TASK 72-41-00-440-004-A00 HPC Assembly - Install The HPC Front Cases (Post HPC Surgical Strike Procedure), Special Procedure-004

DMC:V2500-A1-72-41-0000-04A-710A-B|Issue No:004.00|Issue Date:2019-11-01

Export Control

EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.

Copyright

© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).

Applicability

V2500-A1

Common Information

TASK 72-41-00-440-004-A00 HPC Assembly - Install The HPC Front Cases (Post HPC Surgical Strike Procedure), Special Procedure-004

General

This TASK gives the procedure to install the HP compressor front cases on to the HP compressor rotor assembly after the HP Surgical Strike workscope.

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 numbers.

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 this procedure.

Special limits for the No. 4 bearing compartment are given in this procedure. These limits will apply only to those engines designated for the HPC Surgical Strike Procedure if all Engine Functional Test requirements are maintained as given in Section 71-00-00, including a No. 4 Compartment Scavenge Pressure limit of 145 psig. Test data indicates that engines with a No. 4 compartment vacuum pressure of 17 pph and less will not fail pass off test requirements for P4Scav of 145 psig. Findings that are not in the limits given in this procedure will be cause for engine rejection.

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.

SBE 72-0402

During the assembly procedure lubricate the applicable areas of the VSV mechanism for each stage with a thin layer of 10-108 teflon based lubricant. The following SUBTASK reference is in TASK 72-41-30-440-011-A00 (72-41-30, ASSEMBLY-11, CONFIG-01) refer to SUBTASK 72-41-30-440-208.

To identify, lubricate and install seal rings, refer to SPM TASK 70-44-01-400-501.

For lockwire data and procedures refer to SPM TASK 70-42-05-400-501.

SBE 70-0813

For safety cable data and procedures refer to SPM TASK 70-42-08-400-501.

After assembly apply CoMat 07-038 AIR DRYING ENAMEL to any damaged surface protection, joint flange and attach parts. Use the correct color of the . Refer to 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.

For practices and processes referred to in the procedure by the TASK number are in the SPM.

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
Dial Test IndicatorsLOCALDial Test Indicators6
Dial test indicator stands/blocks and associated equipmentLOCALDial test indicator stands/blocks and associated equipment
FlashlightLOCALFlashlight
DELETED0AM53DELETED
IAE 1F10052 Two cables sling0AM53IAE 1F100522
IAE 1P16002 Cradle pedestal0AM53IAE 1P160021
IAE 1P16046 Removal/Installation fixture0AM53IAE 1P160461
IAE 1P16088 Leak check adapter0AM53IAE 1P160881
IAE 1P16089 Leak check cap0AM53IAE 1P160891
IAE 1P16285 Tie-rod adapter0AM53IAE 1P162851
IAE 1P16543 Removal/Installation fixture0AM53IAE 1P165431
IAE 1R18234 Support rod0AM53IAE 1R182343
IAE 1R18247 Rigging pin0AM53IAE 1R182471
IAE 1R18250 Split ring assembly0AM53IAE 1R182501
IAE 1R18325 Trunnion assembly0AM53IAE 1R183252
IAE 1R18673 Dummy stub shaft0AM53IAE 1R186731
IAE 1R19463 Stand - Surgical strike0AM53IAE 1R194631
IAE 1R19633 Split ring assembly0AM53IAE 1R196331
IAE 6F10030 Vacuum test cart0AM53IAE 6F100301
IAE 1F10028 Support Pedestal0AM53IAE 1F10028
IAE 1F10052 Two cables sling0AM53IAE 1F10052
IAE 1P16002 Cradle pedestal0AM53IAE 1P16002
IAE 1P16046 Removal/Installation fixture0AM53IAE 1P16046
IAE 1P16088 Leak check adapter0AM53IAE 1P16088
IAE 1P16089 Leak check cap0AM53IAE 1P16089
IAE 1P16543 Removal/Installation fixture0AM53IAE 1P16543
IAE 1R18234 Support rod0AM53IAE 1R18234
IAE 1R18247 Rigging pin0AM53IAE 1R18247
IAE 1R18250 Split ring assembly0AM53IAE 1R18250
IAE 1R18325 Trunnion assembly0AM53IAE 1R18325
IAE 1R19633 Split ring assembly0AM53IAE 1R19633
IAE 1R19463 Stand - Surgical strike0AM53IAE 1R19463
IAE 6F10030 Vacuum test cart0AM53IAE 6F10030

