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 72-50-41-300-006 LPT Shaft - Apply Nickel Plating, Repair-006 (VRS1496)
General
Price and availability - none
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Grinding machine | LOCAL | Grinding machine | ||
| Nickel plate equipment | LOCAL | Nickel plate equipment | ||
| Magnetic particle inspection equipment | LOCAL | Magnetic particle inspection equipment | ||
| Vibrating marking pencil | LOCAL | Vibrating marking pencil |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-050 SULFURIC ACID H2SO4 | LOCAL | CoMat 01-050 | ||
| CoMat 01-081 ELECTROPLATING SOLUTION | LOCAL | CoMat 01-081 |
Spares
NONESafety Requirements
NONEProcedure
Refer to the SPM TASK 70-11-03-300-503.
Clean the part.
SUBTASK 72-50-41-350-059 Clean the LP Turbine Shaft
Refer to: Figure
SUBTASK 72-50-41-330-052 Machine Worn Diameter D1
NOTE
If surface has been previously repaired using nickel plate, remove old plating completely.Refer to the SPM TASK 70-33-05-300-503.
Heat treat the part for one hour at 374 to 410 deg F (190 to 210 deg C).
SUBTASK 72-50-41-370-051 Stress Relieve the LP Turbine Shaft
Refer to the SPM TASK 70-11-03-300-503.
Clean the part.
SUBTASK 72-50-41-240-058 Examine the LP Turbine Shaft for Cracks
Refer to the SPM TASK 70-33-05-300-503.
Wire-up the part.
Refer to the SPM TASK 70-11-03-300-503.
Clean the part.
Refer to the SPM TASK 70-33-05-300-503.
Apply stopping-off compound to areas to be left unplated.
SUBTASK 72-50-41-330-053 Prepare the LP Turbine Shaft for Plating
Refer to the SPM TASK 70-33-05-300-503.
Immediately after etch and washing, nickel chloride strike the part.
Refer to the SPM TASK 70-33-05-300-503.
Wash the part in water.
SUBTASK 72-50-41-330-054 Nickel Chloride Strike the LP Turbine Shaft
Refer to the SPM TASK 70-33-05-300-503.
Give a de-embrittlement treatment as soon as possible after plating. Heat treat the part at 374 to 410 deg F (190 to 210 deg C) for 3 hours.
SUBTASK 72-50-41-370-052 De-Embrittle the LP Turbine Shaft
Refer to: Figure
SUBTASK 72-50-41-220-084 Examine the LP Turbine Shaft after Plating
Refer to: Figure
Refer to the SPM TASK 70-33-05-300-503.
Grind the plated area by normal grinding wheel to specified dimensions.
SUBTASK 72-50-41-320-051 Grind the LP Turbine Shaft after Plating
Refer to: Figure
SUBTASK 72-50-41-230-054 Examine the LP Turbine Shaft after Grinding
Figure: Apply nickel plating - LP Turbine Shaft
Apply nickel plating - LP Turbine Shaft

