TASK 72-45-24-300-021 HPT Stage 2 Ring Segment And Vane Cluster - Replace The Vane Cover, Repair-021 (VRS3320)

DMC:V2500-A0-72-45-2401-07A-920A-C|Issue No:001.00|Issue 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 72-45-24-300-021 HPT Stage 2 Ring Segment And Vane Cluster - Replace The Vane Cover, Repair-021 (VRS3320)

Effectivity

FIG/ITEM

PART NO.

02-130

2A0152CL21

02-131

2A0152CL22

02-132

2A0152CL23

02-133

2A0152CL24

02-134

2A0152CL25

02-135

2A0152CL26

02-136

2A0152CL27

02-137

2A0152CL28

02-138

2A0152CL29

02-139

2A0152CL30

02-140

2A0152CL31

02-141

2A0152CL32

02-142

2A0152CL33

02-143

2A0152CL34

02-144

2A0152CL35

02-145

2A0152CL36

02-146

2A0152CL37

02-147

2A0152CL38

02-148

2A0152CL39

02-149

2A0152CL40

02-150

2A0152CL41

02-350

2A0152CL21

02-351

2A0152CL22

02-352

2A0152CL23

02-353

2A0152CL24

02-354

2A0152CL25

02-355

2A0152CL26

02-356

2A0152CL27

02-357

2A0152CL28

02-358

2A0152CL29

02-359

2A0152CL30

02-360

2A0152CL31

02-361

2A0152CL32

02-362

2A0152CL33

02-363

2A0152CL34

02-364

2A0152CL35

02-365

2A0152CL36

02-366

2A0152CL37

02-367

2A0152CL38

02-368

2A0152CL39

02-369

2A0152CL40

02-370

2A0152CL41

02-420

2A1052CL21

02-421

2A1052CL22

02-422

2A1052CL23

02-423

2A1052CL24

02-424

2A1052CL25

02-425

2A1052CL26

02-426

2A1052CL27

02-427

2A1052CL28

02-428

2A1052CL29

02-429

2A1052CL30

02-430

2A1052CL31

02-431

2A1052CL32

02-432

2A1052CL33

02-433

2A1052CL34

02-434

2A1052CL35

02-435

2A1052CL36

02-436

2A1052CL37

02-437

2A1052CL38

02-438

2A1052CL39

02-439

2A1052CL40

02-440

2A1052CL41

02-130

2A1152CL21

02-131

2A1152CL22

02-132

2A1152CL23

02-133

2A1152CL24

02-134

2A1152CL25

02-135

2A1152CL26

02-136

2A1152CL27

02-137

2A1152CL28

02-138

2A1152CL29

02-139

2A1152CL30

02-140

2A1152CL31

02-141

2A1152CL32

02-142

2A1152CL33

02-143

2A1152CL34

02-144

2A1152CL35

02-145

2A1152CL36

02-146

2A1152CL37

02-147

2A1152CL38

02-148

2A1152CL39

02-149

2A1152CL40

02-150

2A1152CL41

02-350

2A1152CL21

02-351

2A1152CL22

02-352

2A1152CL23

02-353

2A1152CL24

02-354

2A1152CL25

02-355

2A1152CL26

02-356

2A1152CL27

02-357

2A1152CL28

02-358

2A1152CL29

02-359

2A1152CL30

02-360

2A1152CL31

02-361

2A1152CL32

02-362

2A1152CL33

02-363

2A1152CL34

02-364

2A1152CL35

02-365

2A1152CL36

02-366

2A1152CL37

02-367

2A1152CL38

02-368

2A1152CL39

02-369

2A1152CL40

02-370

2A1152CL41

02-420

2A1252CL21

02-421

2A1252CL22

02-422

2A1252CL23

02-423

2A1252CL24

02-424

2A1252CL25

02-425

2A1252CL26

02-426

2A1252CL27

02-427

2A1252CL28

02-428

2A1252CL29

02-429

2A1252CL30

02-430

2A1252CL31

02-431

2A1252CL32

02-432

2A1252CL33

02-433

2A1252CL34

02-434

2A1252CL35

02-435

2A1252CL36

02-436

2A1252CL37

02-437

2A1252CL38

02-438

2A1252CL39

02-439

2A1252CL40

02-440

2A1252CL41

Material of component

RR

DESCRIPTION

SYMBOL

MATERIAL

Stage 2 HPT vane assembly

-

Nickel alloy

Stage 2 HPT vane cover

-

Nickel alloy

General

The practices and processes referred to in the procedure by the TASK number are in the SPM.

