TASK 72-41-13-300-031 HP Compressor Rear Shaft - Repair Surface Damage On The Splines By Hand Dressing - Repair 031 - VRS6516

DMC:V2500-A0-72-41-1301-06A-649A-C|Issue No:001.00|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 72-41-13-300-031 HP Compressor Rear Shaft - Repair Surface Damage On The Splines By Hand Dressing - Repair 031 - VRS6516

Effectivity

FIG/ITEM

PART NO

ASSEMBLY

01-900

6A4151

A

01-900

6A4158

C

01-900

6A5868

C

01-900

6A7708

B

01-900

6A7712

D

01-900

6A7714

D

Material of component

PART IDENTIFICATION

MATERIAL

HP Compressor Rear Shaft

Inconel 718 (QYX)

General

This TASK gives the procedure to repair surface damage on the HP Compressor Splines by hand dressing.

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 72-41-13.

This repair scheme is written in 3 parts.

PART 1 - Dress to X1 Depth.

Hand dress the HP Compressor Rear Shaft Splines to remove damage to the depth of the damage only.

PART 2 - Dress to X2 Depth.

Hand dress the HP Compressor Rear Shaft Splines to remove damage to twice the depth of the damage.

PART 3 - Dress to remove burrs, raised material and sharp edges.

Hand dress the HP Compressor Rear Shaft Splines to remove burrs, raised material and sharp edges.

The depth of the applied dressing must be in accordance with the instructions in the inspection/check, refer to TASK 72-41-13-200-001-C00 or TASK 72-41-13-200-001-D00 or TASK 72-41-13-200-001-E00 or TASK 72-41-13-200-001-F00.

Where a defect affects more than one surface (i.e. is on an edge or corner) the damage must be assessed using the most conservative limits from the affected surfaces.

If dressing is required on an edge or corner all edges created by the dressing process must be broken to maximum 0.005 in. (0.13 mm).

If the repair is to be applied to a spline which has been dressed previously care must be taken to make sure that the depth of the existing dressed area(s) is not increased by the latest application of the repair.

Power tools or hand held power tools are not to be used to repair the component.

No dressing is allowed in the critical fillet radius, refer to Figure. Polishing in accordance with Part 3 may overlap the critical fillet radius.

TASKS identified by SPM TASK are in the standard practices and processes manual.

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 Consumables Index (PCI).

NOTE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Fluorescent Penetrant Inspection EquipmentLOCALFluorescent penetrant inspection equipment
Dimensional inspection equipmentLOCALDimensional inspection equipment
Vibrating marking pencilLOCALVibrating marking pencil
Binocular inspection equipmentLOCALBinocular inspection equipment

X10

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-096 MARKER PENLOCALCoMat 02-096
CoMat 02-124C MARKING INKK6858CoMat 02-124C
CoMat 05-074 ALUMINIUM OXIDE ABRASIVE PAPER06565CoMat 05-074
CoMat 05-106 ABRASIVE STONEK6835CoMat 05-106
CoMat 05-111 EMERY POLISHING PAPER06565CoMat 05-111
CoMat 06-022 FLUORESCENT PENETRANT (POST-EMULSIFIED ULTRA HIGH SENSITIVITY)LOCALCoMat 06-022

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-41-13-210-001 Examine the HP Compressor Rear Shaft

    1. Refer to Figure, Figure and Figure.

      2. Examine the damage on the HP Compressor Rear Shaft.

          1. If the defects are not within the limits or if any of the repair area(s) extend into a critical fillet radius.

          1. Reject.

          2. If the defects are within the limits and the repair will not extend into a critical fillet radius.

          1. Mark the location(s) that are to be repaired and continue with the repair.

      3. Examine the spline end faces for a dot mark from a previous repair.

        NOTE

        The dot mark will only exist if VRS6516 has been applied previously.

        1. lf there is no dot mark on any of the spline end faces.

        1. Continue the repair from Step.

        2. If there is a dot mark on one of the spline end faces.

        1. Continue the repair from Step, Step or Step as necessary.

    2. SUBTASK 72-41-13-210-002 Identify a Reference Spline (If Required)

    1. Refer to Figure and Figure.

      2. If this is the first application of VRS6516 vibro-peen a dot mark on the end face of one of the HP Compressor Rear Shaft Splines to act as a reference.

