TASK 72-41-30-440-003-A00 HPC Front Case And Vane Assembly - Install The Variable Inlet Guide Vanes, Assembly-003

DMC:V2500-A1-72-41-3000-02A-710A-B|Issue No:004.00|Issue Date:2019-05-01

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

Common Information

TASK 72-41-30-440-003-A00 HPC Front Case And Vane Assembly - Install The Variable Inlet Guide Vanes, Assembly-003

General

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

All of the temporary marks made in this procedure must be removed after completion of this task.

For standard torque data and procedures, refer to SPM TASK 70-41-00-400-501, SPM TASK 70-41-01-400-501 and SPM TASK 70-41-02-400-501.

Special torque data and assembly tolerances are included in the procedure.

Lubricate all threads and touch 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 70-44-01-400-501.

After assembly apply CoMat 07-038 AIR DRYING ENAMEL to any damaged surface protection, joint flanges and parts used to attach. Use the correct colour of the air drying enamel. Refer to the SPM TASK 70-63-02-380-501.

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.

Pre SBE 72-0027: Refer to Figure for a sectional view of the HP Compressor Front Case.

SBE 72-0027: Refer to Figure for a sectional view of the HP Compressor Front Case.

The Fits and Clearances, NEW PARTS DIMENSIONS and REJECT IF MORE THAN columns will be used by most operators. This permits the full use of the maximum wear allowance and a reduction in the number of parts which are rejected, is possible.

As long as REJECT IF MORE THAN columns do not include reject values, NEW PART DIMENSIONS do not have to be measured before assembly, as there are no reject-if criteria. Values are only valid for new parts, not for worn parts.

The column WORN PART DIMENSION (Non-select) is included for operators who want to have full interchangeability. If this column is used an increase in the number of parts which are rejected is possible.

After the part has been in service for some time the REJECT IF MORE THAN and WORN PART DIMENSIONS could be changed. The operator must tell IAE and if agreed the manual will be changed.

The abbreviation Intf shows an interference or tight fit. This causes REJECT IF MORE THAN to become REJECT IF LESS THAN.

The abbreviation clear shows a clearance fit.

This TASK gives the procedure to install the variable inlet guide vanes (VIGV). The subsequent TASKS give the procedure to assemble HP Compressor Front Cases.

Install the Stage 3 to 6 Rotor Path Rings Pre SBE 72-0027 by TASK 72-41-30-440-001-A00 (ASSEMBLY-001).

Install the Stage 5 and 6 Rotor Path Rings SBE 72-0027 by TASK 72-41-30-440-001-B00 (ASSEMBLY-001).

Measure and then machine Stage 6 VSV and the Stage 3 to 6 Rotor Path Linings by TASK 72-41-30-440-002-A00 (ASSEMBLY-002).

Install the Stage 3 VSV by TASK 72-41-30-440-004-A00 (ASSEMBLY-004).

Install the Stage 4 VSV by TASK 72-41-30-440-005-A00 (ASSEMBLY-005).

Install the Stage 5 VSV by TASK 72-41-30-440-006-A00 (ASSEMBLY-006).

Install the Stage 6 VSV by TASK 72-41-30-440-007-A00 (ASSEMBLY-007).

Install the VIGV and the Stage 3 to 6 Connector Assemblies by TASK 72-41-30-440-008-A00 (ASSEMBLY-008).

Measure the HP Compressor Front Cases by TASK 72-41-30-440-009-A00 (ASSEMBLY-009).

Disassemble the HP Compressor Front Cases by TASK 72-41-30-440-010-A00 (ASSEMBLY-010).

Check and Set VSV System with Optimised Build and Setting Clearances - SBE 72-0402 by TASK 72-41-30-440-011-A00 (ASSEMBLY-011).

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 1R18248 Rigging pin0AM53IAE 1R182484
IAE 1R18638 Rigging pin0AM53IAE 1R186384
IAE 1R18250 Split ring assembly0AM53IAE 1R182501
IAE 1R18260 Bushing assembly tool0AM53IAE 1R182601
IAE 1R18277 Air plug gage0AM53IAE 1R182771
IAE 1R18278 Setting ring0AM53IAE 1R182781
IAE 1R18279 Setting ring0AM53IAE 1R182791
IAE 1R18280 Air gage unit0AM53IAE 1R182801
IAE 1R18295 Bushing assembly tool0AM53IAE 1R182951
IAE 1R18423 Rigging pin0AM53IAE 1R184234
IAE 1R18892 Rigging pin0AM53IAE 1R188924
IAE 1R19633 Split ring assembly0AM53IAE 1R196331
IAE 1R18579 Pusher installation tool0AM53IAE 1R18579
IAE 1R18576 Pusher installation tool0AM53IAE 1R18576
IAE 1R18577 Bushing installation tool0AM53IAE 1R18577
IAE 1R18573 Cylinder, hydraulic0AM53IAE 1R18573
IAE 1R18582 Pusher installation tool0AM53IAE 1R18582
IAE 1R19633 Split ring assembly0AM53IAE 1R19633

