Export Control
EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.Copyright
© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).Applicability
All
Common Information
TASK 70-46-02-460-501 Bushing Replacement
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-139 ABRASIVE CROCUS CLOTH | LOCAL | CoMat 05-139 | ||
| CoMat 10-039 ENGINE OIL | LOCAL | CoMat 10-039 | ||
| CoMat 10-040 LUBRICANT (ENGINE OIL) | 0AM53 | CoMat 10-040 | ||
| CoMat 10-057 FILLER | LOCAL | CoMat 10-057 |
Spares
NONESafety Requirements
WARNING
Procedure
Use CoMat 05-139 ABRASIVE CROCUS CLOTH and CoMat 10-039 ENGINE OIL or CoMat 10-040 LUBRICANT (ENGINE OIL), to clean bushings with light scratches and scores. Do not touch the glossy surfaces of the bushings, unless they have scratches or scores.
NOTE
The alternative procedure to remove a bushing is to grind two grooves, 180 degrees apart, in the internal diameter of the bushing; but be very careful not to grind into the housing. If the bushing is carburized, it will be easier to grind when locally heat-treated to approximately 400 deg F (204 deg C) for 15 to 20 minutes; but be very careful not to let the housing become too hot. Then, with a drift or punch and a hammer, break the bushing, into the housing, before it is removed.If the bushings are locked with pins, remove the pins before you remove the bushings. It may be necessary to use a drill to remove a pin. Always use a drill jig, to guide the drill, then only drill to a sufficient depth to release the bushing. The necessary drill jigs are included in the tool data specified for each type of bushing. If a drill jig is not available, carefully drill the pin and use a bushing or lever as a guide. Alternatively, remove the pin with a small drift or punch.
Ream the new bushing to the correct dimension; then polish it with CoMat 05-139 ABRASIVE CROCUS CLOTH and CoMat 10-039 ENGINE OIL or CoMat 10-040 LUBRICANT (ENGINE OIL).
Fill the pin holes with CoMat 10-057 FILLER. Make sure that no air is caught in the filler. Use a pointed or hyperdermic type of tool, to apply the filler, then apply the filler tightly.
NOTE
The pin holes can also be filled with weld. Use a weld wire which is made of the same material as the housing (Refer to the SPM TASK 70-31-03-310-501). Machine away the surface of the weld, to make it level with the surface of the housing.Machine away the unwanted filler, level with the surface of the housing.
When the bushings are replaced frequently, and the housing has become weak because of the many pin holes, the unwanted holes can be filled by the procedure that follows:
SUBTASK 70-46-02-460-001 Bushings and Bearing Liners
