TASK 72-50-00-430-002-B00 LP Turbine (LPT) And Turbine Exhaust Case (TEC) Unit - Assemble The TEC To The LPT Module, Assembly-002 - SBE 72-0063

DMC:V2500-A1-72-50-0000-02B-710A-B|Issue No:003.00|Issue Date:2017-05-01

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-A1 and POST SBE 72-0063

Common Information

TASK 72-50-00-430-002-B00 LP Turbine (LPT) And Turbine Exhaust Case (TEC) Unit - Assemble The TEC To The LPT Module, Assembly-002 - SBE 72-0063

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.

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

For standard torque data and procedures, refer to SPM TASK 70-41-01-400-501, SPM TASK 70-41-00-400-501 and SPM TASK 70-41-01-400-501.

Special torque data and 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.

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.

Refer to TASK 72-50-00-990-501 for a sectional view of the LP turbine module.

For oil service tube installation reference the SPM TASK 70-41-00-400-501 for general torque tightening procedures.

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 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 1F10073 remove/installation fixture0AM53IAE 1F100731
IAE 1F10074 Guide pogo stick0AM53IAE 1F100741
IAE 1F10076 Locking collar0AM53IAE 1F100761
IAE 1F10153 Installation rod0AM53IAE 1F101531
IAE 1F10178 Storage and Turnover adapter0AM53IAE 1F101781
IAE 1P16374 Wrench support0AM53IAE 1P163741
IAE 1P16426 remove/installation driver0AM53IAE 1P164261

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-141 LOCKWIRELOCALCoMat 02-141
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Washer2
Packing3
Packing1
Washer2
Packing1

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-50-00-220-089 Reference Fits and Clearances of 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 ENGINE-EXHAUST CASE AND FITTINGS (72-50-53, 21-350)

      The Stage 6 Inner Turbine Air Seal ATTACH PARTS & FITTINGS-LP TURBINE MINI MODULE (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 ENGINE-EXHAUST CASE AND FITTINGS (72-50-53, 21-350)

      The Stage 6 Inner Turbine Air Seal ATTACH PARTS & FITTINGS-LP TURBINE MINI MODULE (72-50-00, 01-240)

      No. 5 Bearing Housing

      141.001

      Clear

      141.099

      0.800

      Stage 6 Inner Turbine Air Seal

      140.099

      1.001

      140.200

      Clear

    1. SUBTASK 72-50-00-220-090 Reference Fits and Clearances of the LP Turbine Case and the Turbine Exhaust Case 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 ENGINE-LP TURBINE CASE AND ROTOR (72-50-10, 01-010)

      Turbine Exhaust Case ENGINE-EXHAUST CASE AND FITTINGS (72-50-53, 21-300)

      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 ENGINE-LP TURBINE CASE AND ROTOR (72-50-10, 01-010)

      Turbine Exhaust Case ENGINE-EXHAUST CASE AND FITTINGS (72-50-53, 21-300)

      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 72-50-00-220-091 References Fits and Clearances of the LP Turbine 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 ENGINE-LP TURBINE SHAFT (72-50-41, 01-200)

      The 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 ENGINE-LP TURBINE SHAFT (72-50-41, 01-200)

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

      LP Turbine Shaft Diameter

      92.009

      Intf

      92.019

      0.008

      No. 5 Bearing Bore

      91.991

      0.028

      91.999

      Intf

    1. SUBTASK 72-50-00-220-092 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 ENGINE-LP TURBINE SHAFT (72-50-41, 01-200)

      The 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 ENGINE-LP TURBINE SHAFT (72-50-41, 01-200)

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

      LP Turbine Shaft Diameter

      94.976

      Clear

      94.991

      0.010

      No. 5 Bearing Seal Spacer

      95.001

      0.048

      95.024

      Clear

    1. SUBTASK 72-50-00-220-093-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 ENGINE-LP TURBINE SHAFT (72-50-41, 01-200)

      The 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 ENGINE-LP TURBINE SHAFT (72-50-41, 01-200)

      The 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 72-50-00-220-093-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-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 ENGINE-LP TURBINE SHAFT (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 ENGINE-LP TURBINE SHAFT (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 72-50-00-220-094 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 72-50-00-220-095 Reference Fits and Clearances of the No. 5 Bearing Nozzle and the Turbine Exhaust Case 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)

      The Turbine Exhaust Case ENGINE-EXHAUST CASE AND FITTINGS (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)

      The Turbine Exhaust Case ENGINE-EXHAUST CASE AND FITTINGS (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 72-50-00-220-096 Reference Fits and Clearances of the No. 5 Bearing Transfer Tube and the Turbine Exhaust Case 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)

      Turbine Exhaust Case ENGINE-EXHAUST CASE AND FITTINGS (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)

      Turbine Exhaust Case ENGINE-EXHAUST CASE AND FITTINGS (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 72-50-00-220-097 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 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 in millimetres)

