TASK 72-00-50-420-003-C00 LPT Module - Install The Turbine Exhaust Case (TEC) (Horizontal) - Method 2, Installation-004

DMC:V2500-A5-72-00-5000-03D-720A-B|Issue No:008.00|Issue Date:2021-08-01

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

V2500-A5

Common Information

TASK 72-00-50-420-003-C00 LPT Module - Install The Turbine Exhaust Case (TEC) (Horizontal) - Method 2, Installation-004

General

Transportation covers/blanks must be removed immediately before installation of the components.

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.

For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig/item number.

Special torque data is identified by the * symbol after the torque value.

Assembly tolerances are included in the procedure.

Lubricate all threads and abutment faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS, unless other lubricants are referred to in the procedure.

To identify, lubricate and install seal rings, refer to SPM TASK 70-64-02-640-501.

After assembly apply CoMat 07-038 AIR DRYING ENAMEL to any damaged surface protection, joint flanges and attach parts. Use the correct color of the air drying enamel. Refer to SPM TASK 70-38-21-380-501.

The number for each radial location must be identified in a clockwise direction. These start at the engine top position when you look from the rear of the engine, unless stated differently in the procedure.

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
Electronic balance craneLOCALElectronic balance crane
IAE 1F10016 Mechanical wrench0AM53IAE 1F100161
IAE 1F10026 Hydraulic hand pump0AM53IAE 1F100261
IAE 1F10033 Hydraulic installation pusher0AM53IAE 1F100331
IAE 1F10034 Hydraulic installation pusher0AM53IAE 1F100341
IAE 1F10038 Torque wrench0AM53IAE 1F100381
IAE 1F10039 Anti-torque adapter0AM53IAE 1F100391
IAE 1F10040 Anchor wrench plate0AM53IAE 1F100401
IAE 1F10051 Two cable sling0AM53IAE 1F100511
IAE 1F10073 remove/installation fixture0AM53IAE 1F100731
IAE 1F10075 Support pedestal0AM53IAE 1F100752
IAE 1F10076 Locking collar0AM53IAE 1F100761
IAE 1F10178 Storage and Turnover adapter0AM53IAE 1F101781
IAE 6F01029 Pneumatic cart0AM53IAE 6F010291
IAE 6F10030 Vacuum test cart0AM53IAE 6F100301
IAE 1J12244 Sizing sleeve0AM53IAE 1J122441
IAE 1J12263 Seal slider0AM53IAE 1J122631
IAE 1J12523 Seal slider0AM53IAE 1J12523
IAE 1M14143 Support fixture0AM53IAE 1M141431
IAE 1M14461 Supporting fixtureLOCALIAE 1M14461
IAE 1P16354 Vacuum Test Adapter0AM53IAE 1P163541
IAE 1P16374 Wrench support0AM53IAE 1P163741
IAE 1P16377 Guide support0AM53IAE 1P163771
IAE 1P14041 Drier0AM53IAE 1P140411
IAE 1P17523 Blank-off Plate0AM53IAE 1P175231
IAE 1P17041 Drier0AM53IAE 1P17041

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-141 LOCKWIRELOCALCoMat 02-141
CoMat 07-038 AIR DRYING ENAMELk3504CoMat 07-038
CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE03530CoMat 10-045
CoMat 10-045A LEAK CHECK FLUID, BUBBLES-TYPELOCALCoMat 10-045A
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077
CoMat 10-129 ANTI-SEIZE PASTE34568CoMat 10-129

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Sealing ring1
Packing3
Packing1
Packing1

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-50-420-207 Identify the Turbine Exhaust Case (TEC) Mini Module

    2. Make sure that the replacement TEC is fully interchangeable with the mini module that it replaces and with the modules to which it is to be installed. Refer to SPM for Module Identification and Interchangeability.

    1. SUBTASK 72-00-50-220-151 Examine the Module Interfaces

    2. Examine the LP Turbine Module interface E-50/50. Refer to TASK 72-00-50-200-004 (INSPECTION-004).

    1. SUBTASK 72-00-50-220-152 Examine the TEC Mini Module Externally and Examine the Non-Modular Parts

    2. Examine the TEC mini module externally and examine the non-modular parts.

    1. SUBTASK 72-00-50-220-153 Reference Fits and Clearances of the Stage 6 Inner Turbine Air Seal and the No.5 Bearing Housing at Location 2275

    2. Refer to Figure.

    3. Reference the clearance at location 2275. If required, use the data written as a note in TASK 72-50-53-200-000 (INSPECTION-000) and TASK 72-50-00-200-000 (INSPECTION-000).

      Table 1. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2275

      No. 5 Bearing Housing Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-350)

      Stage 6 Inner Turbine Air Seal LP Turbine (LPT) And Turbine Exhaust Case (TEC) Unit (72-50-00, 01-240)

      No. 5 Bearing Housing

      5.5512

      Clear

      5.5551

      0.0315

      Stage 6 Inner Turbine Air Seal

      5.5157

      0.0394

      5.5197

      Clear

      Table 2. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2275

      No. 5 Bearing Housing Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-350)

      Stage 6 Inner Turbine Air Seal LP Turbine (LPT) And Turbine Exhaust Case (TEC) Unit (72-50-00, 01-240)

      No. 5 Bearing Housing

      141.000

      Clear

      141.099

      0.800

      Stage 6 Inner Turbine Air Seal

      140.099

      1.001

      140.200

      Clear

    1. SUBTASK 72-00-50-220-154 Reference Fits and Clearances of the LP Turbine Case and the Tec at Location 2277

    2. Refer to Figure.

    3. Reference the interference at location 2277. If required, use the data written as a note in TASK 72-50-10-200-000 (INSPECTION-000) and TASK 72-50-53-200-000 (INSPECTION-000).

      Table 3. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2277

      LP Turbine Case (72-50-10, 01-010)

      Turbine Exhaust Case Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-020)

      LP Turbine Case Diameter

      38.6587

      Intf

      38.6480

      Clear

      38.6642

      0.0000

      38.6642

      0.0244

      Turbine Exhaust Case Bore

      38.6524

      0.0118

      38.6524

      0.0118

      38.6587

      Intf

      38.6724

      Intf

      Table 4. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2277

      LP Turbine Case (72-50-10, 01-010)

      Turbine Exhaust Case Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-020)

      LP Turbine Case Diameter

      981.931

      Intf

      981.66

      Clear

      982.070

      0.000

      982.07

      0.62

      Turbine Exhaust Case Bore

      981.771

      0.300

      981.77

      0.30

      981.931

      Intf

      982.28

      Intf

    1. SUBTASK 72-00-50-220-155 Reference Fits and Clearances of the LP Shaft and the No. 5 Bearing at Location 2271

    2. Refer to Figure.

    3. Reference the interference at location 2271. If required, use the data written as a note in TASK 72-50-41-200-000 (INSPECTION-000) and TASK 72-50-52-200-000 (INSPECTION-000).

