DMC:V2500-A0-72-50-5301-01A-647A-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 72-50-53-300-029 Turbine Exhaust Case (TEC) - Replace The Damaged Self Locking Shank Nut On The Inner Rear Flange, Repair-029 (VRS5413)
Material of component
RR | ||
|---|---|---|
DESCRIPTION | SYMBOL | MATERIAL |
Turbine exhaust case | - | Corrosion and heat |
resistant iron base alloy |
General
Price and availability - none
The practices and processes referred to in the procedure by the TASK numbers are in the SPM
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Peening tool | LOCAL | Peening tool | (0.250 in.) |
Consumables, Materials and Expendables
NONESpares
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Self locking shank nut | AS27857 | 13 |
Safety Requirements
NONEProcedure
Refer to: Figure
SUBTASK 72-50-53-350-070 Remove the Damaged Self Locking Shank Nut
Refer to: Figure
SUBTASK 72-50-53-350-071 Install the New Self Locking Shank Nut
Figure: Repair Details and Dimensions
Repair Details and Dimensions

