TASK 72-44-00-040-001 HP Turbine (HPT) Stage 1 Nozzle Assembly - Disassemble The Nozzle Assembly, Disassembly-001

DMC:V2500-A0-72-44-0000-00A-530A-B|Issue No:002.00|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 72-44-00-040-001 HP Turbine (HPT) Stage 1 Nozzle Assembly - Disassemble The Nozzle Assembly, Disassembly-001

General

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 CoMat 10-058 PENETRATING OIL before the removal of threaded parts and parts with an interference fit. 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 seal washers removed in this procedure.

Refer to Fig. 72-44-00-990-001 for a sectional view of the stage 1 turbine nozzle assembly.

NOTE

To identify the consumable materials refer to the PCI.

NOTE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
IAE 1F10052 Two cables sling0AM53IAE 1F100521
IAE 1P16075 Fixture0AM53IAE 1P160751
IAE 1P16093 Puller0AM53IAE 1P160931

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 10-058 PENETRATING OILX222XCoMat 10-058

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-44-00-040-051 Remove the Stage 1 HPT Duct Segments

    1. Refer to Figure.

    2. Remove the bolts and stops which hold the stage 1 HPT duct segments in position.

    3. Remove the duct segments.

    2. SUBTASK 72-44-00-040-052 Install the Fixture to the Stage 1 Turbine Nozzle Assembly

    1. Refer to Figure and Figure.

    2. Lift the IAE 1P16075 Fixture 1 off above the stage 1 turbine nozzle assembly with the IAE 1F10052 Two cables sling 1 off, Figure.

      3. Install the fixture to the stage 1 turbine nozzle assembly.

      1. Lower the fixture on to the stage 1 HPT support assembly.

      2. Align the dowel pin in the fixture with the small hole in the support flange.

      3. Lower the fixture until it touches the support flange.

      4. Attach the fixture to the stage 1 HPT support assembly with the eight hex head capscrews, the washers and the nuts.

    4. Remove the stage 1 turbine nozzle assembly from the pallet.

    5. Turn the stage 1 turbine nozzle assembly so the fixture is down, and put it on the bench, Figure.

    6. Remove the HPT cooling duct deflector.

    3. SUBTASK 72-44-00-040-053 Remove the Inner Combustion Chamber Liner Assembly

    1. Refer to Figure.

    2. Lower the ring detail of the IAE 1P16093 Puller 1 off in the inner combustion chamber liner assembly and put it on the rear surface of the stage 1 HPT cooling duct assembly.

    3. Lower the lifting ring in the inner combustion chamber liner assembly and put it on the OD of the ring.

    4. NOTE

      Holes are adjacent to stage 1 HPT vanes.

      Turn the lifting ring until the flats of the outer diameter align with the large holes in the inner combustion chamber liner assembly.

    5. Install the clamp finger in the large hole in the inner combustion chamber and put the stepped shoulder against the flat on the lifting ring.

    6. Move the clamp so the clamp finger is behind the rib on the inner combustion chamber liner assembly.

    7. Align the holes in the clamp with the threaded holes in the lifting ring.

    8. Install the two small capscrews and the one large jackscrew.

    9. Tighten the two small capscrews.

    10. Repeat steps D. through H. and install the remaining clamps.

    11. Turn the lifting ring to make sure the clamp fingers touch the inner combustion chamber liner assembly ribs.

    12. Turn the jackscrews and apply an equal force to remove the inner combustion chamber liner assembly from the stage 1 HPT cooling duct assembly.

    13. Remove the puller from the inner combustion chamber liner assembly.

    4. SUBTASK 72-44-00-040-054-A00 V2500-A1: Remove the Stage 1 HPT Cooling Duct Assembly and the Stage 1 Vane Cluster Assemblies (Pre SBE 72-0029)

    1. Refer to Figure and Figure.

    2. Raise the assembly and remove the stage 1 HPT cooling duct assembly, Figure.

    3. Lower the assembly on to the bench.

    4. Remove the bolts, the sleeve bushings and the washers which hold the stage 1 HPT vane cluster assemblies and the stage 1 HPT seal assembly in position, Figure.

    5. Remove the stage 1 HPT seal assembly.

    6. Remove the nut, the bolt and the spacer from the stage 1 HPT seal assembly.

    7. Remove the screw head bolt from the vane cluster assembly and the nut plate in the stage 1 HPT support assembly.

    8. Remove the stage 1 HPT vane cluster assemblies and the stage 1 HPT seals.

    9. Remove the stage 1 HPT support assembly from the fixture.

    5. SUBTASK 72-44-00-040-054-B00 V2500-A1: Remove the Stage 1 HPT Cooling Duct Assembly and the Stage 1 Vane Cluster Assemblies (SBE 72-0029)

    1. Refer to Figure and Figure

    2. Raise the assembly and remove the stage 1 HPT cooling duct assembly, Figure.

    3. Lower the asembly on to the bench.

    4. Remove the bolts, the washers, the sleeve bushings and the spacers which hold the stage 1 HPT vane cluster assemblies and the stage 1 HPT seal assembly in poistion, Figure.