      Table 5. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2271

      LP Turbine Shaft LPT Shaft And Related Parts (72-50-41, 01-200)

      No. 5 Bearing ENGINE-NO.5 BEARING PLATE AND OIL DEFLECTOR (72-50-52, 20-060)

      LP Turbine Shaft Diameter

      3.6224

      Intf

      3.6228

      0.0003

      No. 5 Bearing Bore

      3.6217

      0.0011

      3.6220

      Intf

      Table 6. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2271

      LP Turbine Shaft LPT Shaft And Related Parts (72-50-41, 01-200)

      No. 5 Bearing ENGINE-NO.5 BEARING PLATE AND OIL DEFLECTOR (72-50-52, 20-060)

      LP Turbine Shaft Diameter

      92.0090

      92.0191

      Intf

      0.0080

      No. 5 Bearing Bore

      91.9912

      91.9988

      0.0279

      Intf

    1. SUBTASK 72-00-50-220-156 Reference Fits and Clearances of the LP Turbine Shaft and the No. 5 Bearing Seal Spacer at Location 2272

    2. Refer to Figure.

    3. Reference the clearance at location 2272. If required, use the data written as a note in TASK 72-50-41-200-000 (INSPECTION-000) and TASK 72-50-42-200-000 (INSPECTION-000).

      Table 7. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2272

      LP Turbine Shaft LPT Shaft And Related Parts (72-50-41, 01-200)

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-120)

      LP Turbine Shaft Diameter

      3.7392

      Clear

      3.7398

      0.0004

      No. 5 Bearing Seal Spacer

      3.7402

      0.0019

      3.7411

      Clear

      Table 8. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2272

      LP Turbine Shaft LPT Shaft And Related Parts (72-50-41, 01-200)

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-120)

      LP Turbine Shaft Diameter

      94.9757

      Clear

      94.9909

      0.011

      No. 5 Bearing Seal Spacer

      95.0011

      0.048

      95.0239

      Clear

    1. SUBTASK 72-00-50-220-157-A00 Reference Fits and Clearances of the LP Turbine Shaft and the No. 5 Bearing Seal Spacer at Location 2273 (Pre SBE 72-0165)

    2. Refer to Figure.

    3. Reference the clearance at location 2273. If required, use the data written as a note in TASK 72-50-41-200-000 (INSPECTION-000) and TASK 72-50-42-200-000 (INSPECTION-000).

      Table 9. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2273

      LP Turbine Shaft LPT Shaft And Related Parts (72-50-41, 01-200)

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-160)

      LP Turbine Shaft Diameter

      3.739

      Clear

      3.740

      0.008

      No. 5 Bearing Seal Spacer

      3.748

      0.019

      3.758

      Clear

      Table 10. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2273

      LP Turbine Shaft LPT Shaft And Related Parts(72-50-41, 01-200)

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-160)

      LP Turbine Shaft Diameter

      94.971

      Clear

      94.996

      0.200

      No. 5 Bearing Seal Spacer

      95.200

      0.480

      95.450

      Clear

    1. SUBTASK 72-00-50-220-157-B00 Reference Fits and Clearances of the LP Turbine Shaft and the No. 5 Bearing Seal Spacer at Location 2273 (SBE 72-0165)

    2. Refer to Figure.

    3. Reference the clearance at location 2273. If required, use the data written as a note in TASK 72-50-41-200-000 (INSPECTION-000) and TASK 72-50-42-200-000 (INSPECTION/CHECK-000).

      Table 11. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2273

      LP Turbine Shaft LPT Shaft And Related Parts (72-50-41, 01-200)

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-160)

      LP Turbine Shaft Diameter

      3.739

      Clear

      3.740

      0.004

      No. 5 Bearing Seal Spacer

      3.744

      0.006

      3.745

      Clear

      Table 12. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2273

      LP Turbine Shaft LPT Shaft And Related Parts (72-50-41, 01-200)

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-160)

      LP Turbine Shaft Diameter

      94.971

      Clear

      94.946

      0.102

      No. 5 Bearing Seal Spacer

      95.098

      0.152

      95.123

      Clear

    1. SUBTASK 72-00-50-220-158 Reference Fits and Clearances of the No. 5 Bearing Seal Spacers at Location 2274

    2. Refer to Figure.

    3. Reference the clearance at location 2274. If required, use the data written as a note in TASK 72-50-42-200-000 (INSPECTION-000).

      Table 13. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2274

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-120)

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-160)

      No. 5 Bearing Seal Spacer

      4.0645

      Clear

      4.0655

      0.002

      No. 5 Bearing Seal Spacer

      4.0675

      0.004

      4.0685

      Clear

      Table 14. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2274

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-120)

      No. 5 Bearing Seal Spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-160)

      No. 5 Bearing Seal Spacer

      103.238

      Clear

      103.264

      0.051

      No. 5 Bearing Seal Spacer

      103.314

      0.102

      103.340

      Clear

    1. SUBTASK 72-00-50-220-159 Reference Fits and Clearances of the No. 5 Bearing Nozzle and the TEC at Location 2283

    2. Refer to Figure.

    3. Reference the clearance at location 2283. If required, use the data written as a note in TASK 72-58-02-200-000 (INSPECTION-000) and TASK 72-50-53-200-000 (INSPECTION-000).

      Table 15. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2283

      No. 5 Bearing Nozzle NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-070)

      Turbine Exhaust Case Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-300)

      No. 5 Bearing Nozzle

      0.534

      Clear

      0.536

      0.002

      Turbine Exhaust Case

      0.538

      0.008

      0.542

      Clear

      Table 16. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2283

      No. 5 Bearing Nozzle NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-070)

      Turbine Exhaust Case Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-300)

      No. 5 Bearing Nozzle

      13.564

      Clear

      13.614

      0.051

      Turbine Exhaust Case

      13.665

      0.203

      13.767

      Clear

    1. SUBTASK 72-00-50-220-160 Reference Fits and Clearances of the No. 5 Bearing Transfer Tube and the TEC at Location 2284

    2. Refer to Figure.

    3. Reference the clearance at location 2284. If required, use the data written as a note in TASK 72-58-02-200-000 (INSPECTION-000) and TASK 72-50-53-200-000 (INSPECTION-000).