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-363 MARKING PENLOCALCoMat 02-363
CoMat 04-007 SILICONE GREASELOCALCoMat 04-007
CoMat 07-038 AIR DRYING ENAMELk3504CoMat 07-038
CoMat 10-077 APPROVED ENGINE OILSX333XCoMat 10-077
CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R)LOCALCoMat 10-108

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-41-30-220-061 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1201 (Pre SBE 70-0052 and SBE 70-0052)

    2. Refer to Figure.

    3. SBE 70-0052: Engine - Additional source for variable stator vane spindle bushings.

    4. Reference dimensions at location 1201. If required use the data written as a note in TASK 72-41-32-200-000 and TASK 72-41-31-200-000.

      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 1201

      VIGV ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500 And 01-600), Spindle Location In The Pre SBE 70-0052:

      VIGV Bush ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-241, 01-242 Or 01-243), Or

      VIGV Bush ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-241, 01-242, 01-243, 01-245, 01-246 Or 01-247)

      VIGV Spindle Diameter

      0.5472

      0.5492

      0.0018

      VIGV Bush Bore

      0.5511

      0.0050

      0.5522

      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 1201

      VIGV ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500 And 01-600), Spindle Location In The Pre SBE 70-0052:

      VIGV Bush ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-241, 01-242 Or 01-243), Or

      VIGV Bush ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-241, 01-242, 01-243, 01-245, 01-246 Or 01-247)

      VIGV Spindle Diameter

      13.900

      13.952

      0.048

      VIGV Bush Bore

      14.000

      0.127

      14.027

    1. SUBTASK 72-41-30-220-064 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1205

    2. Refer to Figure.

    3. Reference dimensions at location 1205. If required use the data written as a note in TASK 72-41-32-200-000 and TASK 72-41-33-200-000.

      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 1205

      VIGV ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500 And 01-600), Spindle

      Location In The Half Bush ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190)

      VIGV Spindle Diameter

      0.2709

      0.2730

      0.0025

      Half Bush Bore

      0.2756

      0.0055

      0.2765

      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 1205

      VIGV ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500 And 01-600), Spindle

      Location In The Half Bush ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190)

      VIGV Spindle Diameter

      6.881

      6.993

      0.067

      Half Bush Bore

      7.000

      0.141

      7.022

    1. SUBTASK 72-41-30-220-065 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1206

    2. Refer to Figure.

    3. Reference dimensions at location 1206. If required use the data written as a note in TASK 72-41-32-200-000 and TASK 72-41-33-200-000.

      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 1206

      VIGV ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500 And 01-600), Inner Spindle

      Location In The Half Bush ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190)

      VIGV Inner Spindle Length

      5.14027

      Intf

      5.15641

      0.00037

      Half Bush Outer Length

      5.13104

      0.02537

      5.13990

      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 1206

      VIGV ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500 And 01-600), Inner Spindle

      Location In The Half Bush ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190)

      VIGV Inner Spindle Length

      130.5630

      Intf

      130.9730

      0.0095

      Half Bush Outer Length

      130.3285

      0.6445

      130.5535

    1. SUBTASK 72-41-30-220-066 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1208

    2. Refer to Figure.

    3. Reference dimensions at location 1208. If required use the data written as a note in TASK 72-41-32-200-000 and TASK 72-41-33-200-000.

      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 1208

      VIGV ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500 And 01-600), Inner Spindle

      Location In The Half Bush ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190)

      VIGV Inner Spindle Length

      6.059

      6.064

      0.0078

      Half Bush Outer Length

      6.072

      0.0251

      6.084

      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 1208

      VIGV ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500 And 01-600), Inner Spindle

      Location In The Half Bush ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190)

      VIGV Inner Spindle Length

      153.902

      154.032

      0.200

      Half Bush Outer Length

      154.232

      0.640

      154.542

    1. SUBTASK 72-41-30-220-067 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1301

    2. Refer to Figure.

    3. Reference dimensions at location 1301. If required use the data written as a note in TASK 72-41-34-200-000.

      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 1301

      VIGV Lever ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-100 And 02-140)

      Location In The Bush ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-460 And 02-560)

      VIGV Lever Pin Diameter

      0.2353

      0.2358

      0.0004

      Bush Inner Bore

      0.2362

      0.0016

      0.2369

      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 1301

      VIGV Lever ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-100 And 02-140)

      Location In The Bush ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-460 And 02-560)

      VIGV Lever Pin Diameter

      5.978

      5.990

      0.01

      Bush Inner Bore

      6.000

      0.04

      6.018

    1. SUBTASK 72-41-30-220-138 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1263 (Pre SBE 70-0052 and SBE 70-0052)

    2. Refer to Figure.

    3. SBE 70-0052: Engine - Additional source for variable stator vane spindle bushings.

    4. Reference dimensions at location 1263. If required use the data written as a note in TASK 72-41-30-200-000 and TASK 72-41-31-200-000.

