TASK 72-41-11-300-016 HPC Stage 3 - 8 Drum Disk - Blend Repair To Restore The Surface Condition On The Stages 3 To 5 Dovetail Slots, Repair-016 (VRS6300)

DMC:V2500-A0-72-41-1101-06A-649A-C|Issue No:002.00|Issue Date:2016-08-01

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 72-41-11-300-016 HPC Stage 3 - 8 Drum Disk - Blend Repair To Restore The Surface Condition On The Stages 3 To 5 Dovetail Slots, Repair-016 (VRS6300)

Effectivity

FIG/ITEM

PART NO.

01-200

6A3508

01-200

6A3648

01-200

6A3934

01-200

6A3936

01-200

6A4189

01-200

6A4900

01-200

6A5594

01-200

6A5467

01-200

6A5592

01-200

6A5659

01-200

6A6473

01-200

6A7379

01-200

6A7380

01-200

6A7382

01-200

6A7383

01-200

6A7384

01-200

6A7385

01-200

6A7401

01-200

6A7705

01-200

6A8236

01-200

6A8316

01-200

6A8318

01-200

6A8350

01-200

6B1379

01-200

6B1380

01-200

6B1381

01-200

6B1382

01-200

6B1383

01-200

6B1384

01-200

6B1385

01-200

6B1386

01-200

6B1387

01-200

6B1391

01-200

6B1392

01-200

6B1393

01-200

6B1401

01-200

6B1402

01-200

6B1403

01-200

6B1404

01-200

6B1405

01-200

6B1406

Material of component

PART IDENT

MATERIAL

HP Compressor Stage 3 to 8 Disks Shaft Assembly

Titanium Alloy

General

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 72-41-11.

This repair permits the removal of damaged material from those areas of the axial dovetail slots, stages 3, 4 and 5, specified Zone B and Zone C only.

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

To put back the surface condition it is necessary to shot peen surfaces where the total depth of material, including damage, removed is more than 0.002 in. (0.05 mm) in depth.

The shot peened part of this repair requires to be source demonstrated and can only be done by approved vendors.

The shot peened part of this repair can only be done four times on any one dovetail stage and must be shot peened after damaged material has been removed.

CAUTION

YOU MUST NOT REMOVE MATERIAL FROM ZONE A.

For Zone A if the damage is galling only, up to 0.002 in. (0.051 mm) maximum, you must do Step.

Local areas of damage (nicks, dents, scores and frettage) may be removed from Zone B and Zone C on all Stage 3, 4 and 5 dovetail posts, provided there are not more than two in number in any Zone for each dovetail post and they are not less than 0.250 in. (6.35 mm) apart.

The maximum depth permitted after damaged material (nicks, dents, scores and/or frettage) is removed, to leave a smooth surface finish in Zone B only, is 0.010 in. (0.254 mm).

If the damage is nicks, dents or scores the maximum depth of damage before material removal, in Zone B only, is 0.005 in. (0.127 mm) and you must remove the damage to 2X depth, to a maximum depth of 0.010 in. (0.254 mm).

If the damage is frettage the maximum depth of damage before material removal, in Zone B only, is 0.010 in. (0.254 mm) and you must remove the damage to depth, to a maximum depth of 0.010 in. (0.254 mm).

The maximum depth permitted after damaged material (nicks, dents, scores and/or frettage) is removed, to leave smooth surface finish in Zone C only, is 0.020 in. (0.508 mm).

Material removal may overlap into other Zones. If this occurs you must use the limit with the least material removal.

TASKS identified by SPM TASK are in the Standard Practices and Manual (SPM).

Price and availability

Refer to International Aero Engines

Related repairs - none

NOTE

Equipment and materials necessary to do this repair are in SPM TASKS given below :
TASK 70-09-00-400-501
TASK 70-11-08-300-503
TASK 70-23-05-230-501
TASK 70-35-03-300-501
TASK 70-38-04-300-503

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 Overhaul Processes and Consumable Index Manual (CoMat).

