TASK 75-32-52-300-001 HPC Stage 7 Bleed Outlet Duct And Seal Assembly - Replace The Rivet(s), Retaining Ring(s) And/Or Seal On The LH Lower Assembly, Repair-001 (VRS6043)

DMC:V2500-A0-75-32-5201-00A-920A-C|Issue No:003.00|Issue Date:2020-02-01

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 75-32-52-300-001 HPC Stage 7 Bleed Outlet Duct And Seal Assembly - Replace The Rivet(s), Retaining Ring(s) And/Or Seal On The LH Lower Assembly, Repair-001 (VRS6043)

Effectivity

FIG/ITEM

PART NO

01-060

6A6533

Material of components

PART IDENT

MATERIAL

Seal retaining ring

Nickel alloy

Seal carrier

Titanium alloy or nickel alloy

Flexible seal duct

Dunlop rubber

Rivet

Corrosion resisting steel

General

This Repair must only be done when the instruction to do so is given in the Inspection-000 TASK 75-32-52-200-100.

This Repair replaces loose and/or damaged rivet(s), damaged retaining ring(s) and/or a damaged seal duct, in the HP compressor stage 7 LH lower air seal assembly.

When loose and/or damaged rivet(s) are to be replaced, go to Step.

When a damaged seal duct or retaining ring(s) is to be replaced, go to Step.

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

TASKs identified by SPM TASK are in the Standard Practices and Processes Manual (SPM).

Price and availability. Refer to International Aero Engines AG.

Related repairs - none

NOTE

Equipment and materials necessary to do this repair are in the SPM TASKS given below:
Refer to SPM TASK 70-09-00-400-501.
Refer to SPM TASK 70-09-01-400-501.
Refer to SPM TASK 70-11-26-300-503.
Refer to SPM TASK 70-23-02-230-501.
Refer to SPM TASK 70-23-05-230-501.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Chemical Cleaning EquipmentLOCALChemical Cleaning Equipment
Penetrant Crack Test EquipmentLOCALPenetrant Crack Test Equipment
Standard Workshop EquipmentLOCALStandard Workshop Equipment
Vertical Drilling MachineLOCALVertical Drilling Machine
Vibro-Engraving EquipmentLOCALVibro-Engraving Equipment
Workshop Inspection EquipmentLOCALWorkshop Inspection Equipment

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 06-064 FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY)LOCALCoMat 06-064

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
RIVET - SOLID UNIVERSAL HEADU1653AS1609012AR

01-080

RIVET - SOLID UNIVERSAL HDU1653AS1613212AR

01-083

Duct - sealK14061012489 or (Supplier PN: ARM944)1

01-086

RING, RETAINING - SEALD33096M11902

01-085

Safety Requirements

NONE

Procedure

    1. SUBTASK 75-32-52-110-059 Clean the Assembly

      1. Chemically clean

      2. Refer to Cleaning TASK 75-32-52-100-100.

    1. SUBTASK 75-32-52-230-066 Do a Crack Test

    1. SUBTASK 75-32-52-323-054 Remove Loose and/or Damaged Rivet(s)

      NOTE

      The SUBTASKS which follow must only be used to replace loose and/or damaged rivet(s).
    2. Refer to Figure and Figure.

      1. Remove loose and/or damaged rivet(s).

      2. Use drill diameter that is smaller than the rivet hole diameter.

    1. SUBTASK 75-32-52-220-066 Examine the Rivet Hole(s)

    2. Refer to Figure and Figure.

      1. Visually examine and measure the diameter of the exposed rivet hole(s).

      2. If diameter of the rivet hole(s) is larger than 0.164 in. (4.175 mm) discard whole silencer assembly.

      3. Mark damaged and oversized rivet holes.

    1. SUBTASK 75-32-52-323-054 Drill the Rivet Hole(s)

    2. Refer to Figure and Figure.

      1. Drill damaged rivet hole(s) to suit the larger rivet(s) as necessary.

      1. Remove the sharp edges around the rivet hole(s).

    1. SUBTASK 75-32-52-110-060 Chemically Clean

      1. Chemically clean around the rivet hole(s).

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

    1. SUBTASK 75-32-52-230-067 Do a Crack Test

      1. Do a local penetrant crack test around the rivet hole(s).

      2. Refer to SPM TASK 70-23-05-230-501.

      3. Cracks are not permitted.

    1. SUBTASK 75-32-52-350-060 Install the Rivet(s)

    2. Refer to Figure and Figure.

      1. Put the rivet(s) in the rivet hole(s) as necessary.

      2. Use AS16090 RIVET - SOLID UNIVERSAL HEAD, 12 max., (75-32-52,01-080) and/or large AS16132 RIVET - SOLID UNIVERSAL HD, 12 max., (75-32-52,01-083) for large holes.

    1. SUBTASK 75-32-52-390-055 Safety the Rivet(s) in Place

    2. Refer to Figure and Figure.

      1. Cold squeeze the rivet(s) in place.

      2. Refer to SPM TASK 70-39-03-390-501.

    1. SUBTASK 75-32-52-110-061 Chemically Clean

      1. Chemically clean the rivet head(s).

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

    1. SUBTASK 75-32-52-230-068 Do a Crack Test

      1. Do a local penetrant crack test on the new rivet(s).

      2. Refer to SPM TASK 70-23-05-230-501.

        1. Discard cracked rivet(s).

        2. Do Step to Step if necessary.

    1. SUBTASK 75-32-52-350-052 Remove the Damaged Seal Duct and/or Retaining Ring(s)

      NOTE

      The SUBTASKS which follow must only be used to replace a damaged seal duct and/or retaining ring(s).
    2. Refer to Figure and Figure.

