TASK 72-32-85-300-022 Fan Case - Replace The Attrition Linings, Repair-022 (VRS1538)

DMC:V2500-A1-72-32-8501-07A-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

V2500-A1

Common Information

TASK 72-32-85-300-022 Fan Case - Replace The Attrition Linings, Repair-022 (VRS1538)

Effectivity

FIG/ITEM

PART NO.

01-100

5W0124

01-100

5W0168

01-100

5W0171

01-100

5W0191

01-100

5W0192

01-100

5W0193

01-100

5W0206

01-100

5W0207

01-100

5W0208

01-100

5W0214

01-100

5W0215

01-100

5W0216

01-100

5W0306

General

This TASK gives the procedure for repair by replacement of the attrition linings. Attrition lining panel sections can be replaced individually. Partial replacement of a panel section by cutting is not permitted. If an area of a panel section is damaged beyond limits then the whole section must be replaced.

Throughout this repair cleanliness must be maintained. Dirt or grease on bonding surfaces will result in poor adhesion and unsatisfactory bonds. Clean cotton or polythene gloves must be worn by all personnel handling parts to be bonded. Handling must be kept to a minimum and components must not be handled on prepared surfaces.

Adhesive curing is accomplished at ambient temperature or above using mechanical clamping or a vacuum bag to secure the replacement linings.

To get good bonding, care must be taken on preparing properly abraded surfaces and proper use of adhesive.

Material of components

PART IDENT

SYMBOL

MATERIAL

Casing

-

Titanium alloy

Attrition linings

-

Aluminum honeycomb

Attrition linings

-

Glass reinforced composite

Attrition linings

-

Filling compound

Attrition linings

-

Non-metallic honeycomb

Price and availability - refer to IAE

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

NOTE

To identify 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
Air hammersLOCALAir hammer
Air grinderLOCALAir grinder
Flux chippersLOCALFlux chippers
Vacuum bag material and sealant tapeLOCALVacuum bag material and sealant tape
Hand toolsLOCALTools, hand
Putty knifeLOCALPutty knife
Vacuum pumpLOCALVacuum pump
Ultrasonic leak detectorLOCALUltrasonic leak detector
Vacuum cleanerLOCALVacuum cleaner
Vacuum valveLOCALVacuum valve
Blasting equipmentLOCALBlasting equipment
IAE 3J13052 Fixture, bonding0AM53IAE 3J130521

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-097 LINT-FREE GLOVESLOCALCoMat 02-097
CoMat 02-099 LINT-FREE CLOTHLOCALCoMat 02-099
CoMat 02-100 GLOVES, LINT-FREELOCALCoMat 02-100
CoMat 02-166 BREATHER CLOTHLOCALCoMat 02-166
CoMat 02-222 BAGGING FILMLOCALCoMat 02-222
CoMat 02-223 RELEASE FILMLOCALCoMat 02-223
CoMat 02-224 SILICONE ADHESIVE POLYESTERTAPELOCALCoMat 02-224
CoMat 02-225A TAPE, VACUUM BAG SEALANT53309CoMat 02-225A
CoMat 02-334 POROUS RELEASE FILMLOCALCoMat 02-334
CoMat 05-003 ABRASIVE MEDIUM ALUMINUM OXIDE, 120/220 GRADELOCALCoMat 05-003
CoMat 05-016 GARNET PAPER, 80-GRITLOCALCoMat 05-016
CoMat 05-185 POLISHING DISCSK0993CoMat 05-185
CoMat 05-186 CONDITIONING DISCSLOCALCoMat 05-186
CoMat 08-006 FILLER, TWO PACKLOCALCoMat 08-006
CoMat 08-154A SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHERLOCALCoMat 08-154A
CoMat 08-155 ADHESION PROMOTERLOCALCoMat 08-155
CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHERLOCALCoMat 08-154
CoMat 02-225 TAPE, VACUUM BAG SEALANT85670CoMat 02-225
CoMat 05-020 WATERPROOF SILICON CARBIDELOCALCoMat 05-020

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Lining, A/O attrition5R0182AR
Lining, A/O attrition5R0274AR
Lining, A/O attrition5R0310AR

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-85-350-087 Prepare the Bonding Surfaces

    1. Refer to Figure and Figure.

    2. Prepare the bonding surface, refer to Figure.

      3. CAUTION

        DO NOT USE POWERED TOOLS WITH STEEL CHISEL OR SIMILAR BITS.