NOTE

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

NOTE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Penetrant Crack Test EquipmentLOCALPenetrant crack test equipment
Standard workshop equipmentLOCALStandard workshop equipment
Chemical cleaning equipmentLOCALChemical cleaning equipment
BinocularsLOCALBinoculars

10X

Glass bead peening equipmentLOCALGlass bead peening equipment
Vibrating marking pencilLOCALVibrating marking pencil
Shot peening equipmentLOCALShot peening equipment

Controlled

IAE 3R19465 Shot Peen Fixture0AM53IAE 3R194651
IAE 3R19466 Almen Plate Carrier0AM53IAE 3R194661
IAE 3R19468 Almen Plate Holder0AM53IAE 3R194681

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-003 ADHESIVE TAPE BLACK WATERPROOFLOCALCoMat 02-003
CoMat 05-020 WATERPROOF SILICON CARBIDELOCALCoMat 05-020
CoMat 05-021 WATERPROOF SILICON CARBIDE44197CoMat 05-021
CoMat 05-028 METALLIC SHOT (CAST STEEL), S230IE249CoMat 05-028
CoMat 05-106 ABRASIVE STONEK6835CoMat 05-106
CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY)LOCALCoMat 06-022

Spares

NONE

Safety Requirements

NONE

Procedure

    1. Repair Facilities

    1. Only the shot peening part of this Repair requires Source Demonstration. This means that any facility not authorized to shot peen, either utilize the Authorized Repair Vendors listed below or contact the IAE Repair Services Group to determine if a qualification program can be initiated at their facility.

