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 75-31-42-300-007 LPC Bleed Master Actuator - Related Parts - Replace The LPC Bleed Master Actuator Bracket Assembly Thin Wall Insert(s), Flanged/Plain Location Dowels, Repair-007 (VRS6667)
Material of components
PART IDENT | SYMBOL | MATERIAL |
LP compressor, bleed master actuator bracket assembly | EEJ or | Corrosion resistant steel |
ENH | Chrome cobalt molybdenum electro flux remelted steel |
General
This Repair must only be done when the instruction to do so is given in Inspection-004 TASK 75-31-42-200-404.
This repair is to replace the thin wall insert(s), when they are broken, worn, cross-threaded or missing, also flanged location dowel when damaged or missing and/or plain dowel when damaged or missing.
Price and availability.
Refer to International Aero Engines.
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Standard Workshop Equipment | LOCAL | Standard Workshop Equipment | ||
| Heat protection gloves | LOCAL | Heat protection gloves |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 03-026 LIQUID NITROGEN | LOCAL | CoMat 03-026 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Remove damaged thin wall insert(s) and discard. Refer to SPM TASK 70-35-26-300-501, SUBTASK 70-35-26-350-001.
SUBTASK 75-31-42-350-061 Remove the Damaged Thin Wall Insert(s), Assembly A
Refer to Figure.
Remove damaged flanged location dowel(s) and discard.
Remove sharp edges around location hole(s).
Use a soft clean cloth and blast with air.
Clean the holes.
SUBTASK 75-31-42-350-062 Remove the Damaged Flanged Location Dowel(s), Assembly A
Refer to Figure.
Remove damaged plain dowel(s) and discard.
Remove sharp edges around location hole(s).
Use a soft clean cloth and blast with air.
Clean the holes.
SUBTASK 75-31-42-350-063 Remove the Damaged Plain Dowel(s), Assembly A
Refer to Figure.
Visually examine dowel location holes.
Make sure you can get an interference fit of 0.00008 inches to 0.00126 inches (0.002 mm to 0.032 mm) on the hole diameter.
Measure dimensions of the dowel location holes.
SUBTASK 75-31-42-220-076 Examine the Dowel Holes, Assembly A
Refer to Figure.
Use AS52761 insert, as necessary.
Install replacement thin wall insert(s). Refer to SPM TASK 70-35-26-300-501, SUBTASK 70-35-26-350-001.
SUBTASK 75-31-42-350-064 Install the Replacement Thin Wall Insert(s), Assembly A
Refer to Figure.
Use AS44806 flanged location dowel.
Ensure dowel(s) are pushed down hard.
Freeze and install replacement flanged location dowel(s).
SUBTASK 75-31-42-350-065 Install the Replacement Flanged Location Dowel(s), Assembly A
Refer to Figure.
Use AS20655 plain dowel, as necessary.
Ensure dowel(s) are pushed down hard.
Freeze and install replacement plain dowel(s).
SUBTASK 75-31-42-350-066 Install the Replacement Plain Dowel(s), Assembly A
Refer to Figure.
Examine thin wall insert(s). Refer to SPM TASK 70-35-26-300-501, SUBTASK 70-35-26-350-001.
SUBTASK 75-31-42-220-077 Examine the Thin Wall Insert(s), Assembly A
Refer to Figure.
Ensure dowel(s) have been pushed down hard.
Examine flanged location dowel(s).
SUBTASK 75-31-42-220-078 Examine the Flanged Location Dowel(s), Assembly A
Refer to Figure.
Ensure dowel(s) have been pushed down hard and do not protrude more than 0.236 inches (6.00 mm).
Examine plain dowel(s).
SUBTASK 75-31-42-220-079 Examine the Plain Dowel(s), Assembly A
Figure: Repair Details and Dimensions
Repair Details and Dimensions

