TASK 72-45-24-300-010 HPT Stage 2 Ring Segment And Vane Cluster - Unplug The Trailing Edge Slots And Cooling Holes, Repair-010 (VRS3317)

DMC:V2500-A0-72-45-2401-00A-652A-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 72-45-24-300-010 HPT Stage 2 Ring Segment And Vane Cluster - Unplug The Trailing Edge Slots And Cooling Holes, Repair-010 (VRS3317)

Effectivity

FIG/ITEM

PART NO.

02-070

2A0172CL21

02-071

2A0172CL22

02-072

2A0172CL23

02-073

2A0172CL24

02-074

2A0172CL25

02-075

2A0172CL26

02-076

2A0172CL27

02-077

2A0172CL28

02-078

2A0172CL29

02-079

2A0172CL30

02-080

2A0172CL31

02-081

2A0172CL32

02-082

2A0172DL33

02-083

2A0172CL34

02-084

2A0172CL35

02-087

2A0172CL38

02-088

2A0172CL39

02-089

2A0172CL40

02-090

2A0172CL41

02-093

2A0172CL36

02-094

2A0172CL36-5

02-095

2A0172CL37

02-096

2A0172CL37-5

02-270

2A1072CL21

02-271

2A1072CL22

02-272

2A1072CL23

02-273

2A1072CL24

02-274

2A1072CL25

02-275

2A1072CL26

02-276

2A1072CL27

02-277

2A1072CL28

02-278

2A1072CL29

02-279

2A1072CL30

02-280

2A1072CL31

02-281

2A1072CL32

02-282

2A1072CL33

02-283

2A1072CL34

02-284

2A1072CL35

02-287

2A1072CL38

02-288

2A1072CL39

02-289

2A1072CL40

02-290

2A1072CL41

02-293

2A1072CL36

02-294

2A1072CL36-5

02-295

2A1072CL37

02-296

2A1072CL37-5

02-070

2A2072CL21

02-071

2A2072CL22

02-072

2A2072CL23

02-073

2A2072CL24

02-074

2A2072CL25

02-075

2A2072CL26

02-076

2A2072CL27

02-077

2A2072CL28

02-078

2A2072CL29

02-079

2A2072CL30

02-080

2A2072CL31

02-081

2A2072CL32

02-082

2A2072CL33

02-083

2A2072CL34

02-084

2A2072CL35

02-087

2A2072CL38

02-088

2A2072CL39

02-089

2A2072CL40

02-090

2A2072CL41

02-093

2A2072CL36

02-094

2A2072CL36-5

02-095

2A2072CL37

02-096

2A2072CL37-5

02-270

2A2172CL21

02-271

2A2172CL22

02-272

2A2172CL23

02-277

2A2172CL28

02-278

2A2172CL29

02-279

2A2172CL30

02-280

2A2172CL31

02-281

2A2172CL32

02-282

2A2172CL33

02-283

2A2172CL34

02-284

2A2172CL35

02-287

2A2172CL38

02-288

2A2172CL39

02-289

2A2172CL40

02-290

2A2172CL41

02-293

2A2172CL36

02-296

2A2172CL37-5

02-070

2A2772CL21

02-071

2A2772CL22

02-072

2A2772CL23

02-073

2A2772CL24

02-074

2A2772CL25

02-075

2A2772CL26

02-076

2A2772CL27

02-077

2A2772CL28

02-078

2A2772CL29

02-079

2A2772CL30

02-080

2A2772CL31

02-081

2A2772CL32

02-082

2A2772CL33

02-083

2A2772CL34

02-084

2A2772CL35

02-085

2A2772CL36

02-086

2A2772CL37

02-087

2A2772CL38

02-088

2A2772CL39

02-089

2A2772CL40

02-090

2A2772CL41

02-270

2A2872CL21

02-271

2A2872CL22

02-272

2A2872CL23

02-273

2A2872CL24

02-274

2A2872CL25

02-275

2A2872CL26

02-276

2A2872CL27

02-277

2A2872CL28

02-278

2A2872CL29

02-279

2A2872CL30

02-280

2A2872CL31

02-281

2A2872CL32

02-282

2A2872CL33

02-283

2A2872CL34

02-284

2A2872CL35

02-285

2A2872CL36

02-286

2A2872CL37

02-287

2A2872CL38

02-288

2A2872CL39

02-289

2A2872CL40

02-290

2A2872CL41

02-050

2A3372

02-050

2A3812

02-250

2A2272

02-260

2A2372

02-260

2A3472

02-260

2A3822

02-260

2A317

02-070

2A3272CL21

02-071

2A3272CL22

02-072

2A3272CL23

02-073

2A3272CL24

02-074

2A3272CL25

02-075

2A3272CL26

02-076

2A3272CL27

02-077

2A3272CL28

02-078

2A3272CL29

02-079

2A3272CL30

02-080

2A3272CL31

02-081

2A3272CL32

02-082

2A3272CL33

02-083

2A3272CL34

02-084

2A3272CL35

02-085

2A3272CL36

02-086

2A3272CL37

02-087

2A3272CL38

02-088

2A3272CL39

02-089

2A3272CL40

02-090

2A3272CL41

02-050

2A5102

02-260

2A5202

02-050

2A5502

02-050

2A5602

Material of component

PART IDENT

SYMBOL

MATERIAL

Stage 2 HPT vane cluster assembly

-

Nickel base alloy

General

Price and availability - refer to IAE

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

NOTE

To identify the consumable materials, refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
ReamersLOCALReamers
Spring wireLOCALSpring wire
Ultrasonic cleaning equipmentLOCALUltrasonic cleaning equipment

