TASK 72-50-10-030-005 LPT Case And Rotor Assembly - Disassemble The LPT Stage 6 Stator Vanes From The LPT, Disassembly-005

DMC:V2500-A0-72-50-1000-05A-530A-B|Issue No:002.00|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 72-50-10-030-005 LPT Case And Rotor Assembly - Disassemble The LPT Stage 6 Stator Vanes From The LPT, Disassembly-005

General

Refer to TASK 72-50-10-030-001 (DISASSEMBLY-001) before you do this TASK.

Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.

Apply the approved penetrating oil before the removal of threaded parts. Let the parts soak before removal. For the approved oils and procedures, refer to the SPM TASK 70-64-00-640-501.

Remove and discard the lockwire before parts are disconnected or removed.

Discard all rubber seal rings, cotter pins and keywashers removed in this procedure.

Refer to TASK 72-50-00-990-501 (DESCRIPTION AND OPERATION-001) for a sectional view of the LP turbine module.

NOTE

Special tools are identified in the procedure by the tool primary number.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
BasketLOCALBasket

For blades and vanes

IAE 1M14094 Retaining block0AM53IAE 1M1409433
IAE 1M14124 Protector ring segment0AM53IAE 1M141243
IAE 1M14010 Assembly/Disassembly fixture0AM53IAE 1M14010

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-50-10-030-144 Install the Protector Ring Segments

    2. Refer to: Figure

    3. Install the IAE 1M14124 Protector ring segment 3 off between the stage 6 vane inner platforms and the stage 5 blade roots.

    1. SUBTASK 72-50-10-030-087 Remove the Retaining Blocks and the Stage 6 Vane Segments

    2. Refer to: Figure

    3. Remove the IAE 1M14094 Retaining block 33 off from the joint of the stage 6 vane. Pull the vane segment rearwards out of the turbine case. Do this procedure with all 33 vane segments.

    4. Put the vane segments in a basket.

    1. SUBTASK 72-50-10-030-145 Remove the Protector Ring Segments

    2. Refer to: Figure

    3. Remove the three protector ring segments.

    1. SUBTASK 72-50-10-030-192 Move the Lifting Ring

    2. Move the lifting ring of the IAE 1M14010 Assembly/Disassembly fixture 1 off from the 'lifting-position' into the 'zero-position' with the use of the lever.

  1. Figure: Remove the stage 6 vanes

    Remove the stage 6 vanes

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Editorial correction due to conversion

Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Tool Number:Basket
Tool Name:Basket
Manufacturer Code:0AM53
Tool Number:IAE 1M14010
Tool Name:IAE 1M14010 Assembly/Disassembly fixture
Manufacturer Code:0AM53
Tool Number:IAE 1M14094
Tool Name:IAE 1M14094 Retaining block
Manufacturer Code:0AM53
Tool Number:IAE 1M14124
Tool Name:IAE 1M14124 Protector ring segment