      IAE - INTERNATIONAL AERO ENGINES AG
      C/O ROLLS-ROYCE PLC.
      PO BOX 31
      DERBY DE24 8BJ
      ENGLAND
      ATTN: MANAGER TECHNICAL SERVICES
    2. Authorized Repair Vendors for the shot peening portion of VRS6300 are listed below:
      METAL IMPROVEMENT COMPANY INC.
      DERBY DIVISION (UK)
      ASCOT DRIVE
      DERBY DE2 8ST
      ENGLAND
      ATTN: DIVISION MANAGER
      METAL IMPROVEMENT COMPANY INC.
      145 ADDISION ROAD
      WINDSOR
      CONNECTICUT
      CT06095
      USA
      ATTN: DIVISION MANAGER
      MTU MAINTENACE GMBH
      FLUGHAFEN HANNOVER
      MUNCHNER STRASSE 31
      POSTFACH 1720
      3012 LANGENHAGEN
      GERMANY
      ATTN. MANAGER, QUALITY ASSURANCE
      ISHIKAWAJIMA-HARIMA HEAVY INDUSTRIES CO. LTD.
      229 TONOGAYA, MIZUHO-MACHI
      NISHITAMA-GUN
      TOKYO 190-1292
      JAPAN
      LUFTHANSA TECHNIK AG
      WEB BEIM JAGER 193
      D-22335 HAMBURG
      GERMANY
    3. The designation by IAE of an Authorized Repair Vendor indicates that the Repair Vendor has demonstrated the necessary capability to enable it to carry out the listed repair work. However, IAE makes no warranties or representations concerning the qualifications or quality standards of the Repair Vendors to carry out the repair work, and accepts no responsibility whatsoever for any work that may be carried out by a Repair Vendor other than when IAE is listed as the Repair Vendor. Authorized Repair Vendors do not act as agents or representatives of IAE.
    2. SUBTASK 72-41-11-220-096 Examine the Assembly
    1. Refer to Figure and Figure.
      2. Visually examine the stage 3, 4 and 5 dovetails, for a code symbol to tell you shot peening has been done before.
      1. Look for the code symbol on the outer diameter of each dovetail post.
      2. Reject the assembly if you see the code symbol with the letter D, N or Z, on an area that is damaged again.
    3. SUBTASK 72-41-11-230-068 Do a Crack Test
      1. Do a local penetrant crack test of the damaged area.
      1. Refer to SPM TASK 70-23-05-230-501.
      4. No cracks are permitted.
    4. SUBTASK 72-41-11-350-068 Remove Damaged Area(s), Zone B Only
    1. CAUTION
      TITANIUM COMPONENTS - YOU MUST USE SILICON CARBIDE TYPE ABRASIVE WHEELS, STONES AND PAPERS TO DRESS, BLEND AND POLISH THIS COMPONENT.
      CAUTION
      TITANIUM COMPONENTS- MAXIMUM SPEED FOR MECHANICAL TOOLS MUST NOT EXCEED 1000 REVOLUTIONS PER MINUTE.
      CAUTION
      TITANIUM COMPONENTS - YOU MUST MAKE SURE THAT WHEN YOU REMOVE MATERIAL, BLEND AND POLISH, TO MAKE SMOOTH, THAT NO SPARKS ARE PRODUCED.
      CAUTION
      TITANIUM COMPONENTS - IF THE MATERIAL SHOWS A CHANGE IN COLOR, TO A DARKER THAN A LIGHT STRAW COLOR, THE COMPONENT IS TO BE REJECTED.
      CAUTION
      TITANIUM COMPONENTS - AVOID BUILD UP OF HEAT BY APPLYING ONLY GENTLE PRESSURE AND KEEPING THE TOOL SPEED AS LOW AS POSSIBLE. USE TECHNIQUES WHICH ALLOW FOR PROGRESSIVE OF THE DRESSING MEDIA TO PRESENT A CONTINUALLY FRESH CUTTING SURFACE TO THE WORK PIECE.
      CAUTION
      DO NOT DWELL ON ONE AREA OF THE COMPONENT.
      CAUTION
      DRESS, WHERE POSSIBLE, IN A CIRCULAR MOTION; TAKING LIGHT CUTS TO AVOID OVERHEATING.
      2. Remove damaged material, as necessary.
      1. Refer to SPM TASK 70-35-03-300-501.
      3. Remove no more material than is necessary.
      4. If you use mechanical tools do not exceed 1000 rpm.
      6. You must restore corner radii.
    3. If material damage is frettage you must dress to depth to a maximum depth of 0.010 in. (0.254 mm).
    4. If material damage is nicks, dents or scores you must dress to 2X depth to a maximum depth of 0.010 in. (0.254 mm).
      NOTE
      Material removal may overlap into other Zones. If this occurs you must use the limit with the least material removal.
      5. Make smooth the cut away area.
        1. Refer to SPM TASK 70-35-03-300-501.
        2. Remove sharp corners.
        3. If you use mechanical tools do not exceed 1000 rpm.
        5. You must restore corner radii.
      6. Polish the cut away area.
      1. Refer to SPM TASK 70-35-03-300-501.
      3. Polish to give a surface finish the same as the adjacent material.
      4. If you use mechanical tools do not exceed 1000 rpm.
      6. You must restore corner radii.
    5. SUBTASK 72-41-11-350-079 Remove Damaged Area(s), Zone C Only
    1. CAUTION
      TITANIUM COMPONENTS - YOU MUST USE SILICON CARBIDE TYPE ABRASIVE WHEELS, STONES AND PAPERS TO DRESS, BLEND AND POLISH THIS COMPONENT.
