TASK 73-13-41-300-006 Fuel Nozzle And Support Assembly - Replace The Hardface On The Outer Swirler, Repair-006 (VRS3163)

DMC:V2500-A0-73-13-4100-00A-609A-C|Issue No:006.00|Issue Date:2020-08-01

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 73-13-41-300-006 Fuel Nozzle And Support Assembly - Replace The Hardface On The Outer Swirler, Repair-006 (VRS3163)

Effectivity

FIG/ITEM

PART NO.

01-020

2A0994

01-020

2A1637

01-020

2A2250

01-020

2A3448

01-020

2A3453

Material of Component

PART IDENT

MATERIAL

Fuel nozzle and support assembly

Corrosion and heat resistant alloy

General

Price and Availability - Refer to IAE.

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

NOTE

To identify the consumable materials, refer to the PCI.

Preliminary Requirements

Pre-Conditions

Action/ConditionData Module/Technical Publication
Make sure all the necessary cleaning and inspection procedures are done before this repair.

Support Equipment

NONE

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 03-066 METAL SPRAYING POWDER, 75 CHROMIUM CARBIDE/25 (80 NICKEL - 20 CHROMIUM ALLOY), FINEDK026CoMat 03-066
CoMat 03-096 PLASMA SPRAY POWDERLOCALCoMat 03-096

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 73-13-41-380-001 Prerequisites

      1. Apply a mask and plug as necessary.

      1. Refer to Figure for the areas to be masked and plugged to prevent the internal cavities of the nozzle assembly from being exposed to foreign materials.

      2. Refer to SPM TASK 70-38-24-380-501.

    2. SUBTASK 73-13-41-330-001 Remove wear and/or existing coating from the Outer Air Swirler

      1. Remove all coat and wear from the Fuel Nozzle and Support Assembly Outer Air Swirler to the limits given in Figure and by one or more of the procedures that follow:

        1. CAUTION

          REMOVAL OF IAE 53-5 COAT BY MANUAL GRIT BLAST PROCEDURE IS NOT PERMITTED.

          Grind to remove IAE 53-5 plasma coating from the Outer Air Swirler.

        1. Refer to SPM TASK 70-32-07-100-501. Remove minimum amount of material necessary to do the repair.

        2. Remove the IAE 53-5 coat from the Outer Air Swirler by using a fully automated grit blast process. Send the Fuel Nozzle and Support Assembly to an approved source given below for removal of IAE 53-5 coat by automated grit blast.

        1. The Source Demonstration requirements of this repair mean that any facility not authorized to accomplish this repair either utilize the Authorized Repair Vendors listed below or contact IAE Manager Maintenance Operations to determine if a qualification program can be initiated at their facility.

          IAE - International Aero Engines AG

          400 Main Street, Mail Stop 121-10

          East Hartford, CT 06118

          USA

          Email: gpiaecomms@iaev2500.com

          ATTN: Manager, Maintenance Operations

        2. Authorized repair vendor for Repair VRS3163 is listed below:

          Combustor Airmotive Services

          10 Loyang Lane - Mail Stop 107-18

          Singapore 508916

          Tel: 65 65493811

          Fax: 65 65421409

        3. The designation by IAE of an authorized repair vendor indicates that the repair vendor has demonstrated the necessary capability to enable it to carry out the listed repair work. However, IAE makes no warranties or representations concerning the qualifications or quality standards of the repair vendors to carry out the repair work and accepts no responsibility whatsoever for any work that may be carried out by a repair vendor, other than when IAE is listed as the repair vendor. Authorized repair vendors do not act as agents or representatives of IAE.

      2. If necessary, remove the remaining damage and base coat by machining or grind operation.

      1. Refer to SPM TASK 70-32-07-100-501. Remove minimum amount of material necessary to do the repair.

    3. SUBTASK 73-13-41-110-001 Clean the Fuel Nozzle and Assembly

      1. Clean the Outer Air Swirler.

      1. Refer to SPM TASK 70-11-03-300-503.

    4. SUBTASK 73-13-41-230-001 Do a Fluorescent Penetrant Inspection of the Repair Area if Grinding was Performed

      1. If grinding was performed, do a fluorescent penetrant inspection of the repair area.

      2. Use medium sensitivity, water washable.

      3. No cracks permitted.

    5. SUBTASK 73-13-41-220-095 Do a Visual Inspection of the Outer Air Swirler

      1. Do a visual inspection of the Outer Air Swirler.

      1. Inspect for complete removal of coat.

    6. SUBTASK 73-13-41-220-002 Do a Dimensional Inspection of the Outer Air Swirler

      1. Do a dimensional inspection of the Outer Air Swirler.

        1. Refer to Figure.

        1. If Index 5 in Figure is 1.233 in. - 1.247 in. (31.319 mm - 31.673 mm), do the procedure given in Step to Step.

        2. If Index 5 in Figure is 1.247 in. - 1.257 in. (31.674 mm - 31.927 mm), do the procedure given in Step to Step.

    7. SUBTASK 73-13-41-380-002 Prepare the Outer Air Swirler for Base Coat

      1. Prepare the repair area for base coat.

      1. Refer to Figure and Figure.

      2. Refer to SPM TASK 70-34-18-380-501.

      3. Grit blast out of the repair area is not permitted. Use masks or maskants.

    8. SUBTASK 73-13-41-340-001 Apply Base Coat to the Outer Air Swirler

      1. Coat the repair area by IAE 53-47.

      1. Refer to Figure.

      3. Coat out of the repair area is not permitted. Coat to a sufficient thickness to allow for finishing.

      2. Dry machine or dry grind the base coat.

      1. Refer to Figure.

      2. Finish coat thickness must be 0.003 in. - 0.012 in. (0.077 mm - 0.304 mm) thick. Refer to SPM TASK 70-32-07-100-501. No cutting fluids are permitted. Blend edges of the build-up to the initial contour of the parent material.

    9. SUBTASK 73-13-41-340-002 Apply Top Coat to the Outer Air Swirler

      1. Prepare the repair area for coat.

      1. Refer to Figure and Figure.

      2. Refer to SPM TASK 70-34-18-380-501.

      3. Grit blast out of the repair area is not permitted. Use masks or maskants.

      2. Coat the repair area by IAE 53-5.

      1. Refer to Figure.

      3. Coat out of the repair area is not permitted. Coat to a sufficient thickness to allow for finishing.

      3. Finish grind the repaired area.

      1. Refer to Figure.

      2. Finish coating thickness must be 0.002 - 0.006 inch (0.051 - 0.152 mm). Refer to SPM TASK 70-32-07-100-501.

    10. SUBTASK 73-13-41-110-002 Remove Masks or Maskants or Plugs from the Outer Air Swirler

    1. Remove masks or maskants by SPM TASK 70-34-18-380-501.

    11. SUBTASK 73-13-41-110-003 Clean the Outer Air Swirler

      1. Clean the Outer Air Swirler.

      1. Refer to SPM TASK 70-11-03-300-503.

    12. SUBTASK 73-13-41-220-002 Examine the Plasma Coating on the Outer Air Swirler

      1. Examine the coating after repair by IAE 53.

      1. Refer to SPM TASK 70-34-03-340-501.

    13. SUBTASK 73-13-41-220-003 Do a Dimensional Inspection of the Fuel Nozzle and Support Assembly

      1. Do a dimensional inspection of the Fuel Nozzle and Support Assembly.

      1. Refer to Figure and Figure.

      2. Refer to TASK 73-13-41-200-200 (INSPECTION-000).

    14. Figure: Mask the Fuel Nozzle and Support Assembly

    Mask the Fuel Nozzle and Support Assembly

    Figure: Fuel Nozzle and Support Datums

    Fuel Nozzle and Support Datums

    Fuel Nozzle and Support Datums

    Figure: Apply Base Coat On The Outer Air Swirler

    Apply Base Coat On The Outer Air Swirler

    Apply Base Coat On The Outer Air Swirler

    Figure: Apply Topcoat IAE 53-5 On The Outer Air Swirler

    Apply Topcoat IAE 53-5 On The Outer Air Swirler

    Apply Topcoat IAE 53-5 On The Outer Air Swirler

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Deleted consumables CoMat 03-089, 03-101 and revised the replacement procedure. (13VC013A)

Manufacturer Code:DK026
Enterprise Name:STARCK GMBH AND CO KG
BU Name:STARCK GMBH AND CO KG
Street:IM SCHLEEKE 78-91
City:38642 GOSLAR
Country:GERMANY
Phone Number:49-5321-7510
Fax Number:49-5321-7516 192
Internet:www.hcstarck.com
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:DK026
Supply Number:CoMat 03-066
Type:sp01
Supply Short Name:CoMat 03-066 METAL SPRAYING POWDER, 75 CHROMIUM CARBIDE/25 (80 NICKEL - 20 CHROMIUM ALLOY), FINE
Supply Name:CoMat 03-066 METAL SPRAYING POWDER, 75 CHROMIUM CARBIDE/25 (80 NICKEL - 20 CHROMIUM ALLOY), FINE
Specification Groups:
Doc NumberType
AMS 7875 (PW REF)AMPERIT 585.435
Suppliers:
ManufacturerRemarks
DK026
Manufacturer Code:LOCAL
Supply Number:CoMat 03-096
Type:sp01
Supply Short Name:CoMat 03-096 PLASMA SPRAY POWDER
Supply Name:CoMat 03-096 PLASMA SPRAY POWDER
Specification Groups:
Doc NumberType
AMPERIT 298.442 OR AMPERIT 299.442
Suppliers:
ManufacturerRemarks
LOCAL
IAE15
IE252