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

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      Non-select

      REJECT IF

      MORE THAN

      LOCATION 1263

      VIGV Bush ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-241, 01-242 Or 01-243), Or SBE 70-0052:

      VIGV Bush ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-241, 01-242, 01-243 01-245, 01-246 Or 01-247)

      Location With The Sealing Washer ENGINE-HP COMPRESSOR FRONT CASES AND VANES (72-41-30, 01-100)

      VIGV Bush Inner Flange Thickness

      0.055

      0.058

      0.003

      Sealing Washer Thickness

      0.049

      0.009

      0.052

      Table 12. Fits and Clearances (all dimensions in millimetres)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      Non-select

      REJECT IF

      MORE THAN

      LOCATION 1263

      VIGV Bush ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-241, 01-242 Or 01-243), Or SBE 70-0052:

      VIGV Bush ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-241, 01-242, 01-243 01-245, 01-246 Or 01-247)

      Location With The Sealing Washer ENGINE-HP COMPRESSOR FRONT CASES AND VANES (72-41-30, 01-100)

      VIGV Bush Inner Flange Thickness

      1.387

      1.463

      0.077

      Sealing Washer Thickness

      1.250

      0.213

      1.310

    1. SUBTASK 72-41-30-220-139 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1359

    2. Refer to Figure.

    3. Reference dimensions at location 1359. If required use the data written as a note in TASK 72-41-34-200-000.

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

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      Non-select

      REJECT IF

      MORE THAN

      LOCATION 1359

      Upper And Lower VIGV Acutating Rings ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-440 And 02-540)

      Location With The Spacer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-786 And 02-796)

      Upper And Lower VIGV Actuating Ring Spacer Hole Bore

      0.5512

      Intf

      0.5522

      0.0009

      Spacer Diameter

      0.5517

      Clear

      0.5521

      0.0005

      Table 14. Fits and Clearances (all dimensions in millimetres)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      Non-select

      REJECT IF

      MORE THAN

      LOCATION 1359

      Upper And Lower VIGV Actuating Rings ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-440 And 02-540)

      Location With The Spacer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-786 And 02-796)

      Upper And Lower VIGV Actuating Ring Spacer Hole Bore

      14.000

      Intf

      14.027

      0.023

      Spacer Diameter

      14.012

      Clear

      14.023

      0.015

    1. SUBTASK 72-41-30-220-140 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1360

    2. Refer to Figure.

    3. Reference dimensions at location 1360. If required use the data written as a note in TASK 72-41-34-200-000.

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

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      Non-select

      REJECT IF

      MORE THAN

      LOCATION 1360

      VIGV Rig Pin Bracket ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-780 And 02-790)

      Location With The Spacer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-786 And 02-796)

      VIGV Rig Pin Bracket Spacer Hole Bore

      0.3150

      Intf

      0.3158

      0.0007

      Spacer Diameter

      0.3154

      Clear

      0.3157

      0.0004

      Table 16. Fits and Clearances (all dimensions in millimetres)

      NEW PART

      WORN PART

      DIMENSIONS

      DIMENSIONS

      PART IDENT

      Size

      Clearance

      Non-select

      REJECT IF

      MORE THAN

      LOCATION 1360

      VIGV Rig Pin Bracket ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-780 And 02-790)

      Location With The Spacer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-786 And 02-796)

      VIGV Rig Pin Bracket Spacer Hole Bore

      8.000

      Intf

      8.022

      0.019

      Spacer Diameter

      8.010

      Clear

      8.019

      0.012

    1. SUBTASK 72-41-30-440-070 Assemble the VIGV Actuating Ringsand (Pre SBE 72-0385or SBE 72-0416 and SBE 72-0385or SBE 72-0416)

    2. Refer to Figure and Figure.

    3. SBE 72-0385 or SBE 72-0416: Introduction of revised actuating rings with increased dowel locations.

      1. Install the two centralizing actuating housings ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-680) in to the upper VIGV actuating ring ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-440).

      2. Put the two centralizing actuating housings in to position in the upper VIGV actuating ring.

      3. Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-682) and washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-684) to attach the two centralizing actuating housings to the upper VIGV actuating ring.

