TASK 72-41-15-300-024 HPC Stage 7 Rotor Blade - Vibro Polish To Restore The Surface Finish, Repair-024 (VRS6069)

DMC:V2500-A0-72-41-1507-00A-648A-C|Issue No:003.00|Issue Date:2021-05-01

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 72-41-15-300-024 HPC Stage 7 Rotor Blade - Vibro Polish To Restore The Surface Finish, Repair-024 (VRS6069)

Effectivity

FIG/ITEM

PART NO.

ASSEMBLY

02-270

6A3246

A

Deleted

Deleted

Deleted

02-270

6A4905

A

02-270

6A5588

A

02-270

6A6462

A

02-270

6A6493

A

Deleted

Deleted

Deleted

02-270

6A8314

A

02-270

6A8743

B

02-285

6A3247

A

02-285

6A4906

A

02-285

6A5589

A

02-285

6A6463

A

02-285

6A6494

A

Deleted

Deleted

Deleted

02-285

6A8315

A

02-285

6A8744

B

02-300

6A3245C01

A

02-300

6A4907C01

A

02-300

6A5584C01

A

02-300

6A6469C01

A

02-300

6A6492C01

A

Deleted

Deleted

Deleted

02-300

6A8312

A

02-300

6A8741

B

02-315

6A3245C01

A

02-315

6A4907C01

A

02-315

6A5584C01

A

02-315

6A6469C01

A

02-315

6A6492C01

A

Deleted

Deleted

Deleted

02-315

6A8312

A

02-315

6A8741

B

02-316

6B1495

B

02-317

6A3245C02

A

02-317

6A4907C02

A

02-317

6A5584C02

A

02-317

6A6469C02

A

02-317

6A6492C02

A

Deleted

Deleted

Deleted

02-317

6A8313

A

02-317

6A8742

B

Material of component

PART IDENT

RR SYMBOL

MATERIAL

HPC - Stage 7 Rotor Blade

TDY or TTX

Titanium alloy

General

This TASK gives the procedure to restore the surface finish of the HPC Stage 7 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 HPC Stage 7 Rotor Blades can only have this repair completed on them three times.

The blades must have been repaired, where necessary and inspected before vibro-polishing.

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 VRS6069.

The practices and processes referred to in the procedure by the TASK/SUBTASK numbers are in the SPM.

Price and Availability

Refer to International Aero Engines.

Related Repairs

HPC Blade - Restore Stage 7 Anti-Fret Treatment, refer to Repair, VRS6496 TASK 72-41-15-300-050 (REPAIR-050).

NOTE

Equipment and materials necessary to do this repair are given in the SPM TASKS given below:

NOTE

It is possible that some materials in the consumable materials chart cannot be used for some or all of the necessary applications. Before you use the materials, make sure the types, quantities and applications of the materials necessary are legally permitted in your location. All persons must obey all applicable federal, state, local and provincial laws and regulations when it is necessary to work with these materials.

NOTE

To identify the consumable materials refer to the Process Consumable Materials Index (PCI).

NOTE

Other necessary consumable materials are referred to in the SPM TASKS in this TASK.

NOTE

Special tools are identified in the procedure by the tool primary number.

Preliminary Requirements

Pre-Conditions

Action/ConditionData 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 VRS6069.
Restore the airfoil surface finish before you apply VRS6069. Refer to repair VRS6150 (REPAIR-040).TASK 72-41-15-300-040

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
IAE 3R18551 Mask0AM53IAE 3R185511

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 05-093 SUPERFINISHING MEDIA, CERAMIC, ANGLE CUT TRIANGLE IAE56CoMat 05-093
CoMat 05-095 LIQUID COMPOUND (VIBROPOLISHING FINISHING FLUID)IE230CoMat 05-095
CoMat 05-181 VIBRO POLISHING MEDIA, CERAMIC PINLOCALCoMat 05-181
CoMat 05-182 VIBRO POLISHING COMPOUND, LIQUIDIAE56CoMat 05-182
CoMat 05-183 VIBRO POLISHING PASTEIAE56CoMat 05-183

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-41-15-220-177 Make sure that the Component(s) can be Vibro Polished

    2. Refer to Figure for Assembly A and Figure for Assembly B.

      1. Examine the HPC Stage 7 Rotor Blade to find, if VRS6069 was done before.

        1. Examine the component for the repair identification symbol, a 1 in a triangle, and any suffixes.

          1. If the repair identification symbol and a /2 suffix are engraved adjacent to the part number.

          2. Reject.

          1. 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.

