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 72-41-15-300-025 HPC Stage 8 Rotor Blade - Vibro Polish To Restore The Surface Finish, Repair-025 (VRS6070)
Effectivity
FIG/ITEM | PART NUMBER | ASSEMBLY |
|---|---|---|
02-370 | 6A3249 | A |
02-370 | 6A5590 | A |
02-370 | 6A6469 | A |
02-370 | 6A4908 | A |
02-370 | 6A6464 | A |
Deleted | Deleted | Deleted |
02-370 | 6A8747 | B |
02-385 | 6A3250 | A |
02-385 | 6A5591 | A |
02-385 | 6A6497 | A |
Deleted | Deleted | Deleted |
02-385 | 6A4909 | A |
02-385 | 6A6465 | A |
Deleted | Deleted | Deleted |
02-385 | 6A8748 | B |
02-400 | 6A3248C01 | A |
02-400 | 6A5585C01 | A |
02-400 | 6A6495C01 | A |
02-400 | 6A4910C01 | A |
02-400 | 6A6470C01 | A |
Deleted | Deleted | Deleted |
02-400 | 6A8745 | B |
02-415 | 6A3248C01 | A |
02-415 | 6A5585C01 | A |
02-415 | 6A6495C01 | A |
02-415 | 6A4910C01 | A |
02-415 | 6A6470C01 | A |
Deleted | Deleted | Deleted |
02-415 | 6A8745 | B |
02-416 | 6B1496 | B |
02-417 | 6A3248C02 | A |
02-417 | 6A5585C02 | A |
02-417 | 6A6495C02 | A |
02-417 | 6A4910C02 | A |
02-417 | 6A6470C02 | A |
Deleted | Deleted | Deleted |
02-417 | 6A8746 | B |
General
This TASK gives the procedure to restore the surface finish of the HPC Stage 8 Rotor Blade by vibro-polishing.
This repair must only be done when the instruction to do so is given in the relevant inspection procedures (identified by the applicable part number) located in section 72-41-15.
The blades must have been repaired, where necessary and inspected before vibro-polishing.
The HPC Stage 8 Rotor Blades can only have this repair completed on them three times.
Where reference is made to a SUBTASK in a TASK in the form "TASK, SUBTASK" the operator must read and apply the complete TASK. The SUBTASK is listed only when the TASK gives options for the processing of the component. The specified SUBTASK instructs what option must be used during application of the TASK for the successful completion of the Repair Scheme VRS6070.
The practices and processes referred to in the procedure by the TASK/SUBTASK number are in the SPM.
Price and availability
Refer to International Aero Engines.
Related repairs
HPC Blade - Restore Stage 8 Anti-Fret Treatment, refer to Repair, VRS6497 TASK 72-41-15-300-051 (REPAIR-051).
NOTE
NOTE
NOTE
NOTE
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
| Action/Condition | Data Module/Technical Publication |
|---|---|
| Make sure that all cleaning and inspection procedures are done before this repair. | |
| All other repairs must be completed before you apply VRS6070. | |
| Restore the airfoil surface finish before you apply VRS6070. Refer to repair VRS6150 (REPAIR-040). | TASK 72-41-15-300-040 |
Support Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| IAE 3R18552 Mask | 0AM53 | IAE 3R18552 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-093 SUPERFINISHING MEDIA, CERAMIC, ANGLE CUT TRIANGLE | IAE56 | CoMat 05-093 | ||
| CoMat 05-095 LIQUID COMPOUND (VIBROPOLISHING FINISHING FLUID) | IE230 | CoMat 05-095 | ||
| CoMat 05-181 VIBRO POLISHING MEDIA, CERAMIC PIN | LOCAL | CoMat 05-181 | ||
| CoMat 05-182 VIBRO POLISHING COMPOUND, LIQUID | IAE56 | CoMat 05-182 | ||
| CoMat 05-183 VIBRO POLISHING PASTE | IAE56 | CoMat 05-183 |
Spares
NONESafety Requirements
NONEProcedure
Reject.
If the repair identification symbol and a /2 suffix are engraved adjacent to the part number.
Continue with the repair.
If there is no repair identification symbol or if the repair identification symbol is engraved with a /1 suffix or with no suffix adjacent to the part number.
Examine the component for the repair identification symbol, a 1 in a triangle, and any suffixes.
Examine the HPC Stage 8 Rotor Blade to find, if VRS6070 was done before.
SUBTASK 72-41-15-220-179 Make sure that the Component(s) can be Vibro Polished
Apply a mask or maskants to the blade tip, if required. Make sure that the mask or maskants completely covers the aluminum oxide coat on the blade tip and the airfoil surfaces.
Refer to SPM TASK 70-38-25-380-501 and/or use IAE 3R18552 Mask.