        CAUTION

        THE FAN CASE IS MADE FROM TITANIUM ALLOY AND IS THIN IN SOME AREAS. IF YOU HIT THE FAN CASE WITH A CHISEL OR SCRAPER YOU CAN MAKE IT UNSERVICEABLE.

        CAUTION

        YOU MUST USE THE CHISEL, SHARP BLADE OR SCRAPER IN A CIRCUMFERENTIAL DIRECTION TO PREVENT THE EDGES OF THE BLADE SCORING THE FAN CASE.

        CAUTION

        YOU MUST ALWAYS TRY TO POINT THE CHISEL OR SHARP BLADE PARALLEL WITH THE SURFACE OF THE FAN CASE.

        CAUTION

        DO NOT OPERATE WITHOUT SAFETY GOGGLES AND OTHER GUARDS EQUIPMENT. FLYING PARTICLES CAN CAUSE INJURY.

        Remove most of the damaged linings.

      1. Use air hammer or flux chipper with aluminum chisel.

      2. Refer to Figure.

      4. CAUTION

        PREVENT TOO MUCH SURFACE ABRASION OF THE FAN CASE MATERIAL. SURFACE FINISH USING ABRASIVE BLASTING IS NECESSARY. THIS WILL GIVE THE BEST BONDING RESULTS.

        CAUTION

        HAND DRESSING TOOLS ARE NOT TO BE USED AT THE SAME LOCATION, DO NOT DWELL IN ONE AREA OR ANY AREA.

        Remove the remaining unwanted material and adhesive on the case.

      2. Make sure new replacement linings can be placed in the position shown in Figure.

    5. WARNING

      AIR BLASTS CREATE FLYING PARTICLES. YOU MUST USE SAFETY SHIELD AND OTHER PROTECTIVE EQUIPMENT. FLYING PARTICLES CAN CAUSE EYE INJURY.

      Remove the remaining debris with dry air blast and/or vacuum cleaner.

      6. Degrease the repair area.

      1. Refer to the SPM TASK 70-11-26-300-503.

      7. WARNING

        ALWAYS MAKE SURE THAT THERE IS SUFFICIENT VENTILATION IN THE WORK AREA.

        WARNING

        EYE PROTECTION MUST ALWAYS BE USED.

        WARNING

        DO NOT LET THE SOLVENT CLEANER OR ITS VAPOR TOUCH THE EYES OR SKIN.

        WARNING

        PROTECTIVE CLOTHING AND FACE MASKS MUST ALWAYS BE USED.

        WARNING

        ALWAYS KEEP OPEN FLAMES AWAY FROM THE WORK AREA.

        WARNING

        IT IS THE RESPONSIBILITY OF THE OPERATOR TO OBTAIN AND OBSERVE THE MANUFACTURERS MATERIAL SAFETY DATA SHEETS FOR CONSUMABLE MATERIALS INFORMATION SUCH AS, HAZARDOUS INGREDIENTS, PHYSICAL/CHEMICAL CHARACTERISTICS, FIRE, EXPLOSION, REACTIVITY, HEALTH HAZARD DATA, PRECAUTIONS FOR SAFE HANDLNG, USE AND CONTROL MEASURES AND ALSO TO TAKE LOCAL REGULATIONS IN TO CONSIDERATION.

        Inspect the repair area.

      1. Examine the surface.

      2. Any nicks, dents, scratches and gouges, repair the damage.

      3. If necessary, do Repair, VRS1554, TASK 72-32-85-300-016 (REPAIR-016).

      8. Make the bonding area.

      1. Mask off all areas except the bonding area with CoMat 02-224 SILICONE ADHESIVE POLYESTERTAPE and/or other applicable procedures.

      9. WARNING

        A PRESSURIZED AIR STREAM CAN CAUSE INJURY. WEAR SAFETY GOGGLES AND PROTECTIVE CLOTHING.

        Make the repair area rough.

      2. Remove the glossy surface from the repair area of the fan case.

      3. Ensure that a constant matt surface is maintained.

      4. Operate vacuum sand blaster at approximately 70 to 100 psi (480 to 690 kPa).

      5. If you use the pressure blaster to remove the glossy surface from the repair area.

      6. Optimum distance between the nozzle and the repair surface is 5 to 15 in. (127 to 381 mm).

      7. Do the procedure given in the SPM TASK 70-36-02-360-501.

      8. Do not use abrasive paper.

      10. Remove any remaining debris.

      1. Use vacuum cleaner.

      11. Immediately blow out the area.

      1. Use oil free dry air.

      12. CAUTION

        DO NOT USE TAP WATER AND MINERAL WATER. YOU MUST USE DISTILLED OR DEIONIZED WATER DURING THE WATER-BREAK INSPECTION.