          2. Continue with the repair.

    1. SUBTASK 72-41-15-350-073 Apply the Mask to the Component

    2. Refer to Figure for Assembly A and Figure for Assembly B.

      1. Apply a mask or maskants to the HPC Stage 7 Rotor Blade.

      2. Apply a mask or maskants to the blade root. Make sure that the minimum area of the HPC Stage 7 Rotor Blade gas washed surface is covered by the mask or maskants.

      3. Apply a mask or maskants to the blade tip, if required. Make sure that the mask or maskants completely covers the aluminum oxide coating on the blade tip and the airfoil surfaces.

      4. Refer to SPM TASK 70-38-25-380-501 and/or use IAE 3R18551 Mask.

    1. SUBTASK 72-41-15-380-068-A00 Vibro-Polish the Component(s), Assembly A

    2. Refer to Figure.

      1. Vibro-polish the HPC Stage 7 Rotor Blade airfoil and adjacent annulus surfaces.

      2. Refer to SPM TASK 70-38-25-380-501.

        1. Polish the surfaces in the area specified AB.

        2. The surface finish is to be 16 microinches (0.40 micrometers) maximum on a minimum of 70 percent of the surface area.

        3. On the remainder of the blade, the surface finish is to be between 16 microinches (0.40 micrometers) and 32 microinches (0.80 micrometers).

        4. Do not have more than 40 blades for one cubic foot of the vibro-polishing media.

          1. 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.

          2. Option 3: Method Two consumables.

    1. SUBTASK 72-41-15-380-068-B00 Vibro-Polish the Component(s), Assembly B

    2. Refer to Figure.

      1. Vibro-polish the HPC Stage 7 Rotor Blade airfoil and adjacent annulus surfaces.

      2. Refer to SPM TASK 70-38-25-380-501.

        1. Polish the surfaces in the area specified AB.

        2. A maximum of 10 microinches (0.25 micrometers) surface finish is permitted on blade airfoil surfaces.

        3. On the remainder of the blade, the maximum surface finish is to be 16 microinches (0.40 micrometers).

        4. Do not have more than 40 blades for one cubic foot of the vibro-polishing media.

          1. 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.

          2. Option 3: Method Two consumables.

    1. SUBTASK 72-41-15-350-132 Remove the Mask

    2. Remove the mask or maskants from the HPC Stage 7 Rotor Blade.

    1. SUBTASK 72-41-15-110-187 Clean by Aqueous Degreasing

      1. Clean the HPC Stage 7 Rotor Blade by aqueous degreasing.

      2. Refer to SPM TASK 70-11-03-300-503.

    1. SUBTASK 72-41-15-220-178-A00 Inspect the Surface Finish of the Vibro-Polished Component, Assembly A

    2. Refer to Figure.

      1. Inspect the surface finish of the HPC Stage 7 Rotor Blade.

      2. Refer to SPM TASK 70-38-25-380-501.

        1. Examine the surface finish on the each side of the airfoil and the adjacent surfaces in the area specified AB.

        2. The surface finish must obey the limits of Step.

          1. If the surface finish is not in the specified limits, do the repair from Step again.

          2. Record each application of vibro-polishing during procedure of VRS6069.

          3. 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.

        3. If the surface finish is in the specified limits, continue with the repair.

    1. SUBTASK 72-41-15-220-178-B00 Inspect the Surface Finish of the Vibro-Polished Component, Assembly B

    2. Refer to Figure.

      1. Inspect the surface finish of the HPC Stage 7 Rotor Blade.

      2. Refer to SPM TASK 70-38-25-380-501.

        1. Examine the surface finish on the each side of the airfoil and the adjacent surfaces in the area specified AB.

        2. The surface finish must obey the limits of Step.

          1. If the surface finish is not in the specified limits, do the repair from Step again.

          2. Record each application of vibro-polishing during procedure of VRS6069.

          3. 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.

