TASK 72-32-85-300-037 Fan Case - Repair The Anti-Ice Impact Panels, Repair-037 (VRS1821)

DMC:V2500-A0-72-32-8501-11A-610A-C|Issue No:003.00|Issue Date:2019-05-01

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 72-32-85-300-037 Fan Case - Repair The Anti-Ice Impact Panels, Repair-037 (VRS1821)

Effectivity

FIG/ITEM

PART NO.

01-100

5W0144

01-100

5W0149

01-100

5W0154

01-100

5W0169

01-100

5W0172

01-100

5W0194

01-100

5W0195

01-100

5W0196

01-100

5W0197

01-100

5W0198

01-100

5W0217

01-100

5W0218

01-100

5W0219

01-100

5W0220

01-100

5W0221

01-100

5W0222

01-100

5W0223

01-100

5W0224

01-100

5W0225

01-100

5W0226

01-100

5W0307

01-100

5W0313

Material of component

PART IDENT

SYMBOL

MATERIAL

Casing

Titanium alloy

Anti-ice impact panel

Filling compound

Anti-ice impact panel

Aluminum alloy honeycomb

Anti-ice impact panel

Glass reinforced composite

General

Price and availability - Refer to IAE

The Repair scheme gives the procedure for the repair of anti-ice impact panels, by filling with blue filler.

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

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Hand held pneumatic grinderLOCAL
Rotary filesLOCAL
Sealant gunLOCAL

Air powered

Putty knifeLOCAL
Vacuum cleanerLOCAL

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-031 ACETONE (CH3)2COLOCALCoMat 01-031
CoMat 01-076 METHYL ETHYL KETONELOCALCoMat 01-076
CoMat 01-124 ISOPROPYL ALCOHOLLOCALCoMat 01-124
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
CoMat 08-024 SEALANT23354CoMat 08-024
CoMat 08-142 POLYSULPHIDE COMPOUNDLOCALCoMat 08-142

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-85-350-090 Remove Defective Area of Damage

      1. CAUTION

        CHECK THE TOTAL REPAIR AREA PRIOR TO STARTING THE REPAIR. DO NOT CARRY OUT REPAIR BY FILLING THE ANTI-ICE PANELS IF THE TOTAL REPAIRED AREA EXCEEDS 30 PERCENT OF THE TOTAL FAN CASE ANTI-ICE PANEL AREA.

        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

        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

        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 GUARD EQUIPMENT. FLYING PARTICLES CAN CAUSE INJURY.

        NOTE

        Keep the material removal to the minimum necessary to remove damaged area.

        Cut away area to remove broken pieces or make a hole with grinder or file for filling of filler into the damaged area.

      2. Use hand held pneumatic grinder and rotary files.

      3. Refer to Figure.

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

      1. Examine the Glass Reinforced Composite (GRC) skin and check for indications of blistering or lack of bond by pressing or tapping.

      2. Check visually and by tapping.

      3. A hollow sound indicative of a suspect bond.

      4. Remove any unsound material.

      5. If the repaired area on the ice impact panel exceeds 30 percent of the total area, replace it.

      6. Repair, VRS1841 TASK 72-32-85-300-038 (REPAIR-038).

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

      1. Examine the repaired area ratio.

      2. Repaired area ratio must not be more than 30 percent of one segment of anti-ice impact panel.

      3. If more than 30 percent, replace it.

      4. Repair, VRS1841 TASK 72-32-85-300-038 (REPAIR-038).

      1. Make rough the repair areas.

      1. Remove any remaining debris.

      2. Use vacuum cleaner.

      1. Examine the fan case inner surface of the repaired area, if necessary.

      2. Examine the fan case inner surface, if necessary.

      3. Repair any nicks, dents, scratches and gouges.

      4. If necessary, do Repair, VRS1805 TASK 72-32-85-300-042 (REPAIR-042) or Repair, VRS1818 TASK 72-32-85-300-044 (REPAIR-044).

    1. SUBTASK 72-32-85-110-058 Remove the Grease from the Repair Area

      1. 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 MASKS 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.

        Fully remove the grease from the repair area except the blue filler surface.

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

      1. Immediately dry out area with air blast.

      2. Use oil free dry air.

    1. SUBTASK 72-32-85-360-076 Prepare Filler Material

        1. Measure out materials by weight.

        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. NOTE

          You must use plastic gloves, during preparation and use of the sealant, to prevent contamination of the skin.