        Water-break inspection of the repair area.

      1. Refer to the SPM TASK 70-36-02-360-501.

    2. SUBTASK 72-32-85-360-070-001 Bond the Replacement Linings (Vacuum Bag Method)

    2. Degrease the replacement linings and casing, refer to Figure and Figure.

      3. WARNING

        DO NOT GET CLEANING FLUID ON YOUR SKIN OR IN YOUR EYES. PUT ON PROTECTIVE CLOTHING, GOGGLES AND A FACE MASK. USE THE FLUID IN A WELL VENTILATED AREA. DO NOT BREATHE THE VAPOR. IF YOU GET THE CLEANING FLUID ON YOUR SKIN OR IN YOUR EYES, FLUSH IT AWAY WITH WATER. GET MEDICAL AID IF YOUR SKIN OR EYES BECOME IRRITATED.

        NOTE

        Always pour cleaning fluid on the cloth to avoid contaminating the cleaning fluid supply. Wash one small area at a time.
        It is important that the surface is dried with a second clean cloth prior to the cleaning fluid evaporating to prevent the redeposition of contaminants on the fan case surface.

        Remove all grease from the linings and casings.

      1. Refer to the SPM TASK 70-11-26-300-503.

      4. Apply adhesion promoter, refer to Figure and Figure.

        1. WARNING

          YOU MUST FIND AND OBEY THE MANUFACTURER'S HEALTH AND SAFETY DATA FOR THE MATERIAL (MSDS). YOU MUST ALSO REFER TO LOCAL REGULATIONS TO MAKE SURE THAT THE PROCEDURES ARE DONE SAFELY. IF YOU DO NOT DO THIS, AN INJURY OR ENVIRONMENTAL DAMAGE CAN OCCUR.

          Apply the primer.

        1. NOTE

          If primed surface contaminated or bonding is not accomplished within eight hours after application of the adhesion promoter, repeat priming procedure.

          Apply a thin coat of CoMat 08-155 ADHESION PROMOTER to the cleaned surface by brush or clean gauze and allow to dry for approximately 30 minutes at room temperature.

      5. Apply the sealant, refer to Figure, Figure.

        1. WARNING

          YOU MUST FIND AND OBEY THE MANUFACTURER'S HEALTH AND SAFETY DATA FOR THE MATERIAL (MSDS). YOU MUST ALSO REFER TO LOCAL REGULATIONS TO MAKE SURE THAT THE PROCEDURES ARE DONE SAFELY. IF YOU SO NOT DO THIS, AN INJURY OR ENVIRONMENTAL DAMAGE CAN OCCUR.

          CAUTION

          DO NOT USE CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER SEALANT (PR2001B-1/2). THIS MATERIAL IS 30 MINUTES APPLICATION LIFE TYPE SEALANT. THIS BONDING STEP IS ESTIMATED TO TAKE MORE THAN 1 HOUR WHEN DONE BY SKILLED MECHANICS FAMILIARIZED WITH THIS APPLICATION PROCEDURE.

          NOTE

          You must use the plastic gloves, during preparation and use of the sealant, to prevent contamination of the skin.
          Application life is dependent upon ambient environmental conditions. Increases in temperature and low humidity will shorten application time. Conversely, lower temperatures and high humidity will increase application life. For the examples, the life of the mixed sealant is approximately two hours, at 77 deg F (25 deg C) and 50 percent relative humidity.

          Prepare the sealant.

        1. Use CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER. Weigh out 100 parts of base compound (white compound) and 18.5 parts of curing compound (black compound). When using SEMKIT form sealant, prepare either by hand, or using a mixing machine as described in the manufacturer's leaflet. Mix the two parts by kneading until the color of compound is constant quality. No streaks permitted.