      Table 17. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2284

      No. 5 Bearing Transfer Tube NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-030)

      The Turbine Exhaust Case Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-300)

      No. 5 Bearing Transfer Tube

      0.359

      Clear

      0.361

      0.017

      Turbine Exhaust Case

      0.378

      0.023

      0.382

      Clear

      Table 18. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2284

      No. 5 Bearing Transfer Tube NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-030)

      The Turbine Exhaust Case Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-300)

      No. 5 Bearing Transfer Tube

      9.119

      Clear

      9.169

      0.432

      Turbine Exhaust Case

      9.601

      0.584

      9.703

      Clear

    1. SUBTASK 72-00-50-220-161 Reference Fits and Clearances of the No. 5 Bearing Transfer Tube and the No. 5 Bearing Nozzle at Location 2285

    2. Refer to Figure.

    3. Reference the clearance at location 2285. If required, use the data written as a note in TASK 72-58-02-200-000 (INSPECTION-000).

      Table 19. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2285

      No. 5 Bearing Transfer Tube NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-030)

      No. 5 Bearing Nozzle NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-070)

      No. 5 Bearing Transfer Tube

      0.359

      Clear

      0.361

      0.017

      No. 5 Bearing Nozzle

      0.378

      0.023

      0.382

      Clear

      Table 20. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2285

      No. 5 Bearing Transfer Tube NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-030)

      No. 5 Bearing Nozzle NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-070)

      No. 5 Bearing Transfer Tube

      9.119

      Clear

      9.169

      0.432

      No. 5 Bearing Nozzle

      9.601

      0.584

      9.703

      Clear

    1. SUBTASK 72-00-50-220-162 Reference Fits and Clearances of the No. 5 Bearing Transfer Tube and the No. 5 Bearing Nozzle at Location 2286

    2. Refer to Figure.

    3. Reference the clearance at location 2286. If required, use the data written as a note in TASK 72-58-02-200-000 (INSPECTION-000).

      Table 21. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2286

      No. 5 Bearing Transfer Tube NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-030)

      No. 5 Bearing Nozzle NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-070)

      No. 5 Bearing Transfer Tube

      0.394

      Clear

      0.396

      0.017

      No. 5 Bearing Nozzle

      0.413

      0.023

      0.417

      Clear

      Table 22. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 2286

      No. 5 Bearing Transfer Tube NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-030)

      No. 5 Bearing Nozzle NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-070)

      No. 5 Bearing Transfer Tube

      10.008

      Clear

      10.058

      0.432

      No. 5 Bearing Nozzle

      10.490

      0.584

      10.592

      Clear

    1. SUBTASK 72-00-50-220-164 Reference Fits and Clearances of the Stage 7 LP Turbine Blade and the TEC at Location 3792

    2. Refer to Figure.

    3. Reference the interference at location 3792. If required, use the data written as a note in TASK 72-50-32-200-000 (INSPECTION-000) and TASK 72-50-53-200-000 (INSPECTION-000).

      Table 23. Fits and Clearances (all dimensions are in inches)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 3792

      Stage 7 LP Turbine Blade LPT Stage 3, 4, 5, 6, 7 Blades (72-50-32, 01-010)

      Turbine Exhaust Case Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-300)

      Stage 7 LP Turbine Blade

      0.0740

      Minimum

      Turbine Exhaust Case

      0.1770

      Maximum

      Table 24. Fits and Clearances (all dimensions are in millimeters)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      (Non-select)

      REJECT IF

      MORE THAN

      LOCATION 3792

      Stage 7 LP Turbine Blade LPT Stage 3, 4, 5, 6, 7 Blades (72-50-32, 01-010)

      Turbine Exhaust Case Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 21-300)

      Stage 7 LP Turbine Blade

      1.879 Minimum

      Turbine Exhaust Case

      4.493 Maximum

    1. SUBTASK 72-00-50-420-208-A00 Install the No. 5 Bearing Seal Spacers on to the LP Turbine Shaft (Pre SBE 72-0165)

    2. Refer to Figure.

    3. CAUTION

      MAKE SURE THE LID OF THE NO. 5 BEARING SEAL SPACER POINTS TOWARDS THE REAR.

      Install the No. 5 Bearing seal spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-160) to the rear end of the LP Turbine Shaft.

    4. Lightly coat the No. 5 Bearing Carbon Seal ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-140) with CoMat 10-077 APPROVED ENGINE OILS.

    5. Install the carbon seal to the rear end of the LP Turbine Shaft.

    6. Install the No. 5 Bearing seal spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-120) to the rear end of the LP Turbine Shaft.

    7. Install the IAE 1F10033 Hydraulic installation pusher 1 off on the rear end of the LP Turbine Shaft. Attach the reaction adapter (part of the hydraulic installation pusher) to the rear thread of the LP Turbine Shaft.

    8. Tighten the knurled nut (part of the hydraulic installation pusher).

    9. Connect the IAE 1F10026 Hydraulic hand pump 1 off to the coupler of the pusher.

    10. Operate the hydraulic pump to move the No. 5 Bearing seal spacers into the correct position.

      1. Remove the tools as follows.

      2. Disconnect the hydraulic pump from the hydraulic installation pusher.

      3. Release the knurled nut and remove the hydraulic installation pusher.

    1. SUBTASK 72-00-50-420-208-B00 Install the No. 5 Bearing Seal and Spacers on to the LP Turbine Shaft (SBE 72-0165)

    2. Refer to Figure.

    3. SBE 72-0165: Replace the No. 5 Bearing seal spacer with a spacer incorporating fool-proof installation features.

    4. Install the No. 5 Bearing seal spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-160) to the rear end of the LP Turbine Shaft.

    5. Lightly coat the No. 5 Bearing carbon seal ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-140) with a lint-free cloth made moist with CoMat 10-077 APPROVED ENGINE OILS.

    6. Install the carbon seal to the rear end of the LP Turbine Shaft.

    7. Install the No. 5 Bearing seal spacer ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-120) to the rear end of the LP Turbine Shaft.

    8. Install the IAE 1F10033 Hydraulic installation pusher 1 off on the rear end of the LP Turbine Shaft. Attach the reaction adapter (part of the hydraulic installation pusher) to the rear thread of the LP Turbine Shaft.