Price and availability - refer to IAE

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Magnifying glassLOCALMagnifying glass

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 03-151 HIGH TEMP. BRAZING FILLERPOWDERLOCALCoMat 03-151
CoMat 03-152 BRAZING FILLER POWDERLOCALCoMat 03-152
CoMat 03-154 BRAZING FILLER POWDERLOCALCoMat 03-154
CoMat 03-287 WELDING FILLER WIRELOCALCoMat 03-287

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Cover2A0049AR

(for PN 2A0152 and PN 2A1052)

Cover2A0049AR
Cover2A0049AR
Cover2A2706AR

(for PN 2A1152, PN 2A1252 and 2A3152)

Cover2A2706AR
Cover2A2706AR

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-45-24-350-085 Remove the Cover from the Vane Assembly

      1. Remove the cover from the vane.

      2. Refer to Figure. Remove the minimum material necessary from the vane surface so you do not open the plug welded vane cavity hole.

    2. NOTE

      If you open the vane cavity hole, you can prepare and weld the hole with CoMat 03-287 WELDING FILLER WIRE and the manual gas tungsten arc method.
    1. SUBTASK 72-45-24-110-057 Clean the Vane Assembly

      1. Clean the vane.

      2. Do the procedure given in the SPM TASK 70-11-03-300-503. You can also clean the vane in a furnace that is at 1250 to 1350 deg F (677 to 732 deg C) for a minimum of five minutes with a minimum of 10 minutes above 1000 deg F (537.8 deg C). The time above 1000 deg F (537.8 deg C) must not be more than 60 minutes. If you clean the vane in a furnace, you must also do an abrasive clean.

    1. SUBTASK 72-45-24-310-054-001 Install the Replacement Cover by Brazing

      NOTE

      You can braze the cover and the honeycomb at the same time. Refer to Repair, VRS3223 TASK 72-45-24-300-006 (REPAIR-006).
      1. Position the cover on center on the vane.

      2. Refer to Figure or Figure.

      1. Braze the cover to the vane.

      2. Do the procedure given in the SPM TASK 70-31-16-310-501. Braze the cover at 1950 to 2000 deg F (1066 to 1093 deg C).

        Use CoMat 03-151 HIGH TEMP. BRAZING FILLERPOWDERCoMat 03-152 BRAZING FILLER POWDERCoMat 03-154 BRAZING FILLER POWDER. Nickel plate can be omitted if brazed in a vacuum. If you do not braze in a vacuum, nickel plate the area to be brazed by the procedure given in the SPM TASK 70-33-06-300-503. You can tack weld the cover with CoMat 03-287 WELDING FILLER WIRE before you braze it. A minimum of 30 percent joining is required, with the line of braze requirement waived.

    2. NOTE

      Local braze with the manual plasma arc or gas tungsten arc torch method and the initial braze alloy type wire is acceptable. Two braze cycles are permitted.
    1. SUBTASK 72-45-24-310-054-002 Install the Replacement Cover by Welding

      1. Position the cover on center on the vane.

      2. Refer to Figure or Figure.

      1. Weld the cover to the vane.

      2. Do the procedure given in the SPM TASK 70-31-13-310-501. Weld the cover with the manual gas tungsten arc or laser beam method. You can use CoMat 03-287 WELDING FILLER WIRE. You can tack weld the cover to align it.

    1. SUBTASK 72-45-24-220-123 Examine the Repaired Area

      NOTE

      This procedure is an alternative to Step.
      1. Visually inspect the repaired area.

      2. Refer to Figure.

        Use a magnifying glass. Discontinuites that are in 0.015in. (0.381 mm) or less, random or in clusters, are permitted if they are not in linear alignment. Six discontinuites that are porosity, voids or shrinkage and are 0.030in. (0.762 mm) or less are permitted in each joint if they are separated by a minimum of 0.125in. (3.175 mm). Cracks that are 0.125in. (3.175 mm) or less in length and are separated by a minimum of 0.125in. (3.175 mm) in all directions are permitted in the weld or braze material of each joint. Two or more cracks that are separated in a 0.125in. (3.175 mm) crack length distance is treated as a single crack and are permitted in the weld or braze material of each joint.

