TASK 72-32-85-300-018 Fan Case - Repair The Attrition Lining Below The GRC Layer, Repair-018 (VRS1557)

DMC:V2500-A0-72-32-8501-05A-610A-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 72-32-85-300-018 Fan Case - Repair The Attrition Lining Below The GRC Layer, Repair-018 (VRS1557)

Effectivity

FIG/ITEM

PART NO.

01-100

5W0124

01-100

5W0168

01-100

5W0171

01-100

5W0191

01-100

5W0192

01-100

5W0193

Material of component

DESCRIPTION

SYMBOL

MATERIAL

Casing

Titanium alloy

Attrition lining

Aluminum honeycomb

Attrition lining

Non-metallic honeycomb

Attrition lining

Glass reinforced composite

Attrition lining

Filling compound

General

Price and availability - Refer to IAE

This Repair scheme gives the procedure for repair of attrition lining by filling with filler and can be applied below the Glass Reinforced Composite (GRC) layer.

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

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Hand held pneumatic grinderLOCALHand held pneumatic grinder
Rotary filesLOCALRotary files
Plastic scraperLOCALPlastic scraper
Putty knifeLOCALPutty knife
Vacuum cleanerLOCALVacuum cleaner

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-076 METHYL ETHYL KETONELOCALCoMat 01-076
CoMat 02-099 LINT-FREE CLOTHLOCALCoMat 02-099
CoMat 05-016 GARNET PAPER, 80-GRITLOCALCoMat 05-016
CoMat 08-006 FILLER, TWO PACKLOCALCoMat 08-006

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-85-350-073 Remove Defective Areas of Damage

      1. CAUTION

        CHECK THE TOTAL REPAIR AREA PRIOR TO STARTING THE REPAIR. DO NOT CARRY OUT REPAIR BY FILLING THE ATTRITION LININGS IF THE TOTAL REPAIRED AREA EXCEEDS 20 PERCENT OF THE TOTAL FAN CASE ATTRITION LINING AREA. THESE REPAIR LIMITS MUST BE APPLIED TO THE FULL DEPTH OF THE GRC LAYER.

        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

        STOP MACHINING AS SOON AS THE FILES, CUTTERS OR MACHINING BITS ARE THROUGH THE LINING MATERIAL. USE A STOP-MACHINING OR SLEEVE OR OTHER PENETRATION LIMITING DEVICE TO PREVENT DAMAGE TO THE CASING MATERIAL.

        CAUTION

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

        CAUTION

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

        NOTE

        Remove the minimum quantity of material necessary to remove all the damage.

        Remove loose and damaged material from repair area.

      2. Use hand held pneumatic grinder and rotary files.

      3. Be careful not to cause damage to the inner surface of the fan case assembly.

      1. NOTE

        These repair limits must be applied to the full depth of GRC layer.

        Examine the GRC layer and check for indications of blistering or lack of bond by pressing or tapping.

      2. Check visually and by tapping.

      3. A hollow sound is indicative of a suspect bond.

      4. Remove any unsound material.

      5. If damage is more than 4 sqin (25.8 sqcm) in front attrition area, Repair, refer to VRS1538 TASK 72-32-85-300-022(REPAIR-022).

      6. Examine the repaired area, ratio not more than 20 percent of total rear attrition area and/or rear attrition area of one segment of attrition lining.

      7. If more than 20 per cent, repair, refer to VRS1538 TASK 72-32-85-300-022 (REPAIR-022).

      1. NOTE

        Remove the minimum quantity of material necessary to remove all damage.

        Cut away the defective area.

      2. Use hand held pneumatic grinder and rotary files.

      3. Be careful not to cause damage to the inner surface of the fan case assembly.

      1. Make rough the repair area.

      1. Remove any remaining debris.

      2. Use vacuum cleaner.

      1. Examine the fan case inner surface of the repair area.

      2. Examine the fan case inner surface. If necessary repair any nicks, dents, scratches and gouges.

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

    1. SUBTASK 72-32-85-110-071 Remove the Grease from the Repair Area

      WARNING

      ALWAYS MAKE SURE THERE IS SUFFICIENT VENTILATION IN THE WORK AREA. EYE PROTECTION MUST ALWAYS BE USED. DO NOT LET THE SOLVENT CLEANER OR ITS VAPOR TOUCH THE EYES OR SKIN. PROTECTIVE CLOTHING AND FACE MASK MUST ALWAYS BE USED. ALWAYS KEEP OPEN FLAMES AWAY FROM THE WORK AREA. IT IS THE RESPONSIBILITY OF THE OPERATOR TO OBTAIN AND OBSERVE THE MANUFACTURERS MATERIAL SAFETY SHEETS FROM THE CONSUMABLE MATERIALS INFORMATION SUCH AS HAZARDOUS INGREDIENTS, PHYSICAL/CHEMICAL CHARACTERISTICS, FIRE, EXPLOSION, REACTIVITY, HEALTH HAZARD DATA, PRECAUTIONS FOR SAFE HANDLING, USE AND CONTROL MEASURES AND ALSO TO TAKE LOCAL REGULATIONS INTO CONSIDERATION.
      1. Fully remove the grease from the area.

      2. Refer to SPM TASK 70-11-26-300-503.

      1. Immediately dry out area with air blast.

      2. Use oil free air.

    1. SUBTASK 72-32-85-360-060 Prepare Filler Material

      1. Measure out materials by weights.

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

      1. Mix the two parts by kneading until the paste is a constant blue color. No streaks permitted.

      2. Use putty knife.

    1. SUBTASK 72-32-85-350-074 Apply Filler Material

      1. Fill the filler slightly more than necessary in the damaged area.

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

      3. Use air powered sealant gun.

      4. Make sure that the repair area is fully filled with no air pockets.

      5. The filler will gradually set.

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

      1. Cure the filler.

      2. The cure times and temperatures are given in Figure.

      1. CAUTION

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

        NOTE

        The minimum cure time is one hour.

        Blend filler to the contours.

      2. Refer to Figure.

      1. Remove debris.

      2. Use vacuum cleaner.

    1. SUBTASK 72-32-85-220-082 Examine the Repair Area

      1. Examine the surface of repair area.

      2. Make sure that the surface is smooth and flat.

      3. A step is acceptable if less than 0.02 in. (0.5 mm).

      4. Refer to Figure.

  1. Figure: Filling repair the attrition lining

    Filling repair the attrition lining

    Figure: Curing chart for filling material (CoMat 08-006)

    Curing chart for filling material (CoMat 08-006)

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 01-076
Type:sp01
Supply Short Name:CoMat 01-076 METHYL ETHYL KETONE
Supply Name:CoMat 01-076 METHYL ETHYL KETONE
Specification Groups:
Doc NumberType
METHYL ETHYL KETONE, TECHNICAL GRADE, CERTIFIED TO BSI BS 1940 OR ASTM D740, OR TT-M-261
Suppliers:
ManufacturerRemarks
LOCAL
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: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: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:LOCAL
Tool Number:Hand held pneumatic grinder
Tool Name:Hand held pneumatic grinder
Link not Found
Manufacturer Code:LOCAL
Tool Number:Putty knife
Tool Name:Putty knife
Manufacturer Code:LOCAL
Tool Number:Rotary files
Tool Name:Rotary files
Manufacturer Code:LOCAL
Tool Number:Vacuum cleaner
Tool Name:Vacuum cleaner