      4. Tighten the bolts.

      1. Install the two centralizing actuating housings in to the lower VIGV actuating ring ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-540).

      2. Do Stepto Step to install the two centralizing actuating housings in to the lower VIGV actuating ring.

      1. Pre SBE 72-0084: Install the rig pin location brackets ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-780) on to the upper VIGV actuating ring.

      2. Put the two spacers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-786) through the two boltholes at the two locations identified C.

      3. Locate the two rig pin location brackets on to the spacers.

      4. Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-784) and nuts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-782) to attach the brackets to the upper VIGV actuating ring. Make sure the bolt heads are correctly located against the brackets.

      5. Torque the four nuts to 36 lbfin to 45 lbfin (4.00 Nm to 5.00 Nm).

      1. Install the rig pin location bracket ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-790) on to the lower VIGV actuating ring.

      2. Put the two spacers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-796) through the two boltholes at the location identified E.

      3. Locate the rig pin location bracket on the spacers.

      4. Install the two bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-794) and nuts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-792) to attach the bracket to the lower VIGV actuating ring. Make sure the bolt heads are correctly located against the bracket.

      5. Torque the two nuts to 36 lbfin to 45 lbfin (4.00 Nm to 5.00 Nm).

    1. SUBTASK 72-41-30-220-143 Measure the VIGV Spindle Bushes Location Bores

    2. Refer to Figure, Figure and Figure.

      1. Set the tools to measure the bushes location bores.

      2. Connect the IAE 1R18277 Air plug gage 1 off to the IAE 1R18280 Air gage unit 1 off. Connect an air supply to the air gage unit.

      3. Open the air supply valve, part of the air gage unit. Make sure the needle on the air supply gage reads between the two red lines.

      4. Set the needles A and B to the two 20 positions on the air gage unit main gage. Use the needle adjusters to set the needles to the required value.

      5. Install IAE 1R18278 Setting ring 1 off on to the air plug gage. Refer to Figure. The two air jets, on the air plug gage, must be approximately in the center of the setting ring bore.

      6. Align the needle C, on the air gage unit gage, to the same value as the needles A or B. Use the flow adjuster to align the needle C.

      7. Remove the setting ring from the air plug gage.

      8. Install IAE 1R18279 Setting ring 1 off on to the air plug gage. The two air jets, on the air plug gage, must be approximately in the center of the setting ring bore.

      9. Align the needle C, on the air gage unit gage, to the same value as the needles A or B. Use the flow adjuster to align the needle C.

      10. Remove the setting ring from the air plug gage.

      1. Measure the VIGV bush location bores.

      2. Install the air gage plug in to the VIGV outer bush location bore at the No. 1 position. Set the two air jets at approximately the center of the bush location bore.

      3. Write a record of the value shown on the air gage unit gage.

      4. Push the air plug gage in to the inner bush location bore. Set the two air jets at approximately the center of the inner bush location bore.

      5. Write a record of the value shown on the air gage unit gage.

        NOTE

        Each location bore must be measured at the same angle to the case center line.
      6. Do Step to Step at the remaining VIGV bush location bores.

    1. SUBTASK 72-41-30-440-121-001 Install the VIGV Spindle Bushes using IAE 1R18260 and IAE 1R18295 Bush Assembly Tools (Pre SBE 70-0052 and SBE 70-0052)

    2. Refer to Figure.

    3. SBE 70-0052: Engine - Additional source for variable stator vane spindle bushings

      1. Install the VIGV inner bushes.

      2. Pre SBE 70-0052: From the values written down in Step use the correct size bush.

        Red segment - Fig/item 72-41-31, 01-243.

        Yellow segment - Fig/item 72-41-31, 01-241.

        Black segment - Fig/item 72-41-31, 01-242.

      3. SBE 70-0052: From the values written down in Step use the correct size bush.

        Red segment - Fig/item 72-41-31, 01-243 or 72-41-31, 01-245.

        Yellow segment - Fig/item 72-41-31, 01-241 or 72-41-31, 01-246.

        Black segment - Fig/item 72-41-31, 01-242 or 72-41-31, 01-247.

      4. Use IAE 1R18295 Bushing assembly tool 1 off to install the bushes. Refer to detail A on Figure.

      5. Remove the ring, handle, spacer and nylon washer B from the tool pin.

      6. Install the pin with the nylon washer A in to the VIGV bush location at the No. 1 position. Make sure the nylon washer is correctly located on the HP Compressor Front Case outer surface.

      7. Locate the bush that is to be installed on the pin on the inside of the HP Compressor Front Case.

      8. Install the nylon washer B, spacer, ring and handle on to the pin. Turn the handle until the nylon washer B abuts the bush that is to be installed.