    9. Tighten the knurled nut (part of the hydraulic installation pusher).

    10. Connect the IAE 1F10026 Hydraulic hand pump 1 off to the coupler of the pusher.

    11. Operate the hydraulic pump to move the carbon seal into the correct position.

      1. Remove the tools as follows.

      2. Disconnect the hydraulic pump from the hydraulic installation pusher.

      3. Release the knurled nut and remove the hydraulic installation pusher.

    1. SUBTASK 72-00-50-420-209-A00 Install the No. 5 Bearing Inner Race (Pre SBE 72-0165)

    2. Refer to Figure.

    3. Heat the inner race of the No. 5 Bearing ENGINE-NO.5 BEARING PLATE AND OIL DEFLECTOR (72-50-52, 20-060) to approximately 212 deg F (100 deg C).

    4. WARNING

      USE GLOVES TO INSTALL THE HOT INNER RACE OF THE NO. 5 BEARING.

      Install the inner race of the No. 5 Bearing to the LP Turbine Shaft.

    5. Install the IAE 1F10034 Hydraulic installation pusher 1 off on the rear end of the LP Turbine Shaft. Attach the reaction adapter (part of the hydraulic installation pusher) to the rear thread of the LP Turbine Shaft.

    6. Tighten the knurled nut (part of the hydraulic installation pusher).

    7. Connect the IAE 1F10026 Hydraulic hand pump 1 off to the coupler of the pusher.

    8. Operate the hydraulic pump to move the inner race of the No. 5 Bearing into the correct position.

      1. Remove the tools as follows.

      2. Disconnect the hydraulic pump from the hydraulic installation pusher.

      3. Release the knurled nut and remove the hydraulic installation pusher.

    1. SUBTASK 72-00-50-420-209-B00 Install the No. 5 Bearing Inner Race (SBE 72-0165)

    2. Refer to Figure.

    3. SBE 72-0165: Replace the No. 5 Bearing seal spacer with a spacer incorporating fool-proof installation features.

    4. Heat the inner race of the No. 5 Bearing ENGINE-NO.5 BEARING PLATE AND OIL DEFLECTOR (72-50-52, 20-060) to approximately 212 deg F (100 deg C).

    5. WARNING

      USE GLOVES TO INSTALL THE HOT INNER RACE OF THE NO. 5 BEARING.

      Install the inner race of the No. 5 Bearing to the LP Turbine Shaft.

    6. Install the IAE 1F10034 Hydraulic installation pusher 1 off on the rear end of the LP Turbine Shaft. Attach the reaction adapter (part of the hydraulic installation pusher) to the rear thread of the LP Turbine Shaft.

    7. Tighten the knurled nut (part of the hydraulic installation pusher).

    8. Connect the IAE 1F10026 Hydraulic hand pump 1 off to the coupler of the pusher.

    9. Operate the hydraulic pump to move the inner race of the No. 5 Bearing into the correct position.

      1. Remove the tools as follows.

      2. Disconnect the hydraulic pump from the hydraulic installation pusher.

      3. Release the knurled nut and remove the hydraulic installation pusher.

    1. SUBTASK 72-00-50-420-210 Install the Guide Support to the LP Turbine Shaft

    2. Refer to Figure.

    3. Install the IAE 1P16377 Guide support 1 off into the inner diameter of the LP Turbine Shaft. Use an applicable webbing sling.

    4. Make sure that the centering diameter of the guide support is installed correctly to the LP Turbine Shaft. Turn the screw, at the rear end of the guide support, clockwise to connect the guide support to the LP Turbine Shaft.

    5. Put the IAE 1F10075 Support pedestal 1 off below the guide support. Move the support pedestal A near to the rear flange of the LP Turbine Shaft.

    6. Turn the handwheel A until the end of the pedestal-screw touches the guide support. Lock the pedestal-screw with the handwheel B.

    1. SUBTASK 72-00-50-420-211 Install the Remove/Installation Fixture to the TEC

    2. Refer to Figure.

    3. Attach hoist equipment to the upper supports of the IAE 1F10073 remove/installation fixture 1 off.

    4. Install the remove/installation fixture to the rear flange of the Turbine Exhaust Case. Attach the remove/installation fixture with the 13 bolts and washers. Tighten the bolts.

    5. Remove the hoist equipment.

    1. SUBTASK 72-00-50-420-212 Install the TEC to the Guide support

    2. Refer to Figure.

    3. Attach electronic balance crane to hoist equipment. Attach the IAE 1F10051 Two cable sling 1 off to the electronic balance crane. Connect the two cables sling to the spools of the IAE 1F10073 remove/installation fixture 1 off.

    4. Lift the Turbine Exhaust Case from the IAE 1F10178 Storage and Turnover adapter 1 off.

    5. Read and write down the weight shown on the electronic balance crane.

    6. CAUTION

      IN THE FOLLOWING STEPS, THE ELECTRONIC BALANCE CRANE MUST STAY AT APPROXIMATELY THE SAME WEIGHT.

      Lift the Turbine Exhaust Case and engage it to the IAE 1P16377 Guide support. Move the TEC forward.

    7. Install the IAE 1F10075 Support pedestal 1 off behind the Turbine Exhaust Case to the rear end of the guide support. Refer to SUBTASK 72-00-50-420-141, step D.

    1. SUBTASK 72-00-50-420-213 Remove the Supporting Fixture

    2. Refer to Figure.

    3. Release the two hand knobs that attach the two clamps (part of the IAE 1M14143 Support fixture or of the IAE 1M14461 Supporting fixture) 1 off to the Stage 7 Turbine Disk.

    4. Release the four screws that attach the supporting fixture to the LP Turbine Case. Remove the supporting fixture from the rear flange of the LP Turbine Case.

    1. SUBTASK 72-00-50-420-214 Install the TEC to the LP Turbine Case

    2. Refer to Figure.

    3. Remove the IAE 1F10075 Support pedestal A 1 off.

    4. Release the handwheel B of the IAE 1F10075 Support pedestal B 1 off. Turn the handwheel A until the electronic balance crane shows the initial weight. Refer to Step.

    5. WARNING

      THIS STEP IS NECESSARY, BECAUSE THE WEIGHT OF THE LP TURBINE ROTOR INCREASED THE WEIGHT SHOWN ON THE ELECTRONIC BALANCE CRANE.

      Move the TEC forward to the rear flange of the LP Turbine Case. Align the dowel pins.

    6. Turn the jackscrew (part of the remove/installation fixture) clockwise to the stop position. Lock the jackscrew in this position with the IAE 1F10076 Locking collar 1 off.

    7. CAUTION

      MAKE SURE THAT THE NO. 5 BEARING AND THE NO 5 BEARING SEAL SPACERS ENGAGE CORRECTLY.