      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 72-50-00-220-098 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 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 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 72-50-00-220-099 Reference Fits and Clearances of the Stage 7 Turbine Blade and the Turbine Exhaust Case 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 ENGINE-LP TURBINE BLADES (72-50-32, 01-010)

      The Turbine Exhaust Case ENGINE-EXHAUST CASE AND FITTINGS (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 ENGINE-LP TURBINE BLADES (72-50-32, 01-010)

      The Turbine Exhaust Case ENGINE-EXHAUST CASE AND FITTINGS (72-50-53, 21-300)

      Stage 7 LP Turbine Blade

      1.879 Minimum

      Turbine Exhaust Case

      4.493 Maximum

    1. SUBTASK 72-50-00-430-089-A00 Install the Carbon Seal to the LP Turbine Shaft, , Detail A (Pre SBE 72-0162)

    2. Refer to Figure.

    3. Install the carbon seal to the rear end of the LP turbine shaft. Make sure that the groove of the carbon seal points to the rear.

    4. 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.

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

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

    7. Operate the hydraulic pump to move the carbon seal in to 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 72-50-00-430-089-B00 Install the Carbon Seal to the LP Turbine Shaft, , Detail B (SBE 72-0162)

    2. Refer to Figure.

    3. SBE 72-0162: Introduce a new No. 5 bearing face seal

      1. Do an inspection of the No. 5 bearing face seal.

        NOTE

        The old No. 5 bearing face seal have a radial thickness of 0.338 in. to 0.346 in. (8.585 mm to 8.788 mm). Do not use these seals.
      2. Make sure that the radial thickness is 0.234 in. to 0.238 in. (5.944 mm to 6.045 mm).

      1. Install the No. 5 bearing carbon seal as follows:

      2. Use a No. 5 bearing carbon seal from the seal option ENGINE-NO.5 BEARING ASSEMBLY AND SEAL (72-50-42, 20-140).

      3. Soak the carbon seal in hot CoMat 10-077 APPROVED ENGINE OILS for ten minutes.

      4. Install the front seal plate with the flat surface forward.

      5. Install the carbon seal. Use light pressure and push forward.

      6. Install the rear seal plate. Make sure the groove points to the rear.

    1. SUBTASK 72-50-00-430-089-C00 Install the No. 5 Bearing Seal and Spacers onto the LP Turbine Shaft (Pre SBE 72-0165)

      CAUTION

      MAKE SURE THE LIP OF THE NO. 5 BEARING SEAL SPACER POINTS TOWARDS THE REAR.
    2. Refer to Figure.

    3. Install the No. 5 bearing seal spacers 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 (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 (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 carbon seal in to 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 72-50-00-430-089-D00 Install the No. 5 Bearing Seal and Spacers onto 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 (20-140) with CoMat 10-077 APPROVED ENGINE OILS with a lint free cloth.

    6. Install the carbon seal to the rear end of the LP turbine shaft.

    7. Install the No. 5 bearing seal spacer (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 72-50-00-430-090-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 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 in to 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 72-50-00-430-090-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 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 72-50-00-430-091 Install the Guide Pogo Stick to the LP Turbine Shaft

    2. Refer to Figure.

    3. Install the IAE 1F10074 Guide pogo stick 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 pogo stick is installed correctly to the LP turbine shaft. Turn clockwise the screw at the rear end of the guide pogo stick to attach the pogo stick to the LP turbine shaft.

    1. SUBTASK 72-50-00-430-092 Install the Remove/Installation Fixture to the Turbine Exhaust Case

    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 fixture with the 13 screws and washers. Tighten the screws.

    1. SUBTASK 72-50-00-430-093 Install the Turbine Exhaust Case to the LP Turbine Case

    2. Refer to Figure and Figure.

    3. Release the turbine exhaust case and lift it from the IAE 1F10178 Storage and Turnover adapter 1 off.

    4. Install the turbine exhaust case to the IAE 1F10074 Guide pogo stick 1 off front end down.

    5. Move the turbine exhaust case down to the rear flange of the LP turbine case. Align the dowel pins.

    6. Turn the jackscrew (part of the IAE 1F10073 remove/installation fixture) clockwise to the stop position. Safety the jackscrew in the position with the IAE 1F10076 Locking collar 1 off.

    7. CAUTION

      MAKE SURE THAT THE STAGE 6 AIR SEAL, THE NO. 5 BEARING AND THE CARBON SEAL 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 ONTO THE BOLTS. DO NOT TURN THE BOLTS OR MAKE TO AND FRO MOVEMENTS. THE TURBINE EXHAUST CASE/LP TURBINE CASE AND/OR THE BOLTS CAN BE DAMAGED BY SCORES.

        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. CAUTION

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

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

    8. 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 locking collar and the remove/installation fixture.

        NOTE

        If the rear lock nut is not installed, continue with Step.
      3. Remove the guide pogo stick.

    1. SUBTASK 72-50-00-430-094 Install the No. 5 Bearing Nozzle

    2. Refer to Figure.

    3. Install three 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) in to 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 to the bearing nozzle.