      9. Make sure the bush assembly tool is correctly located and is at 90 degrees to the location bore.

      10. Hold the dowel, then continue to turn the handle to install the bush. Do not let the dowel turn.

      11. When the bush is installed remove the bush assembly tool.

      12. Do Step to Step to install the remaining 39 inner bushes.

      1. Install the VIGV outer bushes.

      2. Pre SBE 70-0052: Select the correct size of bush. Refer to Step.

      3. SBE 70-0052: Select the correct size of bush. Refer to Step.

      4. Use IAE 1R18260 Bushing assembly tool 1 off to install the bushes. Refer to detail B on Figure.

      5. Remove the ring, handle, spacer and nylon washer B from the tool pin.

      6. Locate the bush that is to be installed on to the nylon washer A.

      7. Install the pin, nylon washer A and the bush in to the VIGV location at the No. 1 position. Make sure the bush is correctly located.

      8. Install the nylon washer B, spacer, handle and ring removed in Step.

      9. Turn the handle until the nylon washer B touches the inner bush.

      10. Make sure the bush assembly tool is correctly located and is at 90 degrees to the location bore.

      11. Hold the dowel, then continue to turn the handle to install the bush. Do not let the dowel turn.

      12. When the bush is installed remove the bush assembly tool.

      13. Do Step to Step to install the remaining 39 outer bushes.

    1. SUBTASK 72-41-30-440-121-002 Install the VIGV Spindle Bushes using IAE 1R18579, IAE 1R18576, IAE 1R18577, IAE 1R18573 and IAE 1R18582 Bush Assembly Tools (Pre SBE 70-0052 and SBE 70-0052)

    2. Refer to Figure.

    3. SBE 70-0052: Engine - Additional source for variable stator vane spindle bushings

      1. Install the VIGV inner bushes.

      2. Pre SBE 70-0052: From the values written down in Step use the correct size of bush.

        Red segment - Fig/item 72-41-31, 01-243.

        Yellow segment - Fig/item 72-41-31, 01-241.

        Black segment - Fig/item 72-41-31, 01-242.

      3. SBE 70-0052: From the values written down in Step use the correct size of bush.

        Red segment - Fig/item 72-41-31, 01-243 or 72-41-31, 01-245.

        Yellow segment - Fig/item 72-41-31, 01-241 or 72-41-31, 01-246.

        Black segment - Fig/item 72-41-31, 01-242 or 72-41-31, 01-247.

        1. Use the correct installation tool.

        2. For the VIGV long vane bushes ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500) use IAE 1R18579 Pusher installation tool 1 off. Refer to detail A on Figure.

        3. For the VIGV short vane bushes ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-600) use IAE 1R18576 Pusher installation tool 1 off. Refer to detail B on Figure.

      4. Install the pusher in the VIGV bush location at the No. 1 position. Make sure the pusher is correctly located on the HP Compressor Front Case outer surface.

      5. Put the bush on the pusher on the inside of the HP Compressor Front Case.

      6. Install the IAE 1R18577 Bushing installation tool 1 off, on the pusher.

      7. Install the IAE 1R18573 Cylinder, hydraulic 1 off, on the pusher until the cylinder comes against the bush installation.

      8. CAUTION

        YOU MUST MAKE SURE THE ASSEMBLY TOOL IS CORRECTLY LOCATED AT 90 DEGREES TO THE LOCATION BORE TO PREVENT DAMAGE TO THE HP Compressor Front Case.

        Apply hydraulic pressure to the cylinder until the bush is pushed into the compressor case.

      9. Release the hydraulic pressure and remove the assembly tool.

      10. Do Step to Step again to install the remaining 39 inner bushes.

      1. Install the VIGV outer bushes.

      2. Pre SBE 70-0052: Select the correct size of bush. Refer to Step.

      3. SBE 70-0052: Select the correct size of bush. Refer to Step.

      4. Use the IAE 1R18582 Pusher installation tool 1 off to install the bushes for the VIGV long and short vanes. Refer to detail B on Figure.

      5. Put the bush on the pusher and install the pusher in the VIGV bush location at the No. 1 position. Make sure the bush is correctly located.

      6. Install the IAE 1R18577 Bushing installation tool on the pusher.

      7. Install the IAE 1R18573 Cylinder, hydraulic on the pusher until the cylinder comes against the bush installation.

      8. CAUTION

        YOU MUST MAKE SURE THE ASSEMBLY TOOL IS CORRECTLY LOCATED AT 90 DEGREES TO THE LOCATION BORE TO PREVENT DAMAGE TO THE COMPRESSOR CASE.

        Apply hydraulic pressure to the cylinder until the bush is pushed into the HP Compressor Case.