      1. Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.

      2. NOTE

        To determine the number of the spline being repaired, use the spline with the vibro-peened dot mark as the number 1 spline and count clockwise, viewed from the rear, to the repaired spline.

  3. PART 1- DRESS TO X1 DEPTH

    Hand Dress the HP Compressor Rear Shaft Splines to remove damage to the depth of the damage only.

    4. SUBTASK 72-41-13-350-001 Examine the Component

      CAUTION

      IF THE DAMAGED AREA OF THE SPLINE(S) HAS BEEN REPAIRED PREVIOUSLY IN ACCORDANCE WITH VRS6516 CARE MUST BE TAKEN TO MAKE SURE THAT THE DEPTH OF THE EXISTING DRESSING IS NOT INCREASED.

      CAUTION

      IF THE DEPTH OF ANY EXISTING DRESSING WILL BE INCREASED THE COMPONENT MUST BE REJECTED.

      NOTE

      The number(s) or the spline(s) which have been dressed previously were recorded upon successful completion of VRS6516 to make it easier to identify the repair locations.

      NOTE

      The repaired location(s) on the individual spline(s) and the depth of the dressing were not recorded. Care must be taken during inspection to identify previously repaired locations if further repair is required.

    1. Refer to Figure and Figure.

      2. Determine if the new damage or subsequent dressed area will affect an existing repair.

        1. If the new damage is located at a location which has been dressed previously.

        1. Reject.

        2. If the dressed area(s) for the new damage will overlap a previously dressed area and the conditions of the above cautions are satisfied.

        1. Continue with the repair.

    5. SUBTASK 72-41-13-350-002 Hand Dress the Identified Defect(s)

      CAUTION

      DO NOT USE POWER TOOLS OR HAND HELD POWER TOOLS TO REPAIR THE HP COMPRESSOR REAR SHAFT SPLINES.

      CAUTION

      MAKE SURE THAT ALL BURRS CREATED BY THE DRESSING PROCESS ARE REMOVED.

      2. Hand dress to remove damage from the HP Compressor Rear Shaft Splines.

      2. Dress to X1 times the depth of the defect only.

      4. Remove the minimum amount of material necessary to remove the defect(s).

      5. The minimum dress ratio is 50 to 1. The maximum dress ratio is 100 to 1.

      6. Make sure that radii or chamfers affected by the repair do not decrease in size due to the repair.

        NOTE

        Defects positioned next to each other can be treated as a single defect providing the maximum length-depth ratio is maintained. In case of a combination of defects next to each other which must be dressed to Part 1 and Part 2 where the dressed areas will overlap, the repair must be accomplished in accordance with Part 2.

    6. SUBTASK 72-41-13-220-001 Dimensionally Inspect the Repaired Areas

      1. Dimensionally inspect the repaired area(s) of the HP Compressor Rear Shaft Splines.

          1. If the dressed area overlaps a critical fillet radius.

          1. Reject.

          2. If the dressed areas are in excess of the limits.

          1. Reject.

          3. lf the spline is reduced beyond the minimum actual spline thickness.

          1. Reject.

          4. If all of the indications of damage have been removed and the repair(s) are within the limits and the spline is not less than the minimum actual spline thickness.

          1. Continue with the repair.

    7. SUBTASK 72-41-13-110-001 Swab Etch the Repair Area(s)

      1. Cold ferric chloride swab etch the repair areas on the HP Compressor Rear Shaft Splines.

      1. Refer to SPM TASK 70-11-39-300-503, SUBTASK 70-11-39-300-001.

    8. SUBTASK 72-41-13-230-001 Fluorescent Penetrant Inspect

      1. Inspect for cracking at the repair area on the HP Compressor Rear Shaft Splines using fluorescent penetrant inspection.

      1. Refer to SPM TASK 70-23-05-230-501, SUBTASK 70-23-05-230-002.

          1. If cracking is detected.

          1. Reject.

          2. If no cracking is detected.

          1. Continue with the repair.

    9. SUBTASK 72-41-13-350-003 Polish the Repair Area

      CAUTION

      DO NOT USE POWER TOOLS OR HAND HELD POWER TOOLS TO REPAIR THE HP COMPRESSOR REAR SHAFT.

