TASK 72-32-03-300-016 Fan Frame - Blend Repair The Rear Wall Window, Repair-016 (VRS1732)

DMC:V2500-A0-72-32-0301-01A-649A-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 72-32-03-300-016 Fan Frame - Blend Repair The Rear Wall Window, Repair-016 (VRS1732)

Effectivity

FIG/ITEM

PART NO.

03-100

5A0230

03-100

5A0256

03-100

5A0267

03-100

5A0349

03-100

5A0362

03-100

5A0363

03-100

5A0364

03-100

5A0365

03-100

5A0366

03-100

5A0395

03-100

5A0397

03-100

5A0399

03-100

5A0401

03-100

5A0403

03-100

5A0405

03-100

5A0407

03-100

5A0409

03-100

5A0856

03-100

5A1047

03-100

5A1049

03-100

5A1062

03-100

5A1064

03-100

5A1066

03-100

5A1068

03-100

5A1167

03-100

5A6592

03-100

5A6596

03-100

5A0083

03-100

5A0359

03-100

5A1070

03-100

5A1072

03-100

5A1074

03-100

5A1763

03-100

5A1764

03-100

5A1765

03-100

5A1766

03-100

5A1767

03-100

5A1768

03-100

5A1769

03-100

5A1770

03-100

5A1771

03-100

5A1772

03-100

5A1773

03-100

5A1774

03-100

5A1775

03-100

5A1776

03-100

5A1777

03-100

5A1778

03-100

5A1779

03-100

5A1780

03-100

5A1781

03-100

5A1782

03-100

5A1783

03-100

5A1784

03-100

5A1785

03-100

5A1786

03-100

5A1787

03-100

5A1788

03-100

5A1789

03-100

5A1790

03-100

5A1791

03-100

5A1792

Material of component

PART IDENT

SYMBOL

MATERIAL

Fabrication Fan Frame Assembly

Titanium alloy

General

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

Price and availability - none

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

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 05-020 WATERPROOF SILICON CARBIDELOCALCoMat 05-020
CoMat 05-021 WATERPROOF SILICON CARBIDE44197CoMat 05-021
CoMat 06-018 FLUORESCENT PENETRANT (POST-EMULSIFIED HIGH SENSITIVITY)37676CoMat 06-018
CoMat 06-032 DRY DEVELOPER37676CoMat 06-032
CoMat 06-045 EMULSIFIER - FLUORESCENT PENETRANT, HYDROPHILICLOCALCoMat 06-045

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-03-350-067 Remove the Cracks from the Rear Wall Window of the Fan Frame Assembly

    1. Refer to Figure.

      2. CAUTION

        WHEELS, STONES AND ABRASIVE PAPERS USED TO DRESS, MAKE SMOOTH OR POLISH A TITANIUM COMPONENT MUST BE OF THE SILICON CARBIDE TYPE. ALUMINUM OXIDE TYPES MUST NOT BE USED.

        CAUTION

        IF MECHANICAL CUTTERS ARE USED, ONLY SMALL CUTS MUST BE MADE TO PREVENT TOO MUCH HEAT.

        Scallop to remove cracks. The maximum depth of the scalloping is 0.275 in. (7.0 mm).

      1. Use an abrasive stone and a hand held pneumatic grinder. Scalloping must be continued until the crack is removed.

      2. Remove material to a minimum depth of 0.079 in. (2.0 mm) below the surface of the crack.

    3. Blend the weld bead.

      4. Hand polish the repaired area. The surface finish of the repaired area must be 63 microinches (1.6 micrometres).

    2. SUBTASK 72-32-03-220-111 Examine the Fan Frame Assembly

    1. Refer to Figure.

    2. Do a visual and dimensional inspection.

    3. SUBTASK 72-32-03-230-064 Examine the Fan Frame Assembly for Cracks

      1. Do a penetrant crack test of the repaired area.

      1. Refer to the SPM TASK 70-23-05-230-501.

      2. Make sure that there are no cracks in the repaired area.

    4. Figure: Fan frame rear wall window - scalloping limits

    Fan frame rear wall window - scalloping limits

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:37676
Enterprise Name:ITW MAGNAFLUX
BU Name:MAGNAFLUX CORPORATION
Street:155 HARLEM AVE
City:GLENVIEW
State:IL
Zip Code:60025
Country:USA
Phone Number:1-847-657-5300
Fax Number:1-847-867-5388
Internet:www.magnaflux.com
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:LOCAL
Enterprise Name:LOCALLY SUPPLIED
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:X222X
Supply Number:CoMat 06-018
Type:sp01
Supply Short Name:CoMat 06-018FLUORESCENT PENETRANT (POST-EMULSIFIED HIGH SENSITIVITY)
Supply Name:CoMat 06-018 FLUORESCENT PENETRANT (POST-EMULSIFIED HIGH SENSITIVITY)
Specification Groups:
Doc NumberType
It is not permitted to mix the selected CoMat 06‐018 letter suffix material with other CoMat 06‐018 letter suffix materials. Where CoMat 06‐018 is specified with no suffix, use one of the CoMat 06‐018 letter suffix materials.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:37676
Supply Number:CoMat 06-032
Type:sp01
Supply Short Name:CoMat 06-032 DRY DEVELOPER
Supply Name:CoMat 06-032 DRY DEVELOPER
Specification Groups:
Doc NumberType
ZYGLO ZP-4B
Suppliers:
ManufacturerRemarks
37676
Manufacturer Code:X222X
Supply Number:CoMat 06-045
Type:sp01
Supply Short Name:CoMat 06-045 EMULSIFIER - FLUORESCENT PENETRANT, HYDROPHILIC
Supply Name:CoMat 06-045 EMULSIFIER - FLUORESCENT PENETRANT, HYDROPHILIC
Specification Groups:
Doc NumberType
USE THE COMAT 06‐045 LETTER SUFFIX MATERIAL THAT IS APPLICABLE TO THE APPLIED PENETRANT. REFER TO THE APPLICABLE SPM FPI TASK.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Tool Number:Hand held pneumatic grinder
Tool Name:Hand held pneumatic grinder