TASK 72-32-82-300-011 LPC Stage 2.5 Blade - Blend Repair, Repair-011 (VRS1863)

DMC:V2500-A0-72-32-8225-01A-649A-C|Issue No:003.00|Issue Date:2017-02-01

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 72-32-82-300-011 LPC Stage 2.5 Blade - Blend Repair, Repair-011 (VRS1863)

Effectivity

FIG/ITEM

PART NO.

02-100

5R0180

General

This TASK gives the instruction to remove damage on the LP Compressor Rotor Blade(s), stage 2.5 by material removal.

Material of Components

IAE

DESCRIPTION

SYMBOL

MATERIAL

LPC stage 2.5 blade

Titanium alloy

Price and Availability - refer to IAE

The practice and processes referred to in the procedure by the TASK numbers are in the SPM.

NOTE

Equivalent materials or equipment can be used.

NOTE

To identify the consumable materials refer to the PCI.

NOTE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Fluorescent Penetrant Inspection EquipmentLOCALFluorescent penetrant inspection equipment
Glass bead peening equipmentLOCALGlass bead peening equipment
Shot peening equipmentLOCALShot peening equipment
IAE 3J13165 Shot peening fixture0AM53IAE 3J131651
IAE 3J13166 Glass peening fixture0AM53IAE 3J131661
IAE 3J13168 Glass peening fixture0AM53IAE 3J131681

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-293 GLASS BEADSLOCALCoMat 01-293
CoMat 02-003 ADHESIVE TAPE BLACK WATERPROOFLOCALCoMat 02-003
CoMat 05-006 GLASS BEADS0AM53CoMat 05-006
CoMat 05-019 WATERPROOF SILICON CARBIDELOCALCoMat 05-019
CoMat 05-020 WATERPROOF SILICON CARBIDELOCALCoMat 05-020
CoMat 05-021 WATERPROOF SILICON CARBIDE44197CoMat 05-021
CoMat 05-030 CAST STEEL SHOT DELETED0AM53CoMat 05-030
CoMat 05-162 GLASS BEADSLOCALCoMat 05-162

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-82-350-078 Remove the Damage from the LPC Stage 2.5 Blades

      1. CAUTION

        WHEELS, STONES AND ABRASIVE PAPERS USED TO DRESS, MAKE SMOOTH, OR POLISH A TITANIUM COMPONENT MUST BE OF THE SILICON CARBIDE TYPE. ALUMINUM OXIDE TYPE MUST NOT BE USED.
        THE MATERIAL WILL OXIDIZE AND CRACK IF MECHANICAL CUTTERS ARE USED HEAVILY. THIS HAS OCCURRED IF COMPONENT SHOWS DARK STRAW TO BLUE DISCOLORATION. IF AT ANYTIME THIS COLORATION OCCURS. THE COMPONENT MUST BE REJECTED.

        Scallop, make smooth and/or hand polish to remove nicks, scratches and/or damage.

      1. Use abrasive stone or papers and/or fine file. Use light pressure to prevent any risk of overheating material.

      2. Any polish marks must be made in a radial direction from root to tip of the blades.

      3. Surface finish of the repair area must be the same as the adjacent area.

      2. Hand polish the blade leading and/or trailing edge radius and the blade profile to make a smooth shape.

      1. Use CoMat 05-019 WATERPROOF SILICON CARBIDE, CoMat 05-020 WATERPROOF SILICON CARBIDE and CoMat 05-021 WATERPROOF SILICON CARBIDE. Remove the minimum amount of material necessary to give correct radius.

      2. Refer to SPM TASK 70-35-03-300-501.

      3. Refer to Figure.

    2. SUBTASK 72-32-82-220-097 Examine the LPC Stage 2.5 Blades

      1. Do a visual and dimensional examination on the blades.

      1. Visually examine the repaired area for nicks, scratches and/or damage using 10X magnifying glass.

      2. Follow the inspection procedure as given in TASK 72-32-82-200-000.

    3. SUBTASK 72-32-82-230-063 Examine the LPC Stage 2.5 Blade for Cracks

      1. Fluorescent penetrant examine the repaired area.

      1. Refer to SPM TASK 70-23-01-230-501.

      2. Cracks are not permitted.

    4. SUBTASK 72-32-82-350-079 Glass Bead Peen the LPC Stage 2.5 Blades

    1. NOTE

      This is an optional procedure. Do this SUBTASK if necessary after blending to remove the damage from locations 1, 2 and 3, refer to Figure.