      Turn the jackscrew counterclockwise until the flanges of the LP Turbine Case and the Turbine Exhaust Case fit correctly.

      1. CAUTION

        HOLD THE BOLTS IN THEIR POSITION WHEN YOU INSTALL THE NUTS ON TO THE BOLTS. DO NOT TURN THE BOLTS OR MAKE TO-AND-FRO MOVEMENTS. THE TURBINE EXHAUST CASE/LP CASE FLANGE AND/OR THE BOLTS CAN BE DAMAGED.

        CAUTION

        INCORRECT ASSEMBLY OF THE BOLT AND NUT CAN CAUSE OIL TUBE DAMAGE.

        Install the 16 brackets and attach the 114 bolts and nuts which lock the Turbine Exhaust Case to the LP Turbine Case. Refer to Figure.

      2. Assemble the bolt at hole No. 75 in opposite direction to give more space between bolt end and oil tube.

      3. Torque the nuts to 85* lbfin to 95* lbfin (9.60* Nm to 10.73* Nm).

      1. Remove the tools from the engine as follows:

      2. Remove the two cables sling and the electronic balance crane from the remove/installation fixture.

      3. Install the hoist equipment to the upper supports of the remove/installation fixture.

      4. Remove the locking collar and the support pedestal B.

      5. Release the 19 screws which attach the remove/installation fixture to the rear flange of the TEC. Remove the remove/installation fixture.

      6. Remove the guide support.

    1. SUBTASK 72-00-50-420-215 Install the Rear Lock Nut to the LP Turbine Shaft

    2. Refer to Figure.

    3. Install the rear lock nut to the LP Turbine Shaft and hand-tighten the nut.

    4. Attach the IAE 1P16374 Wrench support 1 off to the inner rear flange of the TEC.

    5. Install the IAE 1F10038 Torque wrench 1 off through the wrench support. Engage the torque wrench with the rear lock nut.

    6. Install the IAE 1F10039 Anti-torque adapter 1 off through the torque wrench. Lock the anti-torque adapter to the LP Turbine Shaft.

    7. Install the IAE 1F10016 Mechanical wrench 1 off to the torque wrench. Attach the anti-torque adapter to the mechanical wrench with the IAE 1F10040 Anchor wrench plate 1 off.

    8. Operate the mechanical wrench and torque the rear lock nut to 4000 lbfin to 6000 lbfin (452 Nm to 678 Nm).

    9. Make a correlation mark between the IAE 1F10016 Mechanical wrench and the IAE 1F10038 Torque wrench.

    10. Put a five to eight degree angle of turn to the rear lock nut.

    11. Operate the mechanical wrench to release the torque until the torque valve is zero.

    12. Torque the rear lock nut again to 4000 lbfin to 6000 lbfin (452 Nm to 678 Nm).

    13. Make a correlation mark between the IAE 1F10016 Mechanical wrench 1 off and the IAE 1F10038 Torque wrench 1 off.

    14. Put a five to eight degree angle of turn to the rear lock nut.

    15. Do Step and Step again and check the correlation mark. The mark must be within two degrees maximum on the same place.

    16. If the correlation mark is within the limit, continue with Step.

    17. If the correlation mark is outside the limit, delete the correlation mark and do Step to Step again until the mark is within the limit.

    18. Apply the last five to eight degree angle of turn to the rear lock nut.

    19. Align the slot of the rear lock nut with the slot on the rear end of the LP Turbine Shaft. The alignment of the rear lock nut must be in the torque direction.

    20. If the slots do not align within the specified degree range, re-install torquing hardware, loosen nut to zero and repeat Step to Step.

      1. Remove the tools from the engine as follows.

      2. Remove the anchor wrench plate and the mechanical wrench.

      3. Disengage the lock mechanism of the anti-torque adapter and remove the adapter.

      4. Remove the torque wrench.

      5. Remove the wrench support.

    21. Safety the rear lock nut with the locking ring and the internal retaining ring.

    1. SUBTASK 72-00-50-420-216 Connect the No. 5 Bearing Pressure Tube Assembly

    2. Refer to Figure.

    3. Attach the loop clamp bracket Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-020) to the external flange of the Turbine Exhaust Case with the two bolts Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-040) and two nuts Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-030).

    4. Torque the nuts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

    5. Attach the No. 5 Bearing pressure tube Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-010) to the bracket. Install a nut Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-015) and bolt Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-017) to the clamp and support assembly Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-016).

    6. Torque the nut to 36 lbfin to 45 lbfin (4.07 Nm to 5.08 Nm).

    7. Attach the No. 5 Bearing pressure tube Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-176) to the nipple.

    8. Torque the coupling nut to 200 lbfin to 225 lbfin (22.597 Nm to 25.422 Nm).

    9. Safety the nut with CoMat 02-141 LOCKWIRE.

    10. Attach the loop clamp bracket Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-200) to the tube heat shield with two washers Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-215), nut Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-210) and bolt Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-220).

    11. Torque the bolt to 36 lbfin to 45 lbfin (4.07 Nm to 5.08 Nm).

    12. Attach the bracket to the inner support of the Turbine Exhaust Case with two bolts Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-190) and two nuts Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-180).

    13. Torque the bolts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

    1. SUBTASK 72-00-50-420-217 Install the No. 5 Bearing Nozzle

    2. Refer to Figure.

    3. Install the new packings NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-040) and the No. 5 Bearing Packing Transfer Tube NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-030) into the No. 5 Bearing Nozzle NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-070).

    4. Install the two washers NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-020) and the two bolts NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-010) to attach the transfer tube to the Bearing Nozzle.

    5. Torque the bolts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

    6. Install a new packing NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-080) on the Bearing Nozzle.

    7. Install the Bearing Nozzle into the No. 5 Bearing compartment.

    8. Attach the Bearing Nozzle with two bolts NO.5 BEARING OIL JET AND FILTER (72-58-02, 01-060).

    9. Torque the bolts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

    10. Install the nipple Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-290) and a new packing Turbine Exhaust Case (TEC) Assembly And Related Parts (72-50-53, 20-300) Torque the nipple to 110 lbfin to 120 lbfin (12.43 Nm to 13.56 Nm).

    11. Make sure the No. 5 Pressure tube passage is clear by blowing air through from outer case fitting and make sure it is exiting jets in the compartment.

    1. SUBTASK 72-00-50-420-218-A00 Install the Blind Cap to the LP Turbine Shaft (Pre SBE 72-0227)

    2. Refer to Figure, Figure, Figure, Figure and Figure.

      NOTE

      Use of IAE 1J12263 Seal slider without IAE 1J12244 Sizing sleeve is not permitted.
      1. Extend the sealing ring and install it to the blind cap as follows.