        2. Apply a thin layer of sealant to the hook.

        1. Use air powered sealant gun or putty knife. Be careful not to touch prepared surface.

        3. NOTE

          In order to ensure that front attrition area of the panel honeycomb has contact with the surface of the sealant it is necessary to apply the sealant to the maximum specified thickness 0.118 in. (3.0 mm). The sealant layer thickness must not fall below the specified minimum 0.079 in. (2.0 mm), refer to Figure.
          In order to ensure that rear attrition area (filling honeycomb area) of the panel honeycomb has contact with the surface of the sealant it is necessary to apply the sealant to the maximum specified thickness 0.024 in. (0.61 mm). The sealant layer thickness must not fall below the specified minimum 0.015 in. (0.38 mm), refer to Figure.
          For the best results apply a thin layer of the sealant for rear attrition area but satisfactory results can be achieved with layer as much as 0.02 in. (0.5 mm) thick (for filling honeycomb area only, refer to Figure).
          Wear (CoMat 02-097 LINT-FREE GLOVES) or (CoMat 02-100 GLOVES, LINT-FREE) when you touch the parts.

          Apply the sealant to the bonding surfaces.

        1. Use a putty knife or airpowered sealant gun to apply the sealant to mating surfaces of both components to a thickness of between 0.079 and 0.118 in. (2.0 and 3.0 mm) and between 0.015 and 0.024 in. (0.38 and 0.61 mm), refer to Figure.

      6. NOTE

        If all the attrition linings are to be replaced, circumferential position is free from the initial location. Recommended that there is no joint at the 6 o'clock position.

        Install the replacement linings, refer to Figure, Figure, Figure and Figure.

        1. Put the replacement linings in position and hold with tape.

      7. Secure replacement linings, refer to Figure.

        1. Make-up an annular vacuum bag.

        1. Cover the replacement linings with sheet of CoMat 02-334 POROUS RELEASE FILM that is 3.00in. (76.2 mm) longer than each end of the linings, 3 plies of CoMat 02-166 BREATHER CLOTH and one ply of CoMat 02-223 RELEASE FILM.

        2. Spread over them a sheet of CoMat 02-222 BAGGING FILM between the area of the metal surface of the fan case and the anti-ice impact panels.

        3. Seal the edges of the bagging film to the metal surface of the fan case and the anti-ice impact panels with CoMat 02-225 TAPE, VACUUM BAG SEALANT.

        2. Evacuate the air from the vacuum bag and check for leaks audibly or with an ultrasonic leak detector.

        1. Use a vacuum pump and ultrasonic leak detector.

      3. Apply and maintain a vacuum of 10.2 psi (70 KPa). This must be maintained during the whole cure time.

      8. Cure the sealant.

      1. Allow the CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER to cure for nine hours at ambient temperature 77 deg F to 95 deg F (25 deg C to 35 deg C).

      2. Cure may be hastened by applying heat. CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER can obtain a serviceable cure hardness after four hours at 113 deg F (45 deg C).

      3. If the remaining sealant material after repair exceeds the limit, dress the sealant material with CoMat 05-020 WATERPROOF SILICON CARBIDE, if necessary, refer to Figure and Figure.

    9. Remove the vacuum bags.

    3. SUBTASK 72-32-85-360-070-002 Bond the Replacement Linings

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

    2. Degrease the replacement linings and casings, refer to Figure, Figure and Figure.

      3. WARNING

        DO NOT GET CLEANING FLUID ON YOUR SKIN OR IN YOUR EYES. PUT ON PROTECTIVE CLOTHING, GOGGLES AND A FACE MASK. USE THE FLUID IN A WELL VENTILATED AREA. DO NOT BREATHE THE VAPOR. IF YOU GET THE CLEANING FLUID ON YOUR SKIN OR IN YOUR EYES, FLUSH IT AWAY WITH WATER. GET MEDICAL AID IF YOUR SKIN OR EYES BECOME IRRITATED.

        NOTE

        Always pour cleaning fluid on the cloth to avoid contaminating the cleaning fluid supply. Wash one small area at a time.
        It is important that the surface is dried with a second clean cloth prior to the cleaning fluid evaporating to prevent the redeposition of contaminants on the fan case surface.

        Remove all grease from the linings and casing.

      1. Refer to the SPM TASK 70-11-26-300-503.

      4. Apply adhesion promoter, refer to Figure and Figure.

        1. WARNING

          YOU MUST FIND AND OBEY THE MANUFACTURER'S HEALTH AND SAFETY DATA FOR THE MATERIAL (MSDS). YOU MUST ALSO REFER TO LOCAL REGULATIONS TO MAKE SURE THAT THE PROCEDURES ARE DONE SAFELY. IF YOU DO NOT DO THIS, AN INJURY OR ENVIRONMENTAL DAMAGE CAN OCCUR.

