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Rotax发动机螺旋桨撞击或发动机意外停机后的发动机检查SL-912 i-001
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Preparation:

Before the propeller gearbox is removed, the work described below must be carried out to identify any further malfunctions:

- General visual inspection, see current Maintenance Manual Line (MML) for the respective engine type.

NOTE: Particular attention is needed in the corresponding zone of the crankcase and gear- box mounting screw holes, including the dowels. If any cracks/abnormalities are found, the engine must be shipped to any Rotax approved overhaul facility for repair/ overhaul.

- Remove the surrounding assemblies, see current airframe and propeller manufacturer’s

instructions.

- Remove the gearbox oil line assy, if installed.

-Remove the external alternator, if installed.


Step

Procedure

1

Remove   the gearbox and drive gear.

See   current Maintenance Manual Line (MML) for the respective engine type.

 

2

Perform   a crankshaft run-out inspection on the PTO side.

See current Maintenance   Manual Heavy (MMH) Chapter72-10-00 for the respective engine type.

 

3

Perform   a crankshaft distortion inspection.

See current Maintenance   Manual Heavy (MMH) Chapter 72-00-00 for the respective engine type.

4

If any of the above   measurements are exceeded, the engine needs to be shipped to any Rotax   approved overhaul facility for repair/overhaul.

 

5

If the above measurements are within limits, perform service of the whole gearbox in accordance with   current Maintenance Manual Heavy (MMH) Chapter 72-10-00 for the respective   engine type.


Step

Procedure

 

 

6

Perform NDT inspection of the   propeller shaft (1), gear set (2) and gearbox housing (3). For 912, 912 i and   914 (series), also perform NDT inspection of the dog hub (4) or clutch hub   (5).

NOTE:   In the case of 912 i, 915 i and 916 i   engine series, the gearbox housing has an electrophoretic coating (black)   that does not require removal in order to perform the crack detection.

 

7

If cracks are detected on any of these   components the parts need to be replaced.

NOTE:   The gearbox mounting screw holes, dowel   holes and roller bearing fixa-   tion screw holes must be carefully inspected for any cracks or abnormal- ities.


1 Propeller shaft

2 Gear set

3 Gearbox housing

4 Dog hub

5 Clutch hub

Step

Procedure

 

8

Disassemble overload clutch and damper clutch. See Chapter 72-10-00 Maintenance   Manual Heavy (MMH).

NOTE:       The overload clutch of the 912, 914 and 912i Series, needs to be shipped   to any Rotax approved overhaul facility for repair/overhaul.

 

9

Check all given wear limits for the   gearbox assy. See current Maintenance Manual   Heavy (MMH) Chapter 72-10-00 of the respective engine type section “Inspection” and “Wear Limits”.

10

Replace all 100% replacement parts in accordance with current Maintenance Manual Line (MML) chapter 05-50-00, for the respective engine type.

1Oil seal

2 Ball bearing

3 Washer

4 Hex screw

5 Thrust washer

6 Ring half (x2)

7 Roller bearing

8 Oil seal

9 Oil inlet flange 10 O-ring

11 O-ring

12 Sealing ring

13 O-ring

14 Retaining ring

15 Torsion shaft

16 Retaining ring

17Needle bearing

Step

Procedure

11

If the rest of the parts are not within given limits or have unusual wear or damage, the parts need to be replaced.

12

Assemble gearbox. See current Maintenance   Manual Heavy (MMH) Chapter 72-10-

00   of the respective engine type, section “Assembly”.

 

13

Re-install drive gear in   accordance with current Maintenance Manual Line (MML) chapter 05-50-00, for   the respective engine type. Check the crankshaft run-out. See current Maintenance Manual Heavy (MMH) Chapter 72-10-00 for the respective engine type.

14

Re-install the gearbox   in accordance with current Maintenance Manual Line (MML) chapter 05-50-00 for   the respective engine type.


Finishing work:

- Install the gearbox oil line assy, if installed.

- Install the external alternator, if installed.

-Install the surrounding assemblies, see current airframe and propeller manufacturer’s instruc- tions.


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