      1. Polish the repair area(s) on the HP Compressor Rear Shaft Splines.

      1. Hand polish the repair areas.

      2. The surface texture of the repair area(s) on the flanks must be 80 microinches (2.0 micrometres) or better.

      3. The surface texture of the repair area(s) on the top face must be 126 microinches (3.2 micrometres) or better.

    10. SUBTASK 72-41-13-220-002 Bedding Check the Contact Surface (If Required)

    1. Refer to Figure, Figure, Figure and Figure.

      NOTE

      The SUBTASK only needs to be applied if the contact surface of the pressure flank or a combination of the pressure flank and the top face has been dressed in accordance with Part 1 or Part 2 of VRS6516. If the non-pressure flank or just the top face has been dressed then this SUBTASK need not be applied.

      2. Do a bedding check (blue bed check) of the contact surface of the pressure flank of the repaired spline(s).

      1. There must be a minimum of 90% bedding of the pressure flank of the repaired spline(s) after all dressing is complete.

          1. lf there is less than 90% bedding of the contact surface on the pressure flank.

          1. Reject.

          2. lf there is more than 90% bedding of the contact surfaces on the pressure flank.

          1. Continue with the repair.

    11. SUBTASK 72-41-13-350-004 Identify the Repair

    1. Refer to Figure and Figure.

      NOTE

      If the HP Compressor Rear Shaft is already identified with the repair scheme number VRS6516 from a previous repair application, only the number of the repaired splines needs to be added.

      2. Vibro-peen VRS6516 at the indicated location(s) on the HP Compressor Rear Shaft.

      1. Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.

      3. Vibro-peen the number of the repaired spline(s) adjacent to the repair scheme number at the indicated location.

      1. Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.

      2. To determine the spline number, use the spline with the vibro-peened dot mark as number 1 and count clockwise, viewed from the rear, to the repaired spline(s).

      4. Remove raised material, burrs and/or sharp edges at the vibro-peen marking area and the dot mark.

      1. NOTE

        It will only be required to remove raised material, burrs and/or sharp edges from the dot mark location if this is the first application of VRS6516.

  12. PART 2-DRESS TO X2 DEPTH

    Hand dress the HP Compressor Rear Shaft Splines to remove damage to twice the depth of the damage

    13. SUBTASK 72-41-13-210-003 Examine the Component

      CAUTION

      IF THE DAMAGED AREA OF THE SPLINE(S) HAS BEEN REPAIRED PREVIOUSLY IN ACCORDANCE WITH VRS6516 CARE MUST BE TAKEN TO MAKE SURE THAT THE DEPTH OF THE EXISTING DRESSING IS NOT INCREASED.

      CAUTION

      IF THE DEPTH OF ANY EXISTING DRESSING WILL BE INCREASED THE COMPONENT MUST BE REJECTED.

      NOTE

      The number(s) or the spline(s) which have been dressed previously were recorded upon successful completion of VRS6516 to make it easier to identify the repair locations.

      NOTE

      The repaired location(s) on the individual spline(s) and the depth of the dressing were not recorded. Care must be taken during inspection to identify previously repaired locations if further repair is required.

    1. Refer to Figure and Figure.

      2. Determine if the new damage or subsequent dressed area will affect an existing repair.

        1. If the new damage is located at a location which has been dressed previously.

        1. Reject.

        2. If the dressed area(s) for the new damage will overlap a previously dressed area and the conditions of the above cautions are satisfied.

        1. Continue with the repair.

    14. SUBTASK 72-41-13-350-005 Hand Dress the Identified Defect(s)

      CAUTION

      DO NOT USE POWER TOOLS OR HAND HELD POWER TOOLS TO REPAIR THE HP COMPRESSOR REAR SHAFT SPLINES.

      CAUTION

      MAKE SURE THAT ALL BURRS CREATED BY THE DRESSING PROCESS ARE REMOVED.

      2. Hand dress to remove damage from the HP Compressor Rear Shaft Splines.

      2. Dress to X2 times the depth of the defect only.

      4. The minimum dress ratio is 50 to 1. The maximum dress ratio is 100 to 1.

      5. Make sure that radii or chamfers affected by the repair do not decrease in size due to the repair.

        NOTE

        Defects positioned next to each other can be treated as a single defect providing the maximum length-depth ratio is maintained. In case of a combination of defects next to each other which must be dressed to Part 1 and Part 2 where the dressed areas will overlap, the repair must be accomplished in accordance with Part 2.