          NOTE

          If primed surface contaminated or bonding is not accomplished within eight hours after application of the adhesion promoter, repeat priming procedure.

          Apply the primer.

        1. Apply a thin coat of CoMat 08-155 ADHESION PROMOTER to the cleaned surface by brush or clean gauze and allow to dry for approximately 30 minutes at room temperature.

      5. Apply the sealant, refer to Figure and Figure.

        1. WARNING

          YOU MUST FIND AND OBEY THE MANUFACTURER'S HEALTH AND SAFETY DATA FOR THE MATERIAL (MSDS). YOU MUST ALSO REFER TO LOCAL REGULATIONS TO MAKE SURE THAT THE PROCEDURES ARE DONE SAFELY. IF YOU DO NOT DO THIS, AN INJURY OR ENVIRONMENTAL DAMAGE CAN OCCUR.

          CAUTION

          DO NOT USE CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER SEALANT (PR2001B-1/2). THIS MATERIAL IS 30 MINUTES APPLICATION LIFE TYPE SEALANT. THIS BONDING STEP IS ESTIMATED TO TAKE MORE THAN 1 HOUR WHEN DONE BY SKILLED MECHANICS FAMILIARIZED WITH THIS APPLICATION PROCEDURE.

          NOTE

          You must use the plastic gloves, during preparation and use of the sealant, to prevent contamination of the skin.
          Application life is dependent upon ambient environmental conditions. Increases in temperature and low humidity will shorten application time. Conversely, lower temperatures and high humidity will increase application life. For the examples, the life of the mixed sealant is approximately two hours, at 77 deg F (25 deg C) and 50 percent relative humidity.

          Prepare the sealant.

        1. Use CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER. Weigh out 100 parts of base compound (white compound) and 18.5 parts of curing compound (black compound). When using SEMKIT form sealant, prepare either by hand, or using a mixing machine as described in the manufacturer's leaflet. Mix the two parts by kneading until the color of compound is constant quality. No streaks permitted.

        2. Apply a thin layer of sealant to the hook.

        1. Use air powered sealant gun or putty knife.

        2. Be careful not to touch prepared surface.

        3. NOTE

          In order to ensure that front attrition area of the panel honeycomb has contact with the surface of the sealant it is necessary to apply the sealant to the maximum specified thickness 0.118 in. (3.0 mm). The sealant layer thickness must not fall below the specified minimum 0.079 in. (2.0 mm), refer to Figure.
          In order to ensure that rear attrition area (filling honeycomb area) of the panel honeycomb has contact with the surface of the sealant it is necessary to apply the sealant to the maximum specified thickness 0.024 in. (0.61 mm). The sealant layer thickness must not fall below the specified minimum 0.015 in. (0.38 mm), refer to Figure.
          For the best results apply a thin layer of the sealant for rear attrition area but satisfactory results can be achieved with layers as much as 0.02 in. (0.5 mm) thick (for filling honeycomb area only, refer to Figure.
          Wear (CoMat 02-097 LINT-FREE GLOVES) or (CoMat 02-100 GLOVES, LINT-FREE) when you touch the parts.

          Apply the sealant to the bonding surfaces.

        1. Use a putty knife or airpowered sealant gun to apply the sealant to mating surfaces of both components to a thickness of between 0.079 and 0.118 in. (2.0 and 3.0 mm) and between 0.015 and 0.024 in. (0.38 and 0.61 mm), refer to Figure.

      6. NOTE

        If all the attrition linings are to be replaced, circumferential position is free from the initial location. Recommended that there is no joint at the 6 o'clock position.

        Install the replacement linings, refer to Figure, Figure and Figure.

        1. Put the replacement linings in position and hold with tape.

      7. Secure the replacement linings.

      8. NOTE

        Make sure that you monitor the ambient temperature of the sealant and work area with suitable instruments, across all of the lining.
        Make sure the full cure time is used and correct temperature maintained.
        If the curing process is applied for 48 hours at 50 deg F (10 deg C) or more the necessary strength has been secured, regardless of the level of humidity.

        Cure the sealant.

        1. Allow the CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER to cure for nine hours at ambient temperature 77 deg F to 95 deg F (25 deg C to 35 deg C).