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 02-123 LAY-OUT FLUIDK6835CoMat 02-123
CoMat 02-126 LOCKWIREK6835CoMat 02-126
CoMat 02-274 SAFETY CABLE KITLOCALCoMat 02-274
CoMat 02-275 SAFETY CABLE KITLOCALCoMat 02-275
CoMat 04-007 SILICONE GREASELOCALCoMat 04-007
CoMat 07-038 AIR DRYING ENAMEL00BB6CoMat 07-038
CoMat 08-013 COLD CURING SILICONE COMPOUNDX222XCoMat 08-013
CoMat 10-077 APPROVED ENGINE OILSX333XCoMat 10-077
CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R)39428CoMat 10-108

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-41-00-440-199 Install the HP Front Split Cases

    1. Refer to Figure.

    2. NOTE

      The retaining clamp plate assembly will need to be released and moved clear of the jacking screws if the axial settings need to be adjusted.

      Loosen the locknut on the heel pin (detail 15). Release the hand knob (detail 22) and move the retaining clamp plate assembly clear of the three jacking screws (detail 12).

    3. If necessary loosen the locknut on the tie-rod adapter (installed through the center of the HP module), refer to Figure by approximately 0.40in. (10 mm) to allow axial movement of the static and rotating parts.

      4. Position the six dial test indicators or equivalent instrumentation measuring devices as follows.

      1. NOTE

        This instrumentation will monitor the relative movement of the HP static components and the stand.

        Put three dial test indicators, equally spaced, on the surface of the stand top plate (detail 3) so each dial indicator button contacts each of the three support plates (detail 4).

      2. Put three dial test indicators, spaced equally, on the IAE 1P16046 Removal/Installation fixture or IAE 1P16543 Removal/Installation fixture 1 off tooling structure so each dial indicator button contacts the rear surface of the stage 2 retaining plate slot on the stage 2 turbine hub ENGINE-STAGE 2 TURBINE HUB (72-45-31, 01-011).

        NOTE

        This instrumentation will monitor the true relative movement of the HP rotating components and the static components. This is the critical dimension to be monitored.

      5. Confirm the true axial displacement of the HP module cases and stage 2 HP turbine and the IAE 1R19463 Stand - Surgical strike Surgical Strike Stand 1 off.

      1. Refer to the record of the readings taken at the six positions with the front half casings removed, refer to TASK 72-41-00-040-001-C00.

      2. Take the readings on the three dial test indicators in contact with each of the three support plates (detail 4). These readings should be the same as the final readings taken during TASK 72-41-00-040-001-C00.

      3. NOTE

        This is to make sure that the relative reverse movement during installation is the same as that recorded during the removal of the cases.

        Take the readings on the three dial test indicators in contact with the rear surface of the stage 2 retaining plate slot on the stage 2 turbine hub ENGINE-STAGE 2 TURBINE HUB (72-45-31, 01-011). These readings should be the same as the final readings taken during TASK 72-41-00-040-001-C00. These readings should be within 0.020 in. (0.5 mm) of the readings taken at the three support plates.

      6. Install the HP compressor front split half casings as given in Step or Step at the same time as the procedure in this SUBTASK.

      1. CAUTION

        THESE READINGS ARE THE MAXIMUM PERMITTED TOTAL MOVEMENT TO RETURN TO THE