DMC:V2500-A0-72-50-4101-00A-655A-CIssue No:002.00Issue Date:2013-11-01
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 72-50-41-300-019 LPT Shaft - Repair The Front Face Of Balance Land - Repair-019 (VRS1501)
General
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
Material of component
DESCRIPTION | SYMBOL | MATERIAL |
|---|---|---|
LP turbine shaft | Non-corrosion resistant steel |
Price and availability - none
NOTE
To identify the consumable materials refer to the PCI.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Standard workshop equipment | LOCAL | Standard workshop equipment | ||
| Grinding machine | LOCAL | Grinding machine | ||
| Magnetic particle inspection equipment | LOCAL | Magnetic particle inspection equipment | ||
| Vibro-engraving equipment | LOCAL | Vibro-engraving equipment |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-019 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-019 | ||
| CoMat 05-020 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-020 |
Spares
NONESafety Requirements
CAUTION
WHEN THE LPT MODULE IS INSTALLED, THICKNESS OF ADJUSTING RING MUST BE CALCULATED USING THE NEW DIMENSION J IF THIS REPAIR IS DONE. DO NOT REINSTALL THE REMOVED ADJUSTING RING.
CAUTION
THIS REPAIR CAN BE DONE ONE TIME ONLY.
Procedure
Refer to Figure.
SUBTASK 72-50-41-210-001 Do a Check of the Repair Marking on the LP Turbine Shaft
Refer to Figure.
Refer to the SPM TASK 70-35-03-300-501.
Remove burrs and break sharp edges.
SUBTASK 72-50-41-324-001 Grind the Front Face of Balance Land of the LP Turbine Shaft
Refer to Figure.
Visually examine the repaired area for galls, nicks, dents, pits, scratches and/or burrs using 10X magnifying glass.
Refer to TASK 72-50-41-200-000 (INSPECTION/CHECK-000).
Visually and dimensionally examine the ground area.
SUBTASK 72-50-41-220-113 Visually and Dimensionally Examine the Ground Area
Refer to the SPM TASK 70-24-01-240-501. No cracks are permitted.
Magnetic particle examine the repaired area.
SUBTASK 72-50-41-240-070 Examine the LP Turbine Shaft for Cracks
Refer to Figure.
SUBTASK 72-50-41-220-114 Measure the Dimension J
Figure: Repair Details and Dimensions
Repair Details and Dimensions