        1. Cure may be hastened by applying heat. CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER can obtain a serviceable cure hardness after four hours at 113 deg F (45 deg C).

        2. If the remaining sealant material around the repair exceeds the dimensional limits, dress the sealant material with CoMat 05-020 WATERPROOF SILICON CARBIDE, if necessary. Refer to Figure and Figure.

    9. Remove the bonding fixture.

    4. SUBTASK 72-32-85-360-071 Fill the Lining Honeycomb and Gap around the Replacement Linings

    1. Refer to Figure, Figure and Figure.

      2. Prepare the fillers, refer to Figure, Figure and Figure.

      2. Refer to the SPM TASK 70-36-02-360-501.

      3. Apply the filler into the honeycomb and the gap around the replacement linings, refer to Figure, Figure and Figure.

      1. Slightly overfill using a putty knife or equivalent. Make sure that the repair area is fully filled with no air pockets.

      2. The gradual setting of the filler will support the newly applied filler.

      3. If any sagging is apparent, locally produced supports will be necessary.

      4. NOTE

        Do not use too much water because it will cause the filler to plasticise.

        If necessary to get a smooth finish, apply a small quantity of cold water to the tool to make it moist.

      1. Use putty knife.

      5. Remove unwanted fillers, refer to Figure, Figure and Figure.

      1. Remove all unwanted filler, when it starts to feel hard. Use putty knife or scraper for a burnishing effect.

      6. Cure the filler.

      1. The cure time given in Figure, you can find the cure time and temperature.

    5. SUBTASK 72-32-85-350-130 Dress the Lining

    1. Refer to Figure.

      2. WARNING

        DO NOT INHALE THE DUST. USE A BREATHING PROTECTION MASK DURING THIS OPERATION.

        CAUTION

        THE MAXIMUM TEMPERATURE WHICH CAN BE USED TO CURE THE FILLER IS 140 DEG F (60 DEG C).

        CAUTION

        THE MINIMUM CURE TIME IS ONE HOUR. DO NOT CURE AT A TEMPERATURE LESS THAN 54 DEG F (12 DEG C).

        NOTE

        Make sure the full cure time is used and correct temperature maintained.

        Abrade the lining to produce the required profile, refer to Figure.