      CAUTION
      TITANIUM COMPONENTS- MAXIMUM SPEED FOR MECHANICAL TOOLS MUST NOT EXCEED 1000 REVOLUTIONS PER MINUTE.
      CAUTION
      TITANIUM COMPONENTS - YOU MUST MAKE SURE THAT WHEN YOU REMOVE MATERIAL, BLEND AND POLISH, TO MAKE SMOOTH, THAT NO SPARKS ARE PRODUCED.
      CAUTION
      TITANIUM COMPONENTS - IF THE MATERIAL SHOWS A CHANGE IN COLOR, TO A DARKER THAN A LIGHT STRAW COLOR, THE COMPONENT IS TO BE REJECTED.
      CAUTION
      TITANIUM COMPONENTS - AVOID BUILD UP OF HEAT BY APPLYING ONLY GENTLE PRESSURE AND KEEPING THE TOOL SPEED AS LOW AS POSSIBLE. USE TECHNIQUES WHICH ALLOW FOR PROGRESSIVE OF THE DRESSING MEDIA TO PRESENT A CONTINUALLY FRESH CUTTING SURFACE TO THE WORK PIECE.
      CAUTION
      DO NOT DWELL ON ONE AREA OF THE COMPONENT.
      CAUTION
      DRESS, WHERE POSSIBLE, IN A CIRCULAR MOTION; TAKING LIGHT CUTS TO AVOID OVERHEATING.
      2. Remove frettage, nicks, dents and/or scores, as necessary, to a maximum depth of 0.020 in. (0.508 mm).
      1. Refer to SPM TASK 70-35-03-300-501.
      3. Remove no more material than is necessary.
      4. If you use mechanical tools do not exceed 1000 rpm.
      6. You must restore corner radii.
        NOTE
        Material removal may overlap into other Zones. If this occurs you must use the limit with the least material removal.
      3. Make smooth the cut away area(s).
      1. Refer to SPM TASK 70-35-03-300-501.
      3. Remove sharp corners.
      4. If you use mechanical tools do not exceed 1000 rpm.
      6. You must restore corner radii.
      4. Polish the cut away area(s).
      1. Refer to SPM TASK 70-35-03-300-501.
      3. Polish to give a surface finish the same as the adjacent material.
      4. If you use mechanical tools do not exceed 1000 rpm.
      6. You must restore corner radii.
    6. SUBTASK 72-41-11-220-097 Examine the Repaired Area(s)
      2. Make a visual inspection of the repaired area(s) and measure the depth of the repaired area(s).
      1. Make sure the surface finish compares with adjacent surfaces.
      2. Refer to the different Zones for the maximum depth of material removal.
    3. NOTE
      1. Ignore SUBTASK 72-41-11-380-054, when the depth of a repaired area is not more than 0.002 in. (0.05 mm).
      2.  Material removal may overlap into other Zones. If this occurs you must use the limit with the least material removal.
    7. SUBTASK 72-41-11-110-063 Do a Swab Etch
      1. Chemically clean.
      1. Refer to SPM TASK 70-11-08-300-503, SUBTASK 70-11-08-300-001.
      2. Swab etch the repaired area.
      1. Refer to SPM , SUBTASK 70-11-08-300-002.
    8. SUBTASK 72-41-11-220-098 Binocular Examine the Repaired Area(s)
      2. Binocular examine the repaired area.
        1. Use 10x binoculars.
        1. Indications of surface defects are not permitted.
        2. Make sure that there is no raised metal remaining.
    9. SUBTASK 72-41-11-230-069 Do a Crack Test
      1. Do a local penetrant crack test of the repaired area.
      1. Refer to SPM TASK 70-23-05-230-501.
      3. No cracks are permitted.
    10. SUBTASK 72-41-11-110-079 Chemically Clean
      1. Chemically clean the repaired area to remove fluorescent penetrant.
      1. Refer to SPM TASK 70-11-26-300-503.
    11. SUBTASK 72-41-11-350-069 Identify the Repair
      NOTE
      This SUBTASK is required when the damaged material removed is more than 0.002 in. (0.05 mm), in depth.
      NOTE
      This SUBTASK shows which stages of dovetails have been repaired and require to be shot peened.
    1. Refer to Figure.
      2. Vibro engrave a code symbol on any dovetail of the stage or stages which have been repaired.
      1. Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.
      2. NOTE
        The letter inside the code symbol shows the number of times this area has been shot peened.
    12. SUBTASK 72-41-11-380-054 Shot Peen the Dovetail Slot
    1. NOTE
      This SUBTASK is only required to put back the surface condition, when the depth of material removal is more than 0.002 in. (0.052 mm).
      NOTE
      Shot peen the dovetail slots in areas identified AD, on stage 3, 4 and/or 5.
      NOTE
      Unwanted shot peen spray is permitted into the dovetail slots and on to the outer diameter of each stage of dovetail posts, to get a continuous fade-out surface condition away from the repaired area.
      2. Find the area to be shot peened.
      1. Refer to Step.