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-339 ALKALI CLEANER (GENERAL PURPOSE)LOCALCoMat 01-339
CoMat 10-058 PENETRATING OIL0AM53CoMat 10-058

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-45-24-350-078 Unplug the Trailing Edge Slots and the Cooling Holes

      CAUTION

      REAMERS ARE RECOMMENDED AS AN ALTERNATIVE TO SPRING WIRE OR DRILL BITS FOR THE INITIAL PROBING. WIRE CAN BREAK OFF LARGER PIECES OF UNWANTED MATERIAL AND FORCE THEM INTO THE INTERNAL CAVITY. DRILLS BREAK EASIER AND CAN GET CAUGHT IN THE HOLE.
      1. Unplug the trailing edge slots and the cooling holes with a reamer. Use spring wire with a pin vise if you cannot reach an area with a reamer.

      2. Refer to Figure and Figure.

        Apply CoMat 10-058 PENETRATING OIL to the holes.

        Let the oil soak into unwanted material in the holes.

        Use a rotary motion while you probe.

        Intermittently move the reamer farther into the hole and then remove it while you hold the vane so the holes point down to let unwanted material fall out.

      1. CAUTION

        THE AIRFOIL HOLES ARE DIFFERENT SIZES. MAKE SURE YOU USE THE CORRECT REAMER SIZE FOR EACH HOLE. DO NOT DAMAGE THE COATING WHEN YOU PROBE THE HOLES.

        Continue to probe so the holes in the airfoil and platform are to the diameters given in Figure, Figure and Figure.

      2. Finish the probing with wire. Reamers are tapered and will cause the holes to have a taper.

        If you use a wire, the taper will be kept to a minimum.

    1. SUBTASK 72-45-24-130-054 Clean the Vane Assembly

      1. Do an ultrasonic cleaning to remove unwanted material from internal areas.

      2. Refer to the SPM TASK 70-13-02-300-501.

        Use CoMat 01-339 ALKALI CLEANER (GENERAL PURPOSE) at a temperature of 150 deg F (66 deg C) maximum.

        Position the vane at different angles to remove unwanted material from the inner areas of the vane.

        NOTE

        Ultrasonics will increase the temperature of the solution.
    1. SUBTASK 72-45-24-720-051 Do an Airflow Check of the Vane Cluster Assembly

      1. Do an airflow check of the airfoil holes in the vane cluster assembly. It is not necessary to do an airflow check of the platform cooling holes.

      2. Refer to the SPM TASK 70-72-01-720-501.

        If the airflow is not sufficient, hand probe the holes again.

        Increase the hole size in small increments. Hand probe only a few holes at a time so you do not cause too much airflow.

        If there is too much airflow, examine the vanes again to find out if the condition is caused by the vane or by air leaks in the test setup.

        If there is too much airflow, reject the vanes.

    1. SUBTASK 72-45-24-130-055 Clean the Vane Assembly

      1. Do an ultrasonic cleaning to remove unwanted material from internal areas.

      2. Refer to the SPM TASK 70-13-02-300-501.

        Use CoMat 01-339 ALKALI CLEANER (GENERAL PURPOSE) at a temperature of 150 deg F (66 deg C) maximum.

        NOTE

        Ultrasonics will increase the temperature of the solution.
  1. Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

Requirements After Job Completion

Follow-On Conditions

NONE
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:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 01-339
Type:sp01
Supply Short Name:CoMat 01-339 ALKALI CLEANER (GENERAL PURPOSE)
Supply Name:CoMat 01-339 ALKALI CLEANER (GENERAL PURPOSE)
Specification Groups:
Doc NumberType
CEE-BEE A-7X7SPMC 104 (PW REF)
SPMC 104CEE-BEE A-7X7
Suppliers:
ManufacturerRemarks
LOCAL
3MCT7
U5702
Manufacturer Code:X222X
Supply Number:CoMat 10-058
Type:sp01
Supply Short Name:CoMat 10-058 PENETRATING OIL
Supply Name:CoMat 10-058 PENETRATING OIL
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Tool Number:Reamers
Tool Name:Reamers
Manufacturer Code:LOCAL
Tool Number:Spring wire
Tool Name:Spring wire
Manufacturer Code:LOCAL
Tool Number:Ultrasonic cleaning equipment
Tool Name:Ultrasonic cleaning equipment