      2. Ensure aerodynamic smoothing is produced.

    6. SUBTASK 72-32-85-220-101 Examine the Repaired Area

    1. Refer to Figure and Figure.

      2. Visually and dimensionally examine the repaired area.

      1. Make sure that flatness of filled surface is smooth. Step is acceptable if less than 0.02 in. (0.5 mm).

      2. If necessary do step 7. again, refer to Figure and Figure.

      3. Examine the replacement linings and check for indications of lack of bond by pressing or tapping.

      1. If lack of bond is apparent, do this TASK again.

    7. SUBTASK 72-32-85-350-153 Identify the Repair

      1. Mark VRS1538 adjacent to the part number.

      1. Use the vibration peen method.

      2. Make a permanent mark by the procedures in the SPM TASK 70-09-00-400-501.

    8. Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimensions

    Repair Details and Dimensions

    Figure: Repair Details and Dimension

    Repair Details and Dimension

    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
Link not Found
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:53309
Enterprise Name:SCHNEE-MOREHEAD, AN ITW COMPANY
BU Name:SCHNEE-MOREHEAD, AN ITW COMPANY
Street:111 N. NURSERY ROAD
City:IRVING
State:TX
Zip Code:75060
Country:USA
Phone Number:1-972-554-3945, 1-800-878-7876
Fax Number:1-972-579-3114
Internet:www.trustsm.com
Manufacturer Code:85670
Enterprise Name:RICHMOND TECHNOLOGY INC
BU Name:RICHMOND TECHNOLOGY INC
Street:1897 EAST COTTON AVE
City:REDLANDS
Zip Code:CA 92374-9797
Country:USA
Phone Number:1-909-794-2111
Fax Number:1-909-794-4003
Internet:www.richmond-technology.com
Manufacturer Code:K0993
Enterprise Name:3M (UK) PLC
BU Name:3M (UK) PLC
Street:3M CENTRE, CAIN ROAD
City:BRACKNELL
Zip Code:RG12 8HT
Country:UNITED KINGDOM
Phone Number:44-161-236-8500
Fax Number:44-161-237-6136
Internet:www.mmm.co.uk
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Link not Found
Link not Found
Manufacturer Code:X111X
Supply Number:CoMat 02-097
Type:sp01
Supply Short Name:CoMat 02-097 LINT-FREE GLOVES
Supply Name:CoMat 02-097 LINT-FREE GLOVES
Specification Groups:
Doc NumberType
DELETED. USE COMAT 02-100.
Suppliers:
ManufacturerRemarks
X111X
Manufacturer Code:X222X
Supply Number:CoMat 02-099
Type:sp01
Supply Short Name:CoMat 02-099 LINT-FREE CLOTH
Supply Name:CoMat 02-099 LINT-FREE CLOTH
Specification Groups:
Doc NumberType
WHERE COMAT 02-099 IS SPECIFIED WITH NO SUFFIX, USE COMAT 02-099A OR COMAT 02-099B.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Supply Number:CoMat 02-100
Type:sp01
Supply Short Name:CoMat 02-100 GLOVES, LINT-FREE
Supply Name:CoMat 02-100 GLOVES, LINT-FREE
Specification Groups:
Doc NumberType
MISC 127 (PW REF)WHITE LINT-FREE NYLON INSPECTION/INSPECTOR GLOVES
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:LOCAL
Supply Number:CoMat 02-166
Type:sp01
Supply Short Name:CoMat 02-166 BREATHER CLOTH
Supply Name:CoMat 02-166 BREATHER CLOTH
Specification Groups:
Doc NumberType
RC-3000-10
Suppliers:
ManufacturerRemarks
LOCAL
51563
85670
Manufacturer Code:LOCAL
Supply Number:CoMat 02-222
Type:sp01
Supply Short Name:CoMat 02-222 BAGGING FILM
Supply Name:CoMat 02-222 BAGGING FILM
Specification Groups:
Doc NumberType
HS-8171
Suppliers:
ManufacturerRemarks
LOCAL
IE532
85670
Manufacturer Code:LOCAL
Supply Number:CoMat 02-223
Type:sp01
Supply Short Name:CoMat 02-223 RELEASE FILM
Supply Name:CoMat 02-223 RELEASE FILM
Specification Groups:
Doc NumberType
A-5000
Suppliers:
ManufacturerRemarks
LOCAL
IE532
85670
Manufacturer Code:LOCAL
Supply Number:CoMat 02-224
Type:sp01
Supply Short Name:CoMat 02-224 SILICONE ADHESIVE POLYESTER TAPE
Supply Name:CoMat 02-224 SILICONE ADHESIVE POLYESTERTAPE
Specification Groups:
Doc NumberType
FLASHTAPE 2
Suppliers:
ManufacturerRemarks
LOCAL
IE532
85670
Manufacturer Code:X222X
Supply Number:CoMat 02-225
Type:sp01
Supply Short Name:CoMat 02-225 TAPE, VACUUM BAG SEALANT
Supply Name:CoMat 02-225 TAPE, VACUUM BAG SEALANT
Specification Groups:
Doc NumberType