      2. Put the blind cap LPT Shaft And Related Parts (72-50-41, 01-150) on to a work bench with the rear end down.

      3. Install the IAE 1J12263 Seal slider 1 off on the blind cap.

      4. Lubricate the new LPT Shaft And Related Parts (72-50-41, 01-160) sealing ring 1 off with CoMat 10-077 APPROVED ENGINE OILS.

      5. Lubricate the outer diameter faces of the seal slider and the blind cap with CoMat 10-077 APPROVED ENGINE OILS.

      6. Put the sealing ring on to the seal slider. The open side of the sealing ring must be in down direction.

      7. CAUTION

        MOVE THE SEALING RING SMOOTHLY AND EQUALLY OVER THE ALL CIRCUMFERENCE, IF NOT SO, THE SEALING RING IS EXTENDED LOCALLY. LOCAL EXTENSION CAN CAUSE DAMAGE TO THE SEALING RING.

        Push the sealing ring down with four or more fingers until it is installed into the groove of the blind cap.

      8. Remove the seal slider from the blind cap.

      1. CAUTION

        DO NOT INSTALL THE BLIND CAP AND THE SEALING RING INTO THE LP TURBINE SHAFT BEFORE Step THE SEALING DIAMETER IS EXTENDED. THE LP TURBINE SHAFT BORE CAN CAUSE DAMAGE TO THE EXTENDED SEALING RING.

        Make the sealing ring diameter smaller as follows.

      2. Put the IAE 1J12244 Sizing sleeve 1 off on to the work bench with the front end down.

      3. Lubricate the inner diameter face of the sizing sleeve and the outer diameter of the sealing ring with CoMat 10-077 APPROVED ENGINE OILS.

      4. Put the blind cap into the sizing sleeve. The diaphragm of the blind cap must be in down direction.

      5. Slowly push the blind cap down until it touches the work bench.

      6. Keep the blind cap in the sizing sleeve for ten or more minutes.

      7. Remove the sizing sleeve from the blind cap.

      1. Examine the sealing ring.

      2. Make sure that there is no damage on the surface.

      3. CAUTION

        DO NOT CORRECT A TWISTED CONDITION OF THE SEALING RING. DISCARD THE TWISTED SEALING RING.

        Make sure that the sealing ring is not twisted.

    3. Install the blind cap on the LP Turbine Shaft. Use the IAE 1P17041 Drier driver 1 off.

    4. Install the internal retaining ring LPT Shaft And Related Parts (72-50-41, 01-100).

    1. SUBTASK 72-00-50-420-218-C00 Install the Blind Cap to the LP Turbine Shaft (SBE 72-0227)

    2. SBE 72-0227: Provide a new blind cap with decreased seal land height.

    3. Refer to Figure and Figure.

      1. Install the new LPT Shaft And Related Parts (72-50-41, 01-160) sealing ring to the blind cap LPT Shaft And Related Parts (72-50-41, 01-150) as follows:

      2. Put the blind cap on to a work bench with the front end down.

      3. Install the IAE 1J12523 Seal slider 1 off on the blind cap.

      4. Lubricate the sealing ring with CoMat 10-077 APPROVED ENGINE OILS.

      5. Lubricate the outer diameter faces of the seal slider and the blind cap with CoMat 10-077 APPROVED ENGINE OILS.

      6. Put the sealing ring on the seal slider. The open side of the sealing ring must be in the up direction.

      7. CAUTION

        MOVE THE SEALING RING SMOOTHLY AND EQUALLY OVER ALL THE CIRCUMFERENCE. IF NOT SO, THE SEALING RING IS EXTENDED LOCALLY, LOCAL EXTENSION CAN CAUSE DAMAGE TO THE SEALING RING.

        Put the sealing ring down with four or more fingers until it is installed into the groove of the blind cap.

      8. Remove the seal slider from the blind cap.

      1. Examine the sealing ring.

      2. Make sure that there is no damage on the surface.

      3. CAUTION

        DO NOT CORRECT A TWISTED CONDITION OF THE SEALING RING. DISCARD THE TWISTED SEALING RING.

        Make sure that the sealing ring is not twisted.

    4. Install the blind cap to the LP Turbine Shaft. Use the IAE 1P17041 Drier 1 off.

    5. CAUTION

      DO NOT USE THE INTERNAL RETAINING RING P/N RR312 WITH THE BLIND CAP P/N 5A1705.

      Install the internal retaining ring LPT Shaft And Related Parts (72-50-41, 01-100).

    1. SUBTASK 72-00-50-420-219 Install the No. 5 Bearing Compartment Cover

      WARNING

      IF YOU DO NOT SECURE THE COMPARTMENT COVER DURING THE LEAK TEST THERE IS A RISK OF PERSONAL INJURY FROM THE RELEASED COVER.
    2. Refer to Figure.

    3. Install a new packing ENGINE-NO.5 BEARING COMPARTMENT COVER (72-58-01, 20-160) on to the No. 5 Bearing compartment cover ENGINE-NO.5 BEARING COMPARTMENT COVER (72-58-01, 20-120).

    4. Install the No. 5 Bearing compartment cover to the Turbine Exhaust Case.

      1. Do a leak check of the compartment cover and oil tubes.

      2. Install 13 work bolts to the compartment cover. Tighten the bolts.

      3. Install the IAE 1P17523 Blank-off Plate to the No. 5 Bearing outer oil feed tube. Refer to Figure.

      4. Install the IAE 1P16354 Vacuum Test Adapter to the No. 5 Bearing oil scavenge tube outlet with three bolts (part of the adapter). Tighten the bolts. Refer to Figure.

      5. Attach the hose on the IAE 6F01029 Pneumatic cart to the adapter.

      6. Control the air pressure to the adapter to 10 psig (68.95 kPa).

      7. Apply CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE or CoMat 10-045A LEAK CHECK FLUID, BUBBLES-TYPE around the cover and oil tube interfaces to check for leaks. Replace the seal of any leaking interface with a new seal.

      8. Do the leak test again.

      9. Remove the 13 work bolts.

    5. Install the No. 5 Bearing shields ENGINE-NO.5 BEARING COMPARTMENT COVER (72-58-01, 20-100) and ENGINE-NO.5 BEARING COMPARTMENT COVER (72-58-01, 20-080) on the No. 5 Bearing compartment cover. Align the bolt holes.