          NOTE

          When mixed the life of the filler is approximately half an hour at 77 deg F (25 deg C).

          Prepare the sealant material.

        2. Use CoMat 08-024 SEALANT or CoMat 08-142 POLYSULPHIDE COMPOUND 75 parts of base compound and 10 parts of curing compound (accelerator) by weight.

        3. Mix the two parts by kneading until the compound is a constant color.

        4. No streaks permitted.

    1. SUBTASK 72-32-85-360-077 Apply Filler Material

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

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

      3. Use air powered sealant gun.

      1. CAUTION

        THE MAXIMUM TEMPERATURE WHICH CAN BE USED TO CURE THE FILLER IS 176 deg F (80 deg C).

        Cure the filler.

        1. CAUTION

          THE MAXIMUM TEMPERATURE WHICH CAN BE USED TO CURE THE FILLER MATERIAL (CoMat 08-006 FILLER, TWO PACK) IS 176 deg F (80 deg C).

          Cure the filler, two pack (CoMat 08-006 FILLER, TWO PACK).

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

        1. CAUTION

          THE MAXIMUM TEMPERATURE WHICH CAN BE USED TO CURE THE SEALANT (CoMat 08-024 SEALANT OR CoMat 08-142 POLYSULPHIDE COMPOUND) IS 120 deg F (49 deg C).

          NOTE

          The minimum cure time is one hour.
        2. NOTE

          The minimum cure time is 1.5 hours. Sealant cure times with a relative humidity of 50 percent.

          Cure the sealant for 10 hours at 77 deg F (25 deg C) or 1.5 hours at 113 deg F (45 deg C).

    1. SUBTASK 72-32-85-220-104 Examine the Repair Area

      1. Examine the surface of the repaired area.

      2. Make sure that the shape of the filling surface is smooth and flat.

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

      4. If necessary, do this TASK again.

      5. Refer to Figure.

  1. 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 the effectivity table. (92VJ808F)

Manufacturer Code:23354
Enterprise Name:PRC-DESOTO INTERNATIONAL, INC.
BU Name:PRC-DESOTO INTERNATIONAL, INC.
Department:PPG AEROSPACE DIV.
Street:823 EASTGATE DRIVE, UNIT 4
City:MT. LAUREL,
State:NJ
Zip Code:08054-1202
Country:USA
Phone Number:1-856-234-1600
Fax Number:1-856-234-5515
Internet:www.ppg.com
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 01-031
Type:sp01
Supply Short Name:CoMat 01-031 ACETONE (CH3)2CO
Supply Name:CoMat 01-031 ACETONE (CH3)2CO
Specification Groups:
Doc NumberType
OMAT: 150 (RR REF)COMMERCIAL GRADE O-A-51
PMC 9008 (PW REF)COMMERCIAL GRADE O-A-51
JCR-041 (JAEC REF)COMMERCIAL GRADE O-A-51
MTH 169 (98%) (MTU REF)COMMERCIAL GRADE O-A-51
Suppliers:
ManufacturerRemarks
LOCAL
K6835
81348
K3504
U1185
24853
70657
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:LOCAL
Supply Number:CoMat 01-124
Type:sp01
Supply Short Name:CoMat 01-124 ISOPROPYL ALCOHOL
Supply Name:CoMat 01-124 ISOPROPYL ALCOHOL
Specification Groups:
Doc NumberType
OMAT:1/40GPR TECHNICAL GRADE
PMC 9094GPR TECHNICAL GRADE
JCR-011GPR TECHNICAL GRADE
Suppliers:
ManufacturerRemarks
LOCAL
U1185
24853
K6835
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:23354
Supply Number:CoMat 08-024
Type:sp01
Supply Short Name:CoMat 08-024 SEALANT
Supply Name:CoMat 08-024 SEALANT
Specification Groups:
Doc NumberType
PR-1422B 1/2 JCR-095
Suppliers:
ManufacturerRemarks
23354
Manufacturer Code:X222X
Supply Number:CoMat 08-142
Type:sp01
Supply Short Name:CoMat 08-142 POLYSULPHIDE COMPOUND
Supply Name:CoMat 08-142 POLYSULPHIDE COMPOUND
Specification Groups:
Doc NumberType
Where CoMat 08-142 is specified with no letter suffix or asterisk, use one of the CoMat 08-142 letter suffix alternative materials.
Suppliers:
ManufacturerRemarks
X222X
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