Apply a mask or maskants to the HPC Stage 8 Rotor Blade.
SUBTASK 72-41-15-350-075 Apply the Mask to the Component
Refer to Figure.
Refer to SPM TASK 70-38-25-380-501.
The surface finish is to be 16 microinches (0.40 micrometers) maximum on a minimum of 70 percent of the surface area.
On the remainder of the blade, the surface finish is to be between 16 microinches (0.40 micrometers) and 32 microinches (0.80 micrometers).
Do not have more than 50 blades for one cubic foot of the vibro-polishing media.
Option 3: Method Two consumables.
Use one of the following options to get the surface finish limits. The dimension of the superfinishing media is to be 10 mm x 10 mm maximum.
Polish the surfaces in the area specified AB.
Vibro-polish the HPC Stage 8 Rotor Blade airfoil and adjacent annulus surfaces.
SUBTASK 72-41-15-380-069-A00 Vibro-Polish the Component(s), Assembly A
Refer to Figure.
Refer to SPM TASK 70-38-25-380-501.
A maximum of 10 microinches (0.25 micrometers) surface finish is permitted on blade airfoil surfaces.
On the remainder of the blade, the maximum surface finish is to be 16 microinches (0.40 micrometers).
Do not have more than 50 blades for one cubic foot of the vibro-polishing media.
Option 3: Method Two consumables.
Use one of the following options to get the surface finish limits. The dimension of the superfinishing media is to be 10 mm x 10 mm maximum.
Polish the surfaces in the area specified AB.
Vibro-polish the HPC Stage 8 Rotor Blade airfoil and adjacent annulus surfaces.
SUBTASK 72-41-15-380-069-B00 Vibro-Polish the Component(s), Assembly B
Remove the mask or maskants from the HPC Stage 8 Rotor Blade.
SUBTASK 72-41-15-350-142 Remove the Mask
Refer to SPM TASK 70-11-03-300-503.
Clean the HPC Stage 8 Rotor Blade by aqueous degreasing.
SUBTASK 72-41-15-110-202 Clean by Aqueous Degreasing
Refer to Figure.
Refer to SPM TASK 70-38-25-380-501.
The surface finish must obey the limits of Step.
Record each application of vibro-polishing during procedure of VRS6070.
Repair can be applied again, only if the repair identification symbol suffix number will not be more than /2 after the initial application. Each application must be recorded.
If the surface finish is not in the specified limits, do the repair from Step again.
If the surface finish is in the specified limits, continue with the repair.
Examine the surface finish on the each side of the airfoil and the adjacent surfaces in the area specified AB.
Inspect the surface finish of the HPC Stage 8 Rotor Blade.
SUBTASK 72-41-15-220-180-A00 Inspect the Surface Finish of the Vibro-Polished Component, Assembly A
Refer to Figure.
Refer to SPM TASK 70-38-25-380-501.
The surface finish must obey the limits of Step.
Record each application of vibro-polishing during procedure of VRS6070.
Repair can be applied again, only if the repair identification symbol suffix number will not be more than /2 after the initial application. Each application must be recorded.
If the surface finish is not in the specified limits, do the repair from Step again.
If the surface finish is in the specified limits, continue with the repair.
Examine the surface finish on the each side of the airfoil and the adjacent surfaces in the area specified AB.
Inspect the surface finish of the HPC Stage 8 Rotor Blade.
SUBTASK 72-41-15-220-180-B00 lnspect the Surface Finish of the Vibro-Polished Component, Assembly B
Refer to SPM TASK 70-09-00-400-501.
If the blade is already identified with the repair identification symbol, only the suffix number is to be updated.
If this is the first application of VRS6070, mark the repair identification symbol, a 1 in a triangle, on the indicated surface adjacent to the part number.
If this is the second application of VRS6070, mark /1 adjacent to the repair identification symbol.
If this is the third application of VRS6070, mark /2 adjacent to the repair identification symbol.
Mark the repair identification symbol and the applicable suffix numbers at the indicated location on the HPC Stage 8 Rotor Blade, use vibration peen method.
SUBTASK 72-41-15-350-076 Identify the Repair
Refer to Repair, VRS6497 TASK 72-41-15-300-051 (REPAIR-051).
Apply the dry film lubricant to the dovetail root of the HPC Stage 8 Rotor Blade for the applicable part numbers.
SUBTASK 72-41-15-380-138 Apply the Dry Film Lubricant
Figure: HPC Stage 8 Rotor Blade - Repair Details And Dimensions - Assembly A
HPC Stage 8 Rotor Blade - Repair Details And Dimensions - Assembly A

Figure: HPC Stage 8 Rotor Blade - Repair Details And Dimensions - Assembly B
HPC Stage 8 Rotor Blade - Repair Details And Dimensions - Assembly B