        3. If the surface finish is in the specified limits, continue with the repair.

    1. SUBTASK 72-41-15-350-074 Identify the Repair

    2. Refer to Figure for Assembly A and Figure for Assembly B.

      1. Mark the repair identification symbol and the applicable suffix numbers at the indicated location on the HPC Stage 7 Rotor Blade, use vibration peen method.

      2. Refer to SPM TASK 70-09-00-400-501.

        1. If this is the first application of VRS6069, mark the repair identification symbol, a 1 in a triangle, on the indicated surface adjacent to the part number.

        2. If the blade is already identified with the repair identification symbol, only the suffix number is to be updated.

      3. If this is the second application of VRS6069, mark /1 adjacent to the repair identification symbol.

      4. If this is the third application of VRS6069, mark /2 adjacent to the repair identification symbol.

      5. Record each application of vibro-polishing during procedure of VRS6069. The process can be applied again, only if the inspection is in agreement with Step or Step, then this must be counted as an additional application of VRS6069 and the applicable suffix number must be updated.

    1. SUBTASK 72-41-15-380-137 Apply the Dry Film Lubricant

      1. Apply the dry film lubricant to the dovetail root of the HPC Stage 7 Rotor Blade for the applicable part numbers.

      2. Refer to Repair, VRS6496 TASK 72-41-15-300-050 (REPAIR-050).

  1. Figure: Repair Details And Dimensions - Assembly A

    Repair Details And Dimensions - Assembly A

    Figure: Repair Details And Dimensions - Assembly B

    Repair Details And Dimensions - Assembly B

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the procedure in its entirety. (19VG261)

Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:IAE56
Enterprise Name:DELETED. REFER TO VENDOR CODE V056V.
Manufacturer Code:IE230
Enterprise Name:DELETED. REFER TO VENDOR CODE FAJU6.
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:CK340
Supply Number:CoMat 05-093
Type:sp01
Supply Short Name:CoMat 05-093 SUPERFINISHING MEDIA, CERAMIC, ANGLE CUT TRIANGLE
Supply Name:CoMat 05-093 SUPERFINISHING MEDIA, CERAMIC, ANGLE CUT TRIANGLE
Specification Groups:
Doc NumberType
ROSLER RM S ANGLE CUT TRIANGLE
Suppliers:
ManufacturerRemarks
CK340
K6835
V056V
Manufacturer Code:DL610
Supply Number:CoMat 05-095
Type:sp01
Supply Short Name:CoMat 05-095 LIQUID COMPOUND (VIBROPOLISHING FINISHING FLUID)
Supply Name:CoMat 05-095 LIQUID COMPOUND (VIBROPOLISHING FINISHING FLUID)
Specification Groups:
Doc NumberType
ARF
Suppliers:
ManufacturerRemarks
DL610
FAJU6
K6835
V140V
V563V
Manufacturer Code:X222X
Supply Number:CoMat 05-181
Type:sp01
Supply Short Name:CoMat 05-181 VIBRO POLISHING MEDIA, CERAMIC PIN
Supply Name:CoMat 05-181 VIBRO POLISHING MEDIA, CERAMIC PIN
Specification Groups:
Doc NumberType
Where CoMat 05-181 is specified with no letter suffix, use CoMat 05-181A or CoMat 05-181B
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:K6835
Supply Number:CoMat 05-182
Type:sp01
Supply Short Name:CoMat 05-182 VIBRO POLISHING COMPOUND, LIQUID
Supply Name:CoMat 05-182 VIBRO POLISHING COMPOUND, LIQUID
Specification Groups:
Doc NumberType
Rosler FC 120
Suppliers:
ManufacturerRemarks
K6835
V056V
Manufacturer Code:K6835
Supply Number:CoMat 05-183
Type:sp01
Supply Short Name:CoMat 05-183 VIBRO POLISHING PASTE
Supply Name:CoMat 05-183 VIBRO POLISHING PASTE
Specification Groups:
Doc NumberType
SVRB 1
Suppliers:
ManufacturerRemarks
K6835
V056V
Manufacturer Code:0AM53
Tool Number:IAE 3R18551
Tool Name:IAE 3R18551 Mask