Where CoMat 02-225 is specified with no suffix or asterisk, use one of the CoMat 02-225 letter suffix alternative materials.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:51563
Supply Number:CoMat 02-225A
Type:sp01
Supply Short Name:CoMat 02-225A TAPE, VACUUM BAG SEALANT
Supply Name:CoMat 02-225A TAPE, VACUUM BAG SEALANT
Specification Groups:
Doc NumberType
SM5160
Suppliers:
ManufacturerRemarks
51563
53309
Manufacturer Code:53912
Supply Number:CoMat 02-334
Type:sp01
Supply Short Name:CoMat 02-334 POROUS RELEASE FILM
Supply Name:CoMat 02-334 POROUS RELEASE FILM
Specification Groups:
Doc NumberType
A5000P3OMAT 2/154 (RR REF)
JCR 302 (JAEC REF)
Suppliers:
ManufacturerRemarks
53912
IE532
Manufacturer Code:X222X
Supply Number:CoMat 05-003
Type:sp01
Supply Short Name:CoMat 05-003 ABRASIVE MEDIUM ALUMINUM OXIDE, 120/220 GRADE
Supply Name:CoMat 05-003 ABRASIVE MEDIUM ALUMINUM OXIDE, 120/220 GRADE
Specification Groups:
Doc NumberType
Use one of the CoMat 05-003 letter suffix alternatives.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:0KHE3
Supply Number:CoMat 05-016
Type:sp01
Supply Short Name:CoMat 05-016 GARNET PAPER, 80-GRIT
Supply Name:CoMat 05-016 GARNET PAPER, 80-GRIT
Specification Groups:
Doc NumberType
GARNET PAPER, CAMI GRIT SIZE 80 GRADE 0 (ANSI B74.18)
Suppliers:
ManufacturerRemarks
0KHE3
1E1X8
LOCAL
C4347
K0993
K2F42
K6835
V571V
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:K0993
Supply Number:CoMat 05-185
Type:sp01
Supply Short Name:CoMat 05-185 POLISHING DISCS
Supply Name:CoMat 05-185 POLISHING DISCS
Specification Groups:
Doc NumberType
JCR-310SCOTCH-BRITE ROLOC DISC ROLOC 3 in. A MED
Suppliers:
ManufacturerRemarks
K0993
28112
Manufacturer Code:LOCAL
Supply Number:CoMat 05-186
Type:sp01
Supply Short Name:CoMat 05-186 CONDITIONING DISCS
Supply Name:CoMat 05-186 CONDITIONING DISCS
Specification Groups:
Doc NumberType
JCR-311SCOTCH-BRITE SURFACE CONDITIONING DISCS
Suppliers:
ManufacturerRemarks
LOCAL
K0993
28112
Manufacturer Code:00BB6
Supply Number:CoMat 08-006
Type:sp01
Supply Short Name:CoMat 08-006 FILLER, TWO PACK
Supply Name:CoMat 08-006 FILLER, TWO PACK
Specification Groups:
Doc NumberType
SCOTCH-WELD EC-3524 B/A
OMAT: 874 (RR REF)
JCR-141 (JAEC REF)
Suppliers:
ManufacturerRemarks
00BB6
76381
94960
K0993
K6835
KF595
U7947
Manufacturer Code:5HCF1
Supply Number:CoMat 08-154
Type:sp01
Supply Short Name:CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER
Supply Name:CoMat 08-154 SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER
Specification Groups:
Doc NumberType
PR-2001 CLASS B-1/2
Suppliers:
ManufacturerRemarks
5HCF1
K6835
KF595
Manufacturer Code:5HCF1
Supply Number:CoMat 08-154A
Type:sp01
Supply Short Name:CoMat 08-154A SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER
Supply Name:CoMat 08-154A SEALANT, TWO PART, EPOXY-CURED POLYTHIOETHER
Specification Groups:
Doc NumberType
PR-2001 CLASS B-2, CERTIFIED TO AMS 3277 TYPE II CLASS B-2
Suppliers:
ManufacturerRemarks
5HCF1
K6835
KF595
Manufacturer Code:5HCF1
Supply Number:CoMat 08-155
Type:sp01
Supply Short Name:CoMat 08-155 ADHESION PROMOTER
Supply Name:CoMat 08-155 ADHESION PROMOTER
Specification Groups:
Doc NumberType
PR-187 ADHESION PROMOTER
Suppliers:
ManufacturerRemarks
5HCF1
K6835
KF595
Manufacturer Code:LOCAL
Tool Number:Air grinder
Tool Name:Air grinder
Manufacturer Code:LOCAL
Tool Number:Air hammer
Tool Name:Air hammers
Manufacturer Code:LOCAL
Tool Number:Blasting equipment
Tool Name:Blasting equipment
Manufacturer Code:LOCAL
Tool Number:Flux chippers
Tool Name:Flux chippers
Manufacturer Code:0AM53
Tool Number:IAE 3J13052
Tool Name:IAE 3J13052 Fixture, bonding
Manufacturer Code:LOCAL
Tool Number:Putty knife
Tool Name:Putty knife
Link not Found
Manufacturer Code:LOCAL
Tool Number:Ultrasonic leak detector
Tool Name:Ultrasonic leak detector
Manufacturer Code:LOCAL
Tool Number:Vacuum bag material and sealant tape
Tool Name:Vacuum bag material and sealant tape
Manufacturer Code:LOCAL
Tool Number:Vacuum cleaner
Tool Name:Vacuum cleaner
Manufacturer Code:LOCAL
Tool Number:Vacuum pump
Tool Name:Vacuum pump
Manufacturer Code:LOCAL
Tool Number:Vacuum valve
Tool Name:Vacuum valve