    7. Install the bearing nozzle in to the No. 5 bearing compartment.

    8. Attach the bearing nozzle with the 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 ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-290) and a new packing ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-300). Torque the nipple to 110 lbfin to 120 lbfin (12.43 Nm to 13.56 Nm).

    1. SUBTASK 72-50-00-430-095 Connect the No. 5 Bearing Pressure Tube Assembly

    2. Refer to Figure.

    3. Attach the loop clamp bracket ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-020) to the external flange of the turbine exhaust case with the two bolts ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-040) and two nuts ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-030).

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

    5. Attach the No. 5 bearing pressure tube ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-010) to the bracket. Install a nut ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-015) and bolt ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-017) to the clamp and support assembly ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-016).

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

    7. Attach the No. 5 bearing pressure tube ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-176) to the nipple.

    8. Torque the coupling nut 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 ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-200) to the tube heat shield with two washers ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-215), nut ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-210) and bolt ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-220).

    11. Torque the bolt 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 ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-190) and two nuts ENGINE - EXHAUST CASE AND FITTINGS (72-50-53, 20-180).

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

    14. WARNING

      BE CAREFUL WHEN YOU USE COMPRESSED AIR. PUT ON PROTECTIVE CLOTHING AND GOGGLES.

      Prove No. 5 pressure tube passage is clear by blowing air through from the outer case fitting and make sure it comes out of the jets in the compartment.

  1. SUBTASK 72-50-00-430-096

    1. SUBTASK 72-50-00-430-097 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 turbine exhaust case.

    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. Safety 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. Put an angle of turn of five to eight degrees to the rear lock nut.

    10. Operate the mechanical wrench to release the torque until the torque value is zero.

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

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

    13. Put an angle of turn of five to eight degrees to the rear lock nut.

    14. Do Step again.

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

    16. If the correlation mark is within limit, apply last angle of turn of five to eight degrees to the rear lock nut.

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

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

    19. Align the slot of the rear lock nut with the slot of the LP turbine shaft rear end. The alignment of the rear lock nut must be in torque direction.

      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.

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

  2. Figure: Fits and Clearances at Interface N50/50 and N50/10

    Sheet 1

    Legend
    Fits and Clearances at Interface N50/50 and N50/10

    Sheet 1

    Close

    Figure: Fits and Clearances at Interface N50/50 and N50/10

    Sheet 2

    Legend
    Fits and Clearances at Interface N50/50 and N50/10

    Sheet 2

    Close

    Figure: Fits and Clearances of No. 5 Bearing and the Turbine Exhaust Case

    Fits and Clearances of No. 5 Bearing and the Turbine Exhaust Case

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

    Sheet 1

    Legend
    Install the Carbon Seal and the Inner Race of the No. 5 Bearing

    Sheet 1

    Close

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

    Sheet 2

    Legend
    Install the Carbon Seal and the Inner Race of the No. 5 Bearing

    Sheet 2

    Close

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

    Sheet 1

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

    Sheet 1

    Close

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

    Sheet 2

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

    Sheet 2

    Close

    Figure: Install the Turbine Shaft Rear Lock Nut

    Install the Turbine Shaft Rear Lock Nut

    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 Exhaust Case

    Install the Turbine Exhaust Case

    Figure: Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 1

    Legend
    Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 1

    Close

    Figure: Installation of the Bolts and Brackets at the Front flange of the Turbine Exhaust Case

    Sheet 2

    Legend
    Installation of the Bolts and Brackets at the Front flange of the Turbine Exhaust Case

    Sheet 2

    Close

    Figure: Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 3

    Legend
    Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 3

    Close

    Figure: Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 4

    Legend
    Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 4

    Close

    Figure: Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 5

    Legend
    Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 5

    Close

    Figure: Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 6

    Legend
    Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 6

    Close

    Figure: Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 7

    Legend
    Installation of the Bolts and Brackets at the Front Flange of the Turbine Exhaust Case

    Sheet 7

    Close

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Updated procedure, fits and clearances tables to standard format. (Editorial)

Link not Found
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
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: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: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 1F10073
Tool Name:IAE 1F10073 remove/installation fixture
Manufacturer Code:0AM53
Tool Number:IAE 1F10074
Tool Name:IAE 1F10074 Guide pogo stick
Manufacturer Code:0AM53
Tool Number:IAE 1F10076
Tool Name:IAE 1F10076 Locking collar
Manufacturer Code:0AM53
Tool Number:IAE 1F10153
Tool Name:IAE 1F10153 Installation rod
Manufacturer Code:0AM53
Tool Number:IAE 1F10178
Tool Name:IAE 1F10178 Storage and Turnover adapter
Manufacturer Code:0AM53
Tool Number:IAE 1P16374
Tool Name:IAE 1P16374 Wrench support
Manufacturer Code:0AM53
Tool Number:IAE 1P16426
Tool Name:IAE 1P16426 remove/installation driver