    6. Treat threads and underside of head of the bolts with CoMat 10-129 ANTI-SEIZE PASTE at assembly.

    7. Attach the 13 bolts. Torque the bolts to 62 lbfin to 72 lbfin (7.006 Nm to 8.136 Nm). Wipe off excess paste.

    1. SUBTASK 72-00-50-420-220 Install the Adapter and the Plate to the TEC

      1. Install the IAE 1P16354 Vacuum Test Adapter 1 off to the No. 5 Bearing outer oil scavenge tube, Figure.

      2. Make sure that the adapter has no damage.

      3. Lubricate the bolts, nuts and washers with CoMat 10-077 APPROVED ENGINE OILS.

      4. Attach the adapter to the No. 5 Bearing outer oil scavenge tube with four bolts. Torque the bolts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

      1. Install the IAE 1P17523 Blank-off Plate 1 off to the No. 5 Bearing outer oil feed tube, Figure.

      2. Make sure that the plate has no damage.

      3. Lubricate the bolts, nuts and washers with CoMat 10-077 APPROVED ENGINE OILS.

      4. Attach the plate to the No. 5 Bearing outer oil feed with two bolts. Torque the bolts to 85 lbfin to 105 lbfin (9.60 Nm to 11.86 Nm).

    1. SUBTASK 72-00-50-420-221 Do an Evacuation Check for the No. 5 Bearing Compartment

    2. Refer to Figure.

    3. Connect the hose of the IAE 6F10030 Vacuum test cart 1 off to the nipple of the IAE 1P16354 Vacuum Test Adapter 1 off.

    4. Attach the cart vacuum gage hose to the plug of the vacuum test adapter.

      NOTE

      Refer to the manufacturer manual for the operation of the vacuum test cart.
    5. Set the air pressure at the test port to -20 inHg (-508 mmHg gage). Based on the ambient pressure, refer to the table below for the vacuum pressure in psia.

      Ambient Pressure of the Day (psia)

      Vacuum Pressure (psia)

      14.7

      4.9

      14.5

      4.7

      14.3

      4.5

      14.1

      4.3

      13.9

      4.1

      13.7

      3.9

      13.5

      3.7

      13.3

      3.5

      13.1

      3.3

      Vacuum pressure (psia) = Ambient pressure of the day (psia) - 9.8 psia

    6. Read the airflow indicated by the rotor meters on the vacuum test cart.

    7. Record the indicated airflow.

    8. If the indication is more than 10 PPH (4.54 kg per hour) reject the module.

    9. Stop the vacuum pump.

    1. SUBTASK 72-00-50-420-222 Remove the Vacuum Test Cart, the Adapter and the Plate

    2. Disconnect the hose of the vacuum test cart from the adapter. Refer to Figure.

    3. Remove the plate and the adapter. Refer to Figure and Figure.

    1. SUBTASK 72-00-50-420-223 Install the Module Dressings

    2. Install the module dressings. Refer to TASK 72-00-50-420-005-B00 (INSTALLATION-007).

  1. Figure: Fits and Clearances at Interface N-50/10 and N-50/50

    Fits and Clearances at Interface N-50/10 and N-50/50

    Figure: Fits and Clearances at Interface N-50/10 and N-50/50

    Fits and Clearances at Interface N-50/10 and N-50/50

    Figure: Fits and Clearances of the No.5 Bearing and the TEC

    Fits and Clearances of the No.5 Bearing and the TEC

    Figure: Install the No.5 Bearing Seal Spacers and the Inner Race of the No.5 Bearing

    Install the No.5 Bearing Seal Spacers and the Inner Race of the No.5 Bearing

    Figure: Install the Guide Support to the LP Turbine Shaft

    Install the Guide Support to the LP Turbine Shaft

    Figure: Install the Remove/Installation Fixture

    Install the Remove/Installation Fixture

    Figure: Installation of the Bolts and Brackets at the Front Flange of the TEC

    Installation of the Bolts and Brackets at the Front Flange of the TEC

    Figure: Installation of the Bolts and Brackets at the Front Flange of the TEC

    Installation of the Bolts and Brackets at the Front Flange of the TEC

    Figure: Installation of the Bolts and Brackets at the Front Flange of the TEC

    Installation of the Bolts and Brackets at the Front Flange of the TEC

    Figure: Install the No. 5 Bearing Nozzle

    Install the No. 5 Bearing Nozzle

    Figure: Connect the No. 5 Bearing Pressure Tube Assembly

    Connect the No. 5 Bearing Pressure Tube Assembly

    Figure: Install the Turbine Shaft Rear Lock Nut

    Install the Turbine Shaft Rear Lock Nut

    Figure: Install the Blind Cap

    Install the Blind Cap

    Figure: Connect the No. 5 Bearing Pressure Tube Assembly

    Connect the No. 5 Bearing Pressure Tube Assembly

    Figure: Installation of the Adapter to No. 5 Bearing Outer Oil Scavenge Tube

    Installation of the Adapter to No. 5 Bearing Outer Oil Scavenge Tube

    Figure: Installation of the Plate to the No. 5 Bearing Outer Oil Feed Tube

    Installation of the Plate to the No. 5 Bearing Outer Oil Feed Tube

    Figure: Connect the Fitting of the Vacuum Test Cart to the Adapter

    Connect the Fitting of the Vacuum Test Cart to the Adapter

    Figure: Pre SBE 72-0227: Installation of the Sealing Ring onto the Blind Cap

    Pre SBE 72-0227: Installation of the Sealing Ring onto the Blind Cap

    Figure: SBE 72-0227: Installation of the Sealing Ring onto the Blind Cap

    SBE 72-0227: Installation of the Sealing Ring onto the Blind Cap

    Figure: Pre SBE 72-0227: Installation of the Sealing Ring into the Sizing Sleeve

    Pre SBE 72-0227: Installation of the Sealing Ring into the Sizing Sleeve

    Figure: Installed Condition of the Sealing Ring

    Installed Condition of the Sealing Ring

    Figure: Installation of the Sealing Ring on the Blind Cap Method 2

    Installation of the Sealing Ring on the Blind Cap Method 2

    Figure: Example of Incorrect Installation of the Sealing Rings on the Blind Cap

    Example of Incorrect Installation of the Sealing Rings on the Blind Cap

    Figure: Oil Jet Air Flow Check

    Oil Jet Air Flow Check

    Figure: Installation of Blind Cap and Retaining Ring

    Installation of Blind Cap and Retaining Ring

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised Step 24.G (CAS-97645-Q0Z2L3)