    15. SUBTASK 72-41-13-220-003 Dimensionally Inspect the Repaired Areas

      1. Dimensionally inspect the repaired area(s) of the HP Compressor Rear Shaft Splines.

          1. If the dressed area(s) overlaps a critical fillet radius.

          1. Reject.

          2. If the dressed area(s) are in excess of twice the limits in the Inspection/Check.

          1. Reject.

          3. lf the spline is reduced beyond the minimum actual spline thickness.

          1. Reject.

          4. If all of the indications of damage have been removed, the repair(s) are within the limits and the spline is not less than the minimum actual spline thickness.

          1. Continue with the repair.

    16. SUBTASK 72-41-13-110-002 Swab Etch the Repair Area(s)

      1. Cold ferric chloride swab etch the repair areas on the HP Compressor Rear Shaft Splines.

      1. Refer to SPM TASK 70-11-39-300-503, SUBTASK 70-11-39-300-001.

    17. SUBTASK 72-41-13-230-002 Fluorescent Penetrant Inspect

      1. Inspect for cracking at the repair area on the HP Compressor Rear Shaft Splines using fluorescent penetrant inspection.

      1. Refer to SPM TASK 70-23-05-230-501, SUBTASK 70-23-05-230-002.

          1. If cracking is detected.

          1. Reject.

          2. If no cracking is detected.

          1. Continue with the repair.

    18. SUBTASK 72-41-13-350-006 Polish the Repair Area(s)

      CAUTION

      DO NOT USE POWER TOOLS OR HAND HELD POWER TOOLS TO REPAIR THE HP COMPRESSOR REAR SHAFT.

      1. Polish the repair area(s) on the HP Compressor Rear Shaft Splines.

      1. Hand polish the repair areas.

      2. The surface texture of the repair area(s) on the flanks must be 80 microinches (2.0 micrometres) or better.

      3. The surface texture of the repair area(s) on the top face must be 126 microinches (3.2 micrometres) or better.

    19. SUBTASK 72-41-13-220-004 Bedding Check the Contact Surface (If Required)

    1. Refer to Figure, Figure, Figure and Figure.

      NOTE

      The SUBTASK only needs to be applied if the contact surface of the pressure flank or a combination of the pressure flank and the top face has been dressed in accordance with Part 1 or Part 2 of VRS6516. If the non-pressure flank or just the top face has been dressed then this SUBTASK need not be applied.

      2. Do a bedding check (blue bed check) of the contact surface of the pressure flank of the repaired spline(s).

      1. There must be a minimum of 90% bedding of the pressure flank of the repaired spline(s) after all dressing is complete.

          1. lf there is less than 90% bedding of the contact surface on the pressure flank.

          1. Reject.

          2. lf there is more than 90% bedding of the contact surfaces on the pressure flank.

          1. Continue with the repair.

    20. SUBTASK 72-41-13-350-007 Identify the Repair

    1. Refer to Figure and Figure.

      NOTE

      If the HP Compressor Rear Shaft is already identified with the repair scheme number VRS6516 from a previous repair application, only the number of the repaired splines needs to be added.

      2. Vibro-peen VRS6516 at the indicated location(s) on the HP Compressor Rear Shaft.

      1. Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.

      3. Vibro-peen the number of the repaired spline(s) adjacent to the repair scheme number at the indicated location.

      1. Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.

      2. To determine the spline number, use the spline with the vibro-peened dot mark as number 1 and count clockwise, viewed from the rear, to the repaired spline(s).

      4. Remove raised material, burrs and/or sharp edges at the vibro-peen marking area and at the dot mark.

      1. NOTE

        It will only be required to remove raised material, burrs and/or sharp edges from the dot mark location if this is the first application of VRS6516.

  21. PART 3 - Dress to Remove Burrs, Raised Material and Sharp Edges.

    Hand dress the HP Compressor Rear Shaft Splines to remove burrs, raised material and sharp edges.

    22. SUBTASK 72-41-13-350-008 Dress the Burrs, Raised Material and/or Sharp Edges at the Repair Area

      CAUTION

      DO NOT USE POWER TOOLS OR HAND HELD POWER TOOLS TO REPAIR THE HP COMPRESSOR REAR SHAFT.

