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 72-32-23-300-006 HPC Front Shaft Assembly - Replace Damaged/Loose Location Bolt(s), Repair-006 (VRS6267)
Material of component
PART IDENT | SYMBOL | MATERIAL |
|---|---|---|
HP Compressor Front Stubshaft | TEG | Titanium aluminium vanadium alloy |
General
This Repair must only be done when the instruction to do so is given in TASK 72-32-23-200-000 (INSPECTION-000).
This Repair replaces damaged/worn location bolt(s) in the HP Compressor Front Stubshaft.
You must use new location bolt(s), cup washer(s) and nut(s).
The practices and processes referred to in the procedure by the TASK/SUBTASK numbers are in the SPM
Price and availability - none
Related repairs - none
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Standard workshop equipment | LOCAL | Standard workshop equipment | ||
| Chemical cleaning equipment | LOCAL | Chemical cleaning equipment | ||
| Penetrant Crack Test Equipment | LOCAL | Penetrant crack test equipment | ||
| Torque tightening equipment | LOCAL | Torque tightening equipment | ||
| Workshop inspection equipment | LOCAL | Workshop inspection equipment | ||
| Vibrating marking pencil | LOCAL | Vibrating marking pencil |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY) | LOCAL | CoMat 06-022 |
Spares
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Nut 0.250in Dia | 4W0002 | 4 A/R | ||
| Washer, Cup | UP11050 | 4 A/R | ||
| Bolt, Locating | UP10762 | 4 A/R |
Safety Requirements
NONEProcedure
Refer to the SPM TASK 70-11-26-300-503 SUBTASK 70-11-26-300-002.
Chemically clean the location hole (s).
SUBTASK 72-32-23-110-085 Chemically Clean the Location Hole(s) in the HPC Front Stubshaft
Refer to the SPM TASK 70-23-05-230-501.
Cracks are not permitted.
Do a local penetrant crack test.
SUBTASK 72-32-23-230-077 Do a Penetrant Crack Test of the Location Hole(s)
Refer to the SPM TASK 70-11-26-300-503 SUBTASK 70-11-26-300-002.
Chemically clean the location hole(s).
SUBTASK 72-32-23-110-086 Chemically Clean the Location Hole(s) in the HPC Front Stubshaft
Refer to the SPM TASK 70-41-00-400-501 and SPM TASK 70-41-01-400-501. Torque tighten the location bolt(s) and nut(s) to a value of 85 to 105 1bf.in (10 to 12 Nm).
Use a light application of engine oil, refer to the SPM TASK 70-41-00-400-501 and SPM TASK 70-41-01-400-501.
Torque tighten the location bolt(s) and nut(s) in place.
Refer to the SPM TASK 70-42-04-400-501.
Crimp the washer.
SUBTASK 72-32-23-350-003 Torque Tighten the Location Bolts(s) and Nut(s)
Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-501.
Make a mark VRS6267 adjacent to the part number.
SUBTASK 72-32-23-350-004 Identify the Repair
Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