Link not Found
Manufacturer Code:03530
Enterprise Name:AMERICAN GAS AND CHEMICAL CO LTD
BU Name:AMERICAN GAS AND CHEMICAL CO LTD
Street:220 PEGASUS AVE
City:NORTHVALE
State:NJ
Zip Code:07647
Country:USA
Phone Number:1-201-767-7300, 1-800-526-1008
Fax Number:1-201-767-1741
Internet:www.amgas.com
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:34568
Enterprise Name:TIODIZE CO., INC.
BU Name:TIODIZE CO., INC.
Street:5858 ENGINEER DRIVE
City:HUNTINGTON BEACH
State:CA
Zip Code:92649
Country:USA
Phone Number:1-714-898-4377
Fax Number:1-714-891-7467
Internet:www.tiodize.com
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Link not Found
Manufacturer Code:LOCAL
Supply Number:CoMat 02-141
Type:sp01
Supply Short Name:CoMat 02-141 LOCKWIRE
Supply Name:CoMat 02-141 LOCKWIRE
Specification Groups:
Doc NumberType
AS3214-02 (0.8 mm)AMS 5689
Suppliers:
ManufacturerRemarks
LOCAL
81343
IE508
58401
Manufacturer Code:00BB6
Supply Number:CoMat 07-038
Type:sp01
Supply Short Name:CoMat 07-038 AIR DRYING ENAMEL
Supply Name:CoMat 07-038 AIR DRYING ENAMEL
Specification Groups:
Doc NumberType
OMAT:7/22B (RR REF)IP9138 R1
JCR-029 (JAEC REF)
Suppliers:
ManufacturerRemarks
00BB6
K3504
Manufacturer Code:03530
Supply Number:CoMat 10-045
Type:sp01
Supply Short Name:CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE
Supply Name:CoMat 10-045 LEAK CHECK FLUID, BUBBLES-TYPE
Specification Groups:
Doc NumberType
LEAK TEC 372E
Suppliers:
ManufacturerRemarks
03530
Manufacturer Code:02570
Supply Number:CoMat 10-045A
Type:sp01
Supply Short Name:CoMat 10-045A LEAK CHECK FLUID, BUBBLES-TYPE
Supply Name:CoMat 10-045A LEAK CHECK FLUID, BUBBLES-TYPE
Specification Groups:
Doc NumberType
SNOOP LIQUID LEAK DETECTOR
Suppliers:
ManufacturerRemarks
02570
U9113
Manufacturer Code:X333X
Supply Number:CoMat 10-077
Type:sp01
Supply Short Name:CoMat 10-077 APPROVED ENGINE OILS
Supply Name:CoMat 10-077 APPROVED ENGINE OILS
Specification Groups:
Doc NumberType
For V2500-A1/A5/D5 models - Refer to V2500 Service Bulletin ENG-79-0108
For V2500-E5 model - Refer to Service Bulletin E5-79-0001
Suppliers:
ManufacturerRemarks
X333X
Manufacturer Code:34568
Supply Number:CoMat 10-129
Type:sp01
Supply Short Name:CoMat 10-129 ANTI-SEIZE PASTE
Supply Name:CoMat 10-129 ANTI-SEIZE PASTE
Specification Groups:
Doc NumberType
TIODIZE T8E PASTE
Suppliers:
ManufacturerRemarks
34568
Manufacturer Code:LOCAL
Tool Number:Electronic balance crane
Tool Name:Electronic balance crane
Manufacturer Code:0AM53
Tool Number:IAE 1F10016
Tool Name:IAE 1F10016 Mechanical wrench
Manufacturer Code:0AM53
Tool Number:IAE 1F10026
Tool Name:IAE 1F10026 Hydraulic hand pump
Manufacturer Code:0AM53
Tool Number:IAE 1F10033
Tool Name:IAE 1F10033 Hydraulic installation pusher
Manufacturer Code:0AM53
Tool Number:IAE 1F10034
Tool Name:IAE 1F10034 Hydraulic installation pusher
Manufacturer Code:0AM53
Tool Number:IAE 1F10038
Tool Name:IAE 1F10038 Torque wrench
Manufacturer Code:0AM53
Tool Number:IAE 1F10039
Tool Name:IAE 1F10039 Anti-torque adapter
Manufacturer Code:0AM53
Tool Number:IAE 1F10040
Tool Name:IAE 1F10040 Anchor wrench plate
Manufacturer Code:0AM53
Tool Number:IAE 1F10051
Tool Name:IAE 1F10051 Two cable sling
Manufacturer Code:0AM53
Tool Number:IAE 1F10073
Tool Name:IAE 1F10073 remove/installation fixture
Manufacturer Code:0AM53
Tool Number:IAE 1F10075
Tool Name:IAE 1F10075 Support pedestal
Manufacturer Code:0AM53
Tool Number:IAE 1F10076
Tool Name:IAE 1F10076 Locking collar
Manufacturer Code:0AM53
Tool Number:IAE 1F10178
Tool Name:IAE 1F10178 Storage and Turnover adapter
Manufacturer Code:0AM53
Tool Number:IAE 1J12244
Tool Name:IAE 1J12244 Sizing sleeve
Manufacturer Code:0AM53
Tool Number:IAE 1J12263
Tool Name:IAE 1J12263 Seal slider
Manufacturer Code:0AM53
Tool Number:IAE 1J12523
Tool Name:IAE 1J12523 Seal slider
Manufacturer Code:0AM53
Tool Number:IAE 1M14143
Tool Name:IAE 1M14143 Support fixture
Link not Found
Manufacturer Code:0AM53
Tool Number:IAE 1P14041
Tool Name:IAE 1P14041 Drier
Manufacturer Code:0AM53
Tool Number:IAE 1P16354
Tool Name:IAE 1P16354 Vacuum Test Adapter
Manufacturer Code:0AM53
Tool Number:IAE 1P16374
Tool Name:IAE 1P16374 Wrench support
Manufacturer Code:0AM53
Tool Number:IAE 1P16377
Tool Name:IAE 1P16377 Guide support
Manufacturer Code:0AM53
Tool Number:IAE 1P17041
Tool Name:IAE 1P17041 Drier
Manufacturer Code:0AM53
Tool Number:IAE 1P17523
Tool Name:IAE 1P17523 Blank-off Plate
Manufacturer Code:0AM53
Tool Number:IAE 6F01029
Tool Name:IAE 6F01029 Pneumatic cart
Manufacturer Code:0AM53
Tool Number:IAE 6F10030
Tool Name:IAE 6F10030 Vacuum test cart