      9. Release the hydraulic pressure and remove the assembly tool.

      10. Do Step to Step again to install the remaining 39 outer bushes.

    1. SUBTASK 72-41-30-440-071 Install the VIGV in the HP Compressor Front Case (Pre SBE 72-0402 and SBE 72-0402)

    2. Refer to Figure and Fig. 72-41-90-990-027.

    3. Pre SBE 72-0402: It is not necessary to lubricate the VIGV locations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) during this SUBTASK.

    4. SBE 72-0402: Lubricate the VIGV locations during these assembly operations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) as specified in TASK 72-41-30-440-011-A00, SUBTASK 72-41-30-440-208.

    5. Install the 40 sealing washers ENGINE-HP COMPRESSOR FRONT CASES AND VANES (72-41-30, 01-100) on the inner bushes. Make sure the sealing washers are correctly located around the inner bush.

      1. Install the guide vanes in the upper half HP Compressor Front Case.

        1. Temporary mark vane sequence number on each vane before it is installed.

          NOTE

          Do not vibropeen.
        2. Refer to SPM TASK 70-09-01-400-501.

      2. NOTE

        Install the two guide vanes ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-600) at the positions 10 and 11.

        Install the 18 guide vanes ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500) and the two guide vanes ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-600) in to the bushes.

      1. Install the guide vanes in the lower half HP Compressor Front Case.

        NOTE

        There are no short spindled guide vanes installed in the lower half HP Compressor Front Case.
      2. Install the 20 guide vanes ENGINE-HP COMPRESSOR VARIABLE VANES (72-41-32, 01-500) as given in Step and Step.

      1. Measure and write down the guide vane end float.

      2. Put two spacers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-060) on the spindle of each guide vane.

        1. Install the 40 guide vane actuating levers on the spindles of the guide vanes and in to their locations in the actuating ring.

        2. The two actuating levers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-140) go at the positions 10 and 11.

        3. The eight actuating levers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-120) go at the positions 1, 2, 19, 20, 21, 22, 39 and 40.

        4. The 30 actuating levers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-100) go at the positions 3 to 9, 12 to 18 and 23 to 38.

      3. Install the 40 slave nuts to attach the actuating levers to the guide vanes. Torque the nuts to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm). The nuts that are used must have no run down torque.

        NOTE

        The guide vane actuating levers must be parallel with the casing center line when you torque the nuts. This is the null position.
      4. At each guide vane apply a load at the inner pivot point, to push the guide vane radially out.

      5. Measure and write a record of the end float, dimension A Figure. Measure between the actuating lever and the specified spacers.

        NOTE

        Temporarily mark the actuating levers with their position numbers. These must be the same as the numbers on the guide vanes location.
      6. Remove the 40 slave nuts and actuating levers from the guide vanes.

      7. Install the 40 slave nuts on to the guide vane spindles. Tighten the slave nuts sufficiently to keep the spacers on the guide vane spindles.

    1. SUBTASK 72-41-30-440-072 Install the VIGV Upper and Lower Actuating Rings (Pre SBE 72-0402, SBE 72-0402, Pre SBE 72-0385 or SBE 72-0416 and SBE 72-0385 or SBE 72-0416)

    2. Refer to Figure and Figure.

    3. Pre SBE 72-0402: It is not necessary to lubricate the VIGV locations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) during this SUBTASK.

    4. SBE 72-0402: Lubricate the VIGV locations during these assembly operations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) as specified in TASK 72-41-30-440-011-A00, SUBTASK 72-41-30-440-208.

      1. Pre SBE 72-0385 or SBE 72-0416: Install the upper guide vane actuating ring ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-440) on to the upper half HP Compressor Front Case.

        SBE 72-0385 or SBE 72-0416: Install the upper guide vane actuating ring ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-440) on to the upper half HP Compressor Front Case.

      2. Put the upper guide vane actuating ring in to position on the upper half HP Compressor Front Case.

        NOTE

        Set the upper guide vane actuating ring adjacent to the guide vanes at the positions 3 to 18.
      3. Install two of IAE 1R18423 Rigging pin 4 off or IAE 1R18892 Rigging pin 4 off and one of IAE 1R18248 Rigging pin 2 off or IAE 1R18638 Rigging pin 2 off to attach the actuating ring to the HP Compressor Front Case at the positions X.

      4. Remove the 16 slave nuts from the guide vanes at the positions 3 to 18.

      5. Remove the two spacers from the spindle of each guide vane.

      6. Install two spacers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-060) to ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-078) on to the spindle of each guide vane at the positions 3 to 18. The thickness of the spacers that are installed are equal to:

        the removed spacer thickness + the end float - 0.003 in. to 0.005 in. (0.08 mm to 0.13 mm).