      3. Seal the full assembly but for the stage or stages which have to be shot peened.
      2. Patch mask all identification marks and symbols.
      4. Shot peen the area(s) identified AD, as necessary.
      1. Refer to SPM TASK 70-38-04-300-503, SUBTASK 70-38-04-300-002.
      3. Use CoMat 05-028 METALLIC SHOT (CAST STEEL), S230 to get an Almen intensity of 0.006 in to 0.010 in. (0.15 mm to 0.25 mm) on 'A' type test strip.
      4.   Shot-peening Data
          Machine type
        Metal shot-peen
          Process type/mode
        Dry/auto
          Shot-type
          Shot size
        0.024 in. to 0.40 in. (0.600 mm to 1.016 mm)
          Shot hardness
        450 Hv to 600 Hv
          Coverage
        200 percent
          Number of nozzles
        4 or 8
          Almen intensity
        0.006 in. to 0.010 in. (0.15 mm to 0.25 mm) using
        an "A" type test strip
        NOTE
        For information the, table speed, oscillation height, type, air pressure, nozzle type/diameter and work distance may change if different equipment is being used. You must achieve full coverage and Almen intensity,
    5. Make sure all loose unwanted cast steel shot is removed.
      6. Remove iron contamination after you have shot-peened, as necessary.
      1. Refer to approved vendors in Step and/or SPM TASK 70-38-04-300-503, SUBTASK 70-38-04-300-002.
      2. Use wet or dry glass beads, with Glass bead peening equipment.
    7. Remove mechanical seals and seal tape.
    13. SUBTASK 72-41-11-220-099 Examine the Shot Peened Area(s)
      2. Make a visual inspection of the shot peened area.
      1. Refer to approved vendors in Step.
    14. 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
    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
    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
Change Type: 
Revised effectivity table and added comat reference. (92VR764I)
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:IE249
Enterprise Name:DELETED - Was FERGUSSON AND WILD CO LTD,ABRASIVES AND AGGREGATES (no longer in business)
BU Name:DELETED - FERGUSSON AND WILD CO LTD,ABRASIVES AND AGGREGATES (no longer in business)
Manufacturer Code:K6835
Enterprise Name:MED-LAB LTD
BU Name:MED-LAB LTD
Street:COPELAND ST
City:DERBY
Zip Code:DE1 2PU
Country:GREAT BRITAIN
Phone Number:44-1332-349094
Fax Number:44-1332-371237
Email:sales@med-lab.co.uk
Internet:www.med-lab.co.uk
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
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: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:IE249
Supply Number:CoMat 05-028
Type:sp01
Supply Short Name:CoMat 05-028 METALLIC SHOT (CAST STEEL), S230
Supply Name:CoMat 05-028 METALLIC SHOT (CAST STEEL), S230
Specification Groups:
Doc NumberType
AMS 2431/1 ASR 230
Suppliers:
ManufacturerRemarks
IE249
K0247
55807
Manufacturer Code:K6835
Supply Number:CoMat 05-106
Type:sp01
Supply Short Name:CoMat 05-106 ABRASIVE STONE
Supply Name:CoMat 05-106 ABRASIVE STONE
Specification Groups:
Doc NumberType
(SS-S-736/2/26) (A-A-3068/2-26)SQUARE FINE SS-S-736 TYPE II CLASS A1
Suppliers:
ManufacturerRemarks
K6835
KC1D9
Manufacturer Code:X222X
Supply Number:CoMat 06-022
Type:sp01
Supply Short Name:CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY)
Supply Name:CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY)
Specification Groups:
Doc NumberType
ARDROX 985-P14 OMAT: 652 (CHEMETALL OAKITE 985-P14)It is not permitted to mix the selected CoMat 06‐022 letter suffix material with other CoMat 06‐022 letter suffix materials. Where CoMat 06‐022 is specified with no suffix, use one of the CoMat 06‐ 022 letter suffix materials. 
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Tool Number:Binoculars
Tool Name:Binoculars
Manufacturer Code:LOCAL
Tool Number:Chemical cleaning equipment
Tool Name:Chemical cleaning equipment
Manufacturer Code:LOCAL
Tool Number:Glass bead peening equipment
Tool Name:Glass bead peening equipment
Manufacturer Code:0AM53
Tool Number:IAE 3R19465
Tool Name:IAE 3R19465 Shot Peen Fixture
Manufacturer Code:0AM53
Tool Number:IAE 3R19466
Tool Name:IAE 3R19466 Almen Plate Carrier
Manufacturer Code:0AM53
Tool Number:IAE 3R19468
Tool Name:IAE 3R19468 Almen Plate Holder
Manufacturer Code:LOCAL
Tool Number:Penetrant crack test equipment
Tool Name:Penetrant Crack Test Equipment
Manufacturer Code:LOCAL
Tool Number:Shot peening equipment
Tool Name:Shot peening equipment
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