      CAUTION

      MAKE SURE THAT ALL OF THE BURRS CREATED BY THE REPAIR PROCESS ARE REMOVED.

      2. Hand dress to remove burrs, raised material and/or sharp edges from the HP Compressor Rear Shaft splines.

      1. Dress to remove burrs, raised material and sharp edges from the defect/repair area only.

      2. If the dressed area overlaps a corner or chamfer make the edges of the polished area smooth.

      3. Make sure that radii or chamfers affected by the repair do not decrease in size due to the repair.

    23. SUBTASK 72-41-13-220-005 Examine the Dressed Areas

      1. Examine the repaired area(s) of the HP Compressor Rear Shaft Splines.

        1. Make sure that all of the burrs, raised material and sharp edges have been removed and that the repair area(s) has a smooth profile.

          1. lf all of the damage burrs, raised material and sharp edges have not been removed or if the repair area(s) does not have a smooth profile.

          1. Reject.

          2. If all of the damage burrs, raised material and sharp edges have been removed and the repair area(s) has a smooth profile.

          1. Continue with the repair.

      2. If the dressed area overlaps another dressed area.

      1. Accept.

      3. If the dressed area overlaps a critical fillet radius.

      1. Reject.

    24. SUBTASK 72-41-13-110-003 Swab Etch the Repair Area(s)

      1. Cold ferric chloride swab etch the repair areas on the HP Compressor Rear Shaft Splines.

      1. Refer to SPM TASK 70-11-39-300-503, SUBTASK 70-11-39-300-001.

    25. SUBTASK 72-41-13-230-003 Fluorescent Penetrant Inspect

      1. Inspect for cracking at the repair area on the HP Compressor Rear Shaft Splines using fluorescent penetrant inspection.

      1. Refer to SPM TASK 70-23-05-230-501, SUBTASK 70-23-05-230-002.

          1. If cracking is detected.

          1. Reject.

          2. If no cracking is detected.

          1. Continue with the repair.

    26. SUBTASK 72-41-13-350-008 Polish the Repair Area

      1. Hand polish the repair area(s).

      1. Hand polish to achieve the required surface texture.

      2. The surface texture of the repair area(s) on the flanks must be 80 microinches (2.0 micrometres) or better.

      3. The surface texture of the repair area(s) on the top face must be 126 microinches (3.2 micrometres) or better.

    27. SUBTASK 72-41-13-220-006 Examine the Polished Areas

      1. Examine the polished area(s) of the HP Compressor Rear Shaft Splines.

      1. Make sure that all of the burrs, raised material and sharp edges have been removed and that the repair area(s) has a smooth profile and that the required surface finish has been achieved.

          1. lf all of the damage burrs, raised material and sharp edges have not been removed, if the repair area(s) does not have a smooth profile or if the required surface finish has not been achieved.

          1. Reject.

          2. If all of the damage burrs, raised material and sharp edges have been removed, the repair area(s) has a smooth profile and if the required surface finish has been achieved.

          1. Continue with the repair.

      2. If the polished area overlaps another polished area or a critical fillet radius.

      1. Accept.

    28. SUBTASK 72-41-13-350-009 Identify the Repair

    1. Refer to Figure and Figure.

      2. Vibro-peen VRS6516 at the indicated location(s) on the HP Compressor Rear Shaft.

      1. Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.

      3. Remove raised material, burrs and/or sharp edges at the vibro-peen marking area and at the dot mark.

      1. NOTE

        It will only be required to remove raised material, burrs and/or sharp edges from the dot mark location if this is the first application of VRS6516.