        Write a record of the thickness of the spacers that are installed.

      7. Install the actuating levers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-100) and ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-140). Make sure the correct actuating lever goes on the correct guide vane at the positions 3 to 18.

      8. Install the 16 nuts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-103) and ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-143) on to the guide vanes at the positions 3 to 18.

      9. Remove the three rigging pins and set the guide vane levers at the null position.

      10. Torque the nuts to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm) plus the run down torque.

      11. Measure the guide vane end float at the positions 3 to 18. Make sure it is 0.003 in to 0.005 in. (0.08 mm to 0.13 mm).

      1. Install the lower guide vane actuating ring ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-540) on to the lower half HP Compressor Front Case.

        NOTE

        There are no short spindled guide vanes in the lower half HP Compressor Front Case.
      2. Install the lower guide vane actuating ring on to the lower half HP Compressor Front Case at the guide vane positions 23 to 38. Use the procedure given in Step to Step.

      3. To attach the actuating ring to the lower half HP Compressor Front Case use the other two IAE 1R18423 Rigging pin 4 off or IAE 1R18892 Rigging pin 4 off and one IAE 1R18248 Rigging pin 2 off or IAE 1R18638 Rigging pin 2 off. Refer to Figure for the positions of the pins.

    1. SUBTASK 72-41-30-440-073 Install the VIGV Shroud (Pre SBE 72-0402, SBE 72-0402, Pre SBE 72-0422 and SBE 72-0422)

    2. Refer to Figure.

    3. SBE 72-0402: HP compressor variable vanes - inlet guide vane and stages 3 to 6 with optimised build and setting instructions.

      SBE 72-0422: HP compressor variable inner shrouds - Introduction of revised one piece bushes

    4. Pre SBE 72-0402 : It is not necessary to lubricate the VIGV locations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) during this SUBTASK.

    5. SBE 72-0402 : Lubricate the VIGV locations during these assembly operations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) as specified in TASK 72-41-30-440-011-A00, SUBTASK 72-41-30-440-208.

      1. Pre SBE 72-0422: Install the guide vane half shroud and the IAE 1R18250 Split ring assembly 1 off in to the upper half HP Compressor Front Case.

        SBE 72-0422: Install the guide vane half shroud and the IAE 1R19633 Split ring assembly 1 off in to the upper half HP Compressor Front Case.

      2. Pre SBE 72-0422: Apply a thin layer of CoMat 04-007 SILICONE GREASE to the 20 half bushes ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190) outer surface.

      3. SBE 72-0422: Apply a thin layer of CoMat 04-007 SILICONE GREASE to the 20 bushes ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190) outer surface.

        NOTE

        The rear upper half of the guide vane half shroud has four location dowels.
      4. Pre SBE 72-0422: Install the 20 half bushes in to the rear upper half of the guide vane half shroud ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-200).

        NOTE

        The rear upper half of the guide vane half shroud has four location dowels.
      5. SBE 72-0422: Install the 20 bushes onto the stator vanes.

      6. Pre SBE 72-0422: Install the guide vanes half shroud and half bushes on to the rear of the guide vanes at the inner pivot point.

      7. SBE 72-0422: Install the guide vanes half shroud on to the rear of the guide vanes at the inner pivot point.

      8. Pre SBE 72-0422: Install one half of IAE 1R18250 Split ring assembly on to the front of the guide vanes at the inner pivot point.

      9. SBE 72-0422: Install one half of IAE 1R19633 Split ring assembly on to the front of the guide vanes at the inner pivot point.

      10. Install the three bolts and nuts, part of the Split Ring Assembly, to attach the Split Ring Assembly to the guide vane half shroud.

      11. Tighten the nuts.

      1. Install the guide vane half shroud and the Split Ring Assembly in the lower half HP Compressor Front Case.

      2. Install the rear lower half of the guide vane half shroud and Split Ring Assembly as given in steps Step to Step.

        NOTE

        The rear lower half of the guide vane half shroud has three location dowels.
  1. Figure: Pre SBE 72-0027: View through the HP Compressor Front Cases