      Glass bead peen if the airfoil has been repaired.

      2. Apply the adhesive tape.

      1. Apply CoMat 02-003 ADHESIVE TAPE BLACK WATERPROOF to the areas which are not to be given glass peening.

      2. Refer to Figure.

      3. Install the blades in to the glass peening fixture.

      4. Glass bead peen the airfoil.

      1. Refer to Figure.

      2. Use 0.003 to 0.012 in. (0.08 to 0.30 mm) diameter CoMat 05-006 GLASS BEADS or CoMat 05-162 GLASS BEADS or 0.0098 to 0.0165 in. (0.25 to 0.41 mm) diameter CoMat 01-293 GLASS BEADS an intensity of 10N-13N.

      3. Use IAE 3J13168 Glass peening fixture 1 off hold an Almen test-strip.

      4. Refer to SPM TASK 70-38-04-300-503.

    5. Remove the blades from the fixture and remove the masking tape.

      6. Remove the glass beads.

      1. Use a clean dry air blast or a soft brush.

      2. Use a vacuum assisted brush to make sure all the glass beads are removed.

      7. Examine the blades.

      1. Visually examine the peened surface for uniform coverage and complete over-lapping of the shot impressions.

      2. Refer to SPM TASK 70-38-04-300-503.

    5. SUBTASK 72-32-82-380-060 Shot peen the LPC Stage 2.5 Blades

    1. NOTE

      This is an optional procedure. Do this SUBTASK if necessary after blending to remove the damage from locations 4, 5, 6, 9 and 10, refer to Figure.

      Shot peen if the areas below the platform of the airfoil have been repaired.

      2. Apply the adhesive tape.

      1. Apply the adhesive tape to the area which are not to be given shot peening.

      2. Refer to Figure.

      3. Install the blades in to the shot peening fixture.

      4. Shot peen the repaired area of the blade shank.

      1. Refer to Figure.

      2. Use SAE No.110 steel shot at an intensity of 6A-8A.

      3. Refer to SPM TASK 70-38-04-300-503.

    5. Remove the blade from the fixture and remove the adhesive tape.

      6. Remove the steel shots.

      1. Use a clean dry air blast or a soft brush.

      2. Use a vacuum assisted brush to make sure all the steel shots are removed.

      7. Examine the blades.

      1. Visually examine the peened surface for uniform coverage and complete over-lapping of the shot impressions.

      2. Refer to SPM TASK 70-38-04-300-503.

    6. SUBTASK 72-32-82-220-127 Examine the Repaired Blades

      1. Examine the repaired area.

      1. Make sure that the repair is satisfactory and that it agrees with the repair instructions.

    7. Figure: LP Compressor Stage 2.5 Blades, Dressing Dimensions

    Sheet 1

    Legend
    LP compressor stage 2.5 blades, dressing dimensions

    Sheet 1

    Close

    Figure: LP Compressor Stage 2.5 Blades, Dressing Dimensions

    Sheet 2

    Legend
    LP compressor stage 2.5 blades, dressing dimensions

    Sheet 2

    Close

    Figure: LP Compressor Stage 2.5 Blades, Dressing Dimensions

    Sheet 3

    Legend
    LP compressor stage 2.5 blades, dressing dimensions

    Sheet 3

    Close

    Figure: LPC Stage 2.5 Blades - Glass Bead Peening Area

    LPC Stage 2.5 Blades - Glass Bead Peening Area

    Figure: LPC Stage 2.5 Blades - Shot Peening Area

    LPC Stage 2.5 Blades - Shot Peening Area

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised figure 1 and figure 2. (92VJ827C)

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:44197
Enterprise Name:SAINT-GOBAIN INDUSTRIAL CERAMICS INC.
BU Name:SAINT-GOBAIN ABRASIVES, INC
Street:ONE NEW BOND STREET
P.O. Box:PO BOX 15008
City:WORCESTER
State:MA
Zip Code:01615-0008
Country:USA
Phone Number:1-508-795-5000
Fax Number:1-508-795-2828
Internet:www.saint-gobain-northamerica.com
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 01-293
Type:sp01
Supply Short Name:CoMat 01-293 GLASS BEADS
Supply Name:CoMat 01-293 GLASS BEADS
Specification Groups:
Doc NumberType
OMAT:1/239SIZE NO.5 (0.0098 to 0.0165IN) CSS 8 VG300 AECMA prEN 2750
JCR-180SIZE NO.5 (0.0098 to 0.0165IN) CSS 8 VG300 AECMA prEN 2750
Suppliers:
ManufacturerRemarks
LOCAL
IE125
07852
IE301
K2769
Manufacturer Code:LOCAL
Supply Number:CoMat 02-003
Type:sp01
Supply Short Name:CoMat 02-003 ADHESIVE TAPE BLACK WATERPROOF
Supply Name:CoMat 02-003 ADHESIVE TAPE BLACK WATERPROOF
Specification Groups:
Doc NumberType
OMAT: 285ISATAPE 160
Suppliers:
ManufacturerRemarks
LOCAL
IE305
K6835
Manufacturer Code:0AM53
Supply Number:CoMat 05-006
Type:sp01
Supply Short Name:CoMat 05-006 GLASS BEADS
Supply Name:CoMat 05-006 GLASS BEADS
Specification Groups:
Doc NumberType
DELETED
Suppliers:
ManufacturerRemarks
0AM53
Manufacturer Code:1E1X8
Supply Number:CoMat 05-019
Type:sp01
Supply Short Name:CoMat 05-019 WATERPROOF SILICON CARBIDE
Supply Name:CoMat 05-019 WATERPROOF SILICON CARBIDE
Specification Groups:
Doc NumberType
OMAT: 5/31 (RR REF)WATERPROOF SILICON CARBIDE ABRASIVE PAPER, CAMI GRIT DESIGNATION 400 (ANSI B74.18)
JCR-184 (JAEC REF)
Suppliers:
ManufacturerRemarks
1E1X8
LOCAL
K6835
Manufacturer Code:1E1X8
Supply Number:CoMat 05-020
Type:sp01
Supply Short Name:CoMat 05-020 WATERPROOF SILICON CARBIDE
Supply Name:CoMat 05-020 WATERPROOF SILICON CARBIDE
Specification Groups:
Doc NumberType
OMAT: 5/33 (RR REF)WATERPROOF SILICON CARBIDE ABRASIVE PAPER, CAMI GRIT DESIGNATION 320 (ANSI B74.18)
JCR-027 (JAEC REF)
JCR-186 (JAEC REF)
Suppliers:
ManufacturerRemarks
1E1X8
LOCAL
K6835
Manufacturer Code:1E1X8
Supply Number:CoMat 05-021
Type:sp01
Supply Short Name:CoMat 05-021 WATERPROOF SILICON CARBIDE
Supply Name:CoMat 05-021 WATERPROOF SILICON CARBIDE
Specification Groups:
Doc NumberType
OMAT: 5/35 (RR REF)WATERPROOF SILICON CARBIDE ABRASIVE PAPER, CAMI GRIT DESIGNATION 240 (ANSI B74.18 )
JCR-188 (JAEC REF)
Suppliers:
ManufacturerRemarks
1E1X8
K6835
LOCAL
Manufacturer Code:0AM53
Supply Number:CoMat 05-030
Type:sp01
Supply Short Name:CoMat 05-030 CAST STEEL SHOT DELETED
Supply Name:CoMat 05-030 CAST STEEL SHOT DELETED
Specification Groups:
Doc NumberType
DELETED
Suppliers:
ManufacturerRemarks
0AM53
Manufacturer Code:LOCAL
Supply Number:CoMat 05-162
Type:sp01
Supply Short Name:CoMat 05-162 GLASS BEADS
Supply Name:CoMat 05-162 GLASS BEADS
Specification Groups:
Doc NumberType
OMAT:1/258SIZE NO.6 (0,007 TO 0,117IN) SIZE NO.7 (0,006 TO 0,010IN) ASTM-E-11-61 MIL-G-9954
Suppliers:
ManufacturerRemarks
LOCAL
0GU70
07852
IE125
IE301
K2769
Manufacturer Code:LOCAL
Tool Number:Fluorescent penetrant inspection equipment
Tool Name:Fluorescent Penetrant Inspection Equipment
Manufacturer Code:LOCAL
Tool Number:Glass bead peening equipment
Tool Name:Glass bead peening equipment
Manufacturer Code:0AM53
Tool Number:IAE 3J13165
Tool Name:IAE 3J13165 Shot peening fixture
Manufacturer Code:0AM53
Tool Number:IAE 3J13166
Tool Name:IAE 3J13166 Glass peening fixture
Manufacturer Code:0AM53
Tool Number:IAE 3J13168
Tool Name:IAE 3J13168 Glass peening fixture
Manufacturer Code:LOCAL
Tool Number:Shot peening equipment
Tool Name:Shot peening equipment