    29. Figure: HP Compressor Rear Shaft Splines - Component Details - Assemblies A, B, C and D

    HP Compressor Rear Shaft Splines - Component Details - Assemblies A, B, C and D

    Figure: HP Compressor Rear Shaft Splines - Dot Marking Location and Repair Details - Assemblies A, B, C and D

    HP Compressor Rear Shaft Splines - Dot Marking Location and Repair Details - Assemblies A, B, C and D

    Figure: HP Compressor Rear Shaft Splines - Dressing Ratios and Shapes - Assemblies A, B, C and D

    HP Compressor Rear Shaft Splines - Dressing Ratios and Shapes - Assemblies A, B, C and D

    Figure: HP Compressor Rear Shaft Splines - Repair Areas and Locations - Assemblies A, B, C and D

    HP Compressor Rear Shaft Splines - Repair Areas and Locations - Assemblies A, B, C and D

    Figure: HP Compressor Rear Shaft Splines - Dressing Details and Dimensions - Assemblies A, B, C and D

    HP Compressor Rear Shaft Splines - Dressing Details and Dimensions - Assemblies A, B, C and D

    Figure: HP Compressor Rear Shaft Splines - Dressing Details for the Top Face - Assemblies A, B, C and D

    HP Compressor Rear Shaft Splines - Dressing Details for the Top Face - Assemblies A, B, C and D

    Figure: HP Compressor Rear Shaft Splines - Dressing Details for the End Face - Assemblies A, B, C and D

    HP Compressor Rear Shaft Splines - Dressing Details for the End Face - Assemblies A, B, C and D

    Figure: HP Compressor Rear Shaft Splines - Identity Marking Location - Assemblies A, B, C and D

    HP Compressor Rear Shaft Splines - Identity Marking Location - Assemblies A, B, C and D

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Added blend repair for VRS6516. (15VR819)

Manufacturer Code:06565
Enterprise Name:SAINT-GOBAIN ABRASIVES
BU Name:SAINT-GOBAIN ABRASIVES
P.O. Box:808
City:TROY
State:NY
Zip Code:12181
Country:USA
Phone Number:1-518-266-2200
Fax Number:1-518-266-2342
Internet:www.saintgobain.com
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:K6858
Enterprise Name:CHEMETALL PLC
BU Name:CHEMETALL PLC
Street:65 DENBIGH RD
City:MILTON KEYNES
State:BLETCHLEY
Zip Code:MK1 1PB
Country:GREAT BRITAIN
Phone Number:44-(0) 1908-649333
Fax Number:44-(0)1908-373939
Email:ukinfo@chemetall.com
Internet:www.chemetall.com
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:X111X
Supply Number:CoMat 02-096
Type:sp01
Supply Short Name:CoMat 02-096 MARKER PEN
Supply Name:CoMat 02-096 MARKER PEN
Specification Groups:
Doc NumberType
TEMPORARY MARKS ON COMPONENTS AND ASSEMBLIESDELETED. USE ONE OF THE SPECIFIED MARKERS IN SPM TASK 70-09-01-400-501 PROCEDURE TO MAKE
Suppliers:
ManufacturerRemarks
X111X
Manufacturer Code:K6858
Supply Number:CoMat 02-124C
Type:sp01
Supply Short Name:CoMat 02-124C MARKING INK
Supply Name:CoMat 02-124C MARKING INK
Specification Groups:
Doc NumberType
OMAT: 264DBLUE METAL
Suppliers:
ManufacturerRemarks
K6858
LOCAL
Manufacturer Code:44197
Supply Number:CoMat 05-074
Type:sp01
Supply Short Name:CoMat 05-074 ALUMINIUM OXIDE ABRASIVE PAPER
Supply Name:CoMat 05-074 ALUMINIUM OXIDE ABRASIVE PAPER
Specification Groups:
Doc NumberType
ANSI/CAMI GRIT SIZE 180 ALUMINIUM OXIDE ABRASIVE PAPER
Suppliers:
ManufacturerRemarks
44197
K6835
LOCAL
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:44197
Supply Number:CoMat 05-111
Type:sp01
Supply Short Name:CoMat 05-111 EMERY POLISHING PAPER
Supply Name:CoMat 05-111 EMERY POLISHING PAPER
Specification Groups:
Doc NumberType
FEPA GRIT SIZE P280 OR P240 EMERY POLISHING PAPER OR ALUMINUM OXIDE ABRASIVE PAPER
Suppliers:
ManufacturerRemarks
44197
K6835
KC1D9
LOCAL
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:Binocular inspection equipment
Tool Name:Binocular inspection equipment
Manufacturer Code:LOCAL
Tool Number:Dimensional inspection equipment
Tool Name:Dimensional inspection equipment
Manufacturer Code:LOCAL
Tool Number:Fluorescent penetrant inspection equipment
Tool Name:Fluorescent Penetrant Inspection Equipment
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