    5. Remove the stage 1 HPT seal assembly.

    6. Remove the nut, the bolt and the spacer from the stage 1 HPT seal assembly.

    7. Remove the screw head bolt from the vane cluster assembly and the nut plate in the stage 1 HPT support assembly.

    8. Remove the stage 1 HPT vane cluster assemblies and the stage 1 HPT seals.

    9. Remove the stage 1 HPT support assembly from the fixture.

    6. SUBTASK 72-44-00-040-054-C00 V2500-A5: Remove the Stage 1 HPT Cooling Duct Assembly and the Stage 1 Vane Assemblies (Pre SBE 72-0151, Pre SBE 72-0598)

    1. Refer to Figure and Figure.

    2. Raise the assembly and remove the stage 1 HPT cooling duct assembly, Figure.

    3. Lower the assembly on to the bench.

    4. Remove the bolts, the washers, the sleeve bushings and the spacers which hold the stage 1 HPT vane assemblies and the stage 1 HPT seal assembly in position, Figure.

    5. Remove the stage 1 HPT seal assembly.

    6. Remove the nut, the bolt and the spacer from the stage 1 HPT seal assembly.

    7. Remove the screw head bolt from the vane assembly and the nut plate in the stage 1 HPT assembly.

    8. Remove the stage 1 HPT vane assemblies and the stage 1 HPT vane seals.

    9. Remove the stage 1 HPT support assembly from the fixture.

    7. SUBTASK 72-44-00-040-054-D00 V2500-A1 Phoenix: Remove the Stage 1 HPT Cooling Duct Assembly and the Stage 1 Vane Assemblies (SBE 72-0340)

    1. Refer to Figure and Figure.

    2. Raise the assembly and remove the stage 1 HPT cooling duct assembly, Figure.

    3. Lower the assembly onto the bench.

    4. Remove the bolts, washers, sleeve bushings and the spacers which hold the stage 1 HPT vane assemblies and the stage 1 HPT seal assembly in position, Figure.

    5. Remove the stage 1 HPT seal assembly.

    6. Remove the nut, bolt and the spacer from the stage 1 HPT seal assembly.

    7. Remove the screw head bolt from the vane assembly and the nut plate in the stage 1 HPT assembly.

    8. Remove the stage 1 HPT vane assemblies and the stage 1 HPT vane seals.

    9. Remove the stage 1 HPT support assembly from the fixture.

    8. SUBTASK 72-44-00-040-054-E00 V2500-A5: Remove the Stage 1 HPT Cooling Duct Assembly and the Stage 1 Vane Assemblies (SBE 72-0151, SBE 72-0598)

    1. Refer to Figure and Figure.

    2. Raise the assembly and remove the stage 1 HPT cooling duct assembly, Figure.

    3. Lower the assembly onto the bench.

    4. Remove the bolts, washers, sleeve bushings and the spacers which hold the stage 1 HPT vane assemblies and the stage 1 HPT seal assembly in position, Figure.

    5. Remove the stage 1 HPT seal assembly.

    6. Remove the nut, bolt and the spacer from the stage 1 HPT seal assembly.

    7. Remove the screw head bolt from the vane assembly and the nut plate in the stage 1 HPT assembly.

    8. Remove the stage 1 HPT vane assemblies and the stage 1 HPT vane seals.

    9. Remove the stage 1 HPT support assembly from the fixture.

    9. Figure: Install the IAE 1P16075 fixture

    Install the IAE 1P16075 fixture

    Figure: Remove the inner combustion chamber liner assembly

    Remove the inner combustion chamber liner assembly

    Figure: Install the IAE 1P16093 puller

    Install the IAE 1P16093 puller

    Figure: V2500-A1 Pre SBE Fig. 72-0029: Remove the stage 1 HPT vane cluster

    V2500-A1 Pre SBE Fig. 72-0029: Remove the stage 1 HPT vane cluster

    Figure: V2500-A1 SBE 72-0029: Remove the stage 1 HPT vane cluster assemblies

    V2500-A1 SBE 72-0029: Remove the stage 1 HPT vane cluster assemblies

    Figure: Remove the stage 1 HPT vane assemblies

    Remove the stage 1 HPT vane assemblies

    Figure: V2500-A5 SBE 72-0151: Remove the stage 1 HPT vane assemblies

    V2500-A5 SBE 72-0151: Remove the stage 1 HPT vane assemblies

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Added SBE 72-0598 information. (18VC516)

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:X222X
Enterprise Name:N/A – REFER TO APPLICABLE COMAT SUFFIX
Manufacturer Code:X222X
Supply Number:CoMat 10-058
Type:sp01
Supply Short Name:CoMat 10-058 PENETRATING OIL
Supply Name:CoMat 10-058 PENETRATING OIL
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:0AM53
Tool Number:IAE 1F10052
Tool Name:IAE 1F10052 Two cables sling
Manufacturer Code:0AM53
Tool Number:IAE 1P16075
Tool Name:IAE 1P16075 Fixture
Manufacturer Code:0AM53
Tool Number:IAE 1P16093
Tool Name:IAE 1P16093 Puller