    Sheet 1

    Legend
    Pre SBE 72-0027: View through the HP Compressor Front Cases

    Sheet 1

    Close

    Figure: SBE 72-0027: View through the HP Compressor Front Cases

    Sheet 2

    Legend
    SBE 72-0027: View through the HP Compressor Front Cases

    Sheet 2

    Close

    Figure: Locations for the fits and clearances

    Locations for the fits and clearances

    Figure: Pre SBE 72-0084: Install the centralizing actuating housings

    Sheet 1

    Legend
    Pre SBE 72-0084: Install the centralizing actuating housings

    Sheet 1

    Close

    Figure: SBE 72-0084: Install the centralizing actuating housings

    Sheet 2

    Legend
    SBE 72-0084: Install the centralizing actuating housings

    Sheet 2

    Close

    Figure: Details of the air gage unit

    Sheet 1

    Legend
    Details of the air gage unit

    Sheet 1

    Close

    Figure: Details of the air gage unit

    Sheet 2

    Legend
    Details of the air gage unit

    Sheet 2

    Close

    Figure: Tools to measure the VIGV location bores

    Tools to measure the VIGV location bores

    Figure: Tools to install the spindle location bushes

    Sheet 1

    Legend
    Tools to install the spindle location bushes

    Sheet 1

    Close

    Figure: Tools to install the spindle location bushes

    Sheet 2

    Legend
    Tools to install the spindle location bushes

    Sheet 2

    Close

    Figure: Position for the variable inlet guide vanes

    Position for the variable inlet guide vanes

    Figure: Pre SBE 70-0052 and SBE 70-0052: Install the variable inlet guide vanes

    Pre SBE 70-0052 and SBE 70-0052: Install the variable inlet guide vanes

    Figure: Measure the guide vane end float

    Measure the guide vane end float

    Figure: The positions for the rigging pins

    The positions for the rigging pins

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised the temporary mark procedure. (18VG365)

Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:X333X
Enterprise Name:REFER TO V2500 SB ENG-79-0108
Link not Found
Manufacturer Code:0AM53
Supply Number:CoMat 02-363
Type:sp01
Supply Short Name:CoMat 02-363 MARKING PEN
Supply Name:CoMat 02-363 MARKING PEN
Specification Groups:
Doc NumberType
PMC 455613401 BLACK (FINE TIP) OR 13501 BLACK (BROAD TIP)
Suppliers:
ManufacturerRemarks
0AM53
Manufacturer Code:LOCAL
Supply Number:CoMat 04-007
Type:sp01
Supply Short Name:CoMat 04-007 SILICONE GREASE
Supply Name:CoMat 04-007 SILICONE GREASE
Specification Groups:
Doc NumberType
SGM494 (CSS 228, DEF STAN 68-69)OMAT: 418 (RR REF)
Suppliers:
ManufacturerRemarks
LOCAL
K7652
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: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:39428
Supply Number:CoMat 10-108
Type:sp01
Supply Short Name:CoMat 10-108 HIGH PERFORMANC EPENETRATING LUBRICANT WITH TEFLON (R)
Supply Name:CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R)
Specification Groups:
Doc NumberType
OMAT: 1080 (RR Ref)TRI-FLOW
Suppliers:
ManufacturerRemarks
39428
K6835
KC4N1
Manufacturer Code:0AM53
Tool Number:IAE 1R18248
Tool Name:IAE 1R18248 Rigging pin
Manufacturer Code:0AM53
Tool Number:IAE 1R18250
Tool Name:IAE 1R18250 Split ring assembly
Manufacturer Code:0AM53
Tool Number:IAE 1R18260
Tool Name:IAE 1R18260 Bushing assembly tool
Manufacturer Code:0AM53
Tool Number:IAE 1R18277
Tool Name:IAE 1R18277 Air plug gage
Manufacturer Code:0AM53
Tool Number:IAE 1R18278
Tool Name:IAE 1R18278 Setting ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18279
Tool Name:IAE 1R18279 Setting ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18280
Tool Name:IAE 1R18280 Air gage unit
Manufacturer Code:0AM53
Tool Number:IAE 1R18295
Tool Name:IAE 1R18295 Bushing assembly tool
Manufacturer Code:0AM53
Tool Number:IAE 1R18423
Tool Name:IAE 1R18423 Rigging pin
Manufacturer Code:0AM53
Tool Number:IAE 1R18573
Tool Name:IAE 1R18573 Cylinder, hydraulic
Manufacturer Code:0AM53
Tool Number:IAE 1R18576
Tool Name:IAE 1R18576 Pusher installation tool
Manufacturer Code:0AM53
Tool Number:IAE 1R18577
Tool Name:IAE 1R18577 Bushing installation tool
Manufacturer Code:0AM53
Tool Number:IAE 1R18579
Tool Name:IAE 1R18579 Pusher installation tool
Manufacturer Code:0AM53
Tool Number:IAE 1R18582
Tool Name:IAE 1R18582 Pusher installation tool
Manufacturer Code:0AM53
Tool Number:IAE 1R18638
Tool Name:IAE 1R18638 Rigging pin
Manufacturer Code:0AM53
Tool Number:IAE 1R18892
Tool Name:IAE 1R18892 Rigging pin
Manufacturer Code:0AM53
Tool Number:IAE 1R19633
Tool Name:IAE 1R19633 Split ring assembly