    1. SUBTASK 72-45-24-230-059 Examine the Repaired Area

      NOTE

      This procedure is an alternative to Step.
      1. Fluorescent penetrant inspect the repaired area.

      2. Do the procedure given in the SPM TASK 70-23-01-230-501 or SPM TASK 70-23-02-230-501.

        Refer to Figure.

        Discontinuities that are 0.015in. (0.381 mm) or less, random or in clusters, are permitted if they are not in linear alignment. Six discontinuities that are porosity, voids or shrinkage and are 0.030in. (0.762 mm) or less are permitted in each joint if they are separated by a minimum of 0.125in. (3.175 mm). Cracks that are 0.125in. (3.175 mm) or less in length and are separated by a minimum of 0.125in. (3.175 mm) in all directions are permitted in the weld or braze material of each joint. Two or more cracks that are separated in a 0.125in. (3.175 mm) crack length distance is treated as a single crack and are permitted in the weld or braze material of each joint.

    1. SUBTASK 72-45-24-280-060 Examine the Vane by the Airflow Check

      1. Do an airflow check.

      2. Do the airflow check on passage BL with passage BM blocked. Refer to Figure. Do the airflow check in the direction shown in Figure.

  1. Figure: Stage 2 HPT vane cover replacement

    Stage 2 HPT vane cover replacement

    Figure: Stage 2 HPT vane cover replacement

    Stage 2 HPT vane cover replacement

    Figure: Weld or braze the replacement stage 2 HPT vane cover (PN 2A0049)

    Weld or braze the replacement stage 2 HPT vane cover (PN 2A0049)

    Figure: Weld or braze the replacement stage 2 HPT vane cover (PN 2A2706)

    Weld or braze the replacement stage 2 HPT vane cover (PN 2A2706)

    Figure: Stage 2 HPT vane airflow check limits

    Stage 2 HPT vane airflow check limits

    Figure: Weld and braze joints crack limits

    Weld and braze joints crack limits

Requirements After Job Completion

Follow-On Conditions

NONE
Link not Found
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Link not Found
Manufacturer Code:LOCAL
Supply Number:CoMat 03-151
Type:sp01
Supply Short Name:CoMat 03-151 HIGH TEMP. BRAZING FILLER POWDER
Supply Name:CoMat 03-151 HIGH TEMP. BRAZING FILLERPOWDER
Specification Groups:
Doc NumberType
OMAT: 3/118NICROBRAZ 130 MSRR9500/114
Suppliers:
ManufacturerRemarks
LOCAL
K6835
63585
IE441
U0163
Manufacturer Code:LOCAL
Supply Number:CoMat 03-152
Type:sp01
Supply Short Name:CoMat 03-152 BRAZING FILLER POWDER
Supply Name:CoMat 03-152 BRAZING FILLER POWDER
Specification Groups:
Doc NumberType
OMAT:3/118AENDEWRANCE CM 52 (-150 MESH) B.S.1845 HTN3 AMS 4778
JCR-218ENDEWRANCE CM 52 (-150 MESH) B.S.1845 HTN3 AMS 4778
Suppliers:
ManufacturerRemarks
LOCAL
K5086
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 03-154
Type:sp01
Supply Short Name:CoMat 03-154 BRAZING FILLER POWDER
Supply Name:CoMat 03-154 BRAZING FILLER POWDER
Specification Groups:
Doc NumberType
MSRR9500/114NIBSI 4 (-150 MESH) AMS4778 B.S.1845 HTN3
OMAT:3/118CNIBSI 4 (-150 MESH) AMS4778 B.S.1845 HTN3
JCR-220NIBSI 4 (-150 MESH) AMS4778 B.S.1845 HTN3
Suppliers:
ManufacturerRemarks
LOCAL
64972
IE306
K5086
K6835
U0163
Manufacturer Code:LOCAL
Supply Number:CoMat 03-287
Type:sp01
Supply Short Name:CoMat 03-287 WELDING FILLER WIRE
Supply Name:CoMat 03-287 WELDING FILLER WIRE
Specification Groups:
Doc NumberType
INCONEL 625 AMS 5837 AMS 5837
Suppliers:
ManufacturerRemarks
LOCAL
2R602
55596
58401
Link not Found