      1. Put a mark on each part, to make sure that they agree at assembly.

      2. Refer to SPM TASK 70-09-01-400-501.

      1. Remove the rivets to release the seal duct and/or retaining ring(s).

    3. Discard the damaged seal duct.

    4. Discard the damaged retaining ring(s).

    1. SUBTASK 75-32-52-220-061 Examine the Rivet Holes

    2. Refer to Figure and Figure.

      1. Visually examine and measure the diameter of the rivet holes.

      2. If diameter of the rivet hole(s) is larger than 0.164 in. (4.175 mm) discard whole silencer assembly.

      3. Mark damaged and oversized rivet holes.

      1. Damaged rivet holes.

      2. Do Step, Step and Step as necessary.

    3. SUBTASK 75-32-52-320-051 Deleted

    4. SUBTASK 75-32-52-350-053 Deleted

    5. SUBTASK 75-32-52-390-051-A00 Deleted

    1. SUBTASK 75-32-52-390-051-B00 Install a New or Serviceable Seal Duct and Retaining Ring(s)

    2. Refer to Figure and Figure.

    3. Align the marks made in Step.

      1. Install a new or serviceable seal duct.

      2. Use 1012489 or ARM944 1012489 or (Supplier PN: ARM944) , 1 off, (75-32-52,01-086).

      1. Install a new or serviceable retaining ring(s).

      2. Use 6M1190 RING, RETAINING - SEAL, 2 max. (75-32-52, 01-085).

      1. Install the rivets to safety all sub parts in position.

      2. Use AS16090 RIVET - SOLID UNIVERSAL HEAD, 12 max., (75-32-52,01-080) and/or large AS16132 RIVET - SOLID UNIVERSAL HD, 12 max., (75-32-52,01-083) for large holes.

    1. SUBTASK 75-32-52-390-056 Safety the New or Serviceable Seal Duct and Retaining Ring(s) in Place

    2. Refer to Figure and Figure.

      1. Cold squeeze the rivets in place.

      2. Refer to SPM TASK 70-39-03-390-501.

    1. SUBTASK 75-32-52-110-062 Chemically Clean

      1. Chemically clean the rivet head(s).

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

    1. SUBTASK 75-32-52-230-069 Do a Crack Test

      1. Do a local penetrant crack test on the new rivets.

      2. Refer to SPM TASK 70-23-05-230-501.

        1. Discard cracked rivet(s).

        2. Do Step to Step if necessary.

    1. SUBTASK 75-32-52-220-062 Examine the Assembled Air Seal Assembly

    2. Refer to Figure and Figure.

      1. Visually examine and measure the dimensions of the air seal assembly.

    3. SUBTASK 75-32-52-350-054 Deleted

  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 list of spares. (EC16VU502/A)

Manufacturer Code:D3309
Enterprise Name:MTU MOTOREN-UND-TURBINE UNION MUNCHEN GMBH
BU Name:MTU MOTOREN-UND-TURBINE UNION MUNCHEN GMBH
Street:DACHAUERSTRASSE 665
P.O. Box:80995
City:MUNCHEN 50
Country:GERMANY
Phone Number:49-89-14890
Fax Number:49-89-1502621
Internet:www.mtu.de
Manufacturer Code:K1406
Enterprise Name:DUNLOP LTD - PRECISION RUBBER DIV
BU Name:DUNLOP LTD - PRECISION RUBBER DIV
Street:ASHBY ROAD
City:LOUGHBROUGH
State:LEICS
Province:SHEPSHED
Zip Code:LE12 9EQ
Country:ENGLAND
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:U1653
Enterprise Name:Society Of British Aerospace Companies, LTD.
Link not Found
Part Number:6M1190
Part Name:RING, RETAINING - SEAL
Manufacturer Code:D3309
Unit Of Issue:EA
Part Number:AS16090
Part Name:RIVET - SOLID UNIVERSAL HEAD
Manufacturer Code:U1653
Unit Of Issue:EA
Part Number:AS16132
Part Name:RIVET - SOLID UNIVERSAL HD
Manufacturer Code:U1653
Manufacturer Code:X222X
Supply Number:CoMat 06-064
Type:sp01
Supply Short Name:CoMat 06-064FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY)
Supply Name:CoMat 06-064 FLUORESCENT PENETRANT (WATER WASHABLE MEDIUM SENSITIVITY)
Specification Groups:
Doc NumberType
It is not permitted to mix the selected CoMat 06‐064 letter suffix material with other CoMat 06‐064 letter suffix materials.Where CoMat 06‐064 is specified with no suffix, use one of the CoMat 06‐064 letter suffix materials.
Suppliers:
ManufacturerRemarks
X222X
Link not Found
Link not Found
Manufacturer Code:LOCAL
Tool Number:Standard Workshop Equipment
Tool Name:Standard Workshop Equipment
Link not Found
Link not Found
Link not Found