve tappets further than this limit, perform an 
additional engine run for about 5 min. at 3500 rpm after refitting the valve 
covers. To get the hydraulic valve tappets primed, this process can be re-
peated another 2 times.

Step

Procedure

5

Repeat on all other cylinders.

Step

Procedure

1

Inspect valve spring support (1). Measure the wear referring to the reference surface 
(inner area of valve spring support) in radial direction (2) to outer side with a dial 
gauge. Value t = max. 0.04 mm (0.0016in.). See 

Fig. 6

. An exceeding of 

max. 0.04 mm (0.0016 in.) is not acceptable.

NOTE:

The valve spring support indicates a possible malfunction of valve
train caused by incorrectly or insufficiently purged hydraulic valve
tappets. At standard conditions no wear is visible even after a long
time of operation. If the visual inspection shows some wear on the
valve spring support surface, measure the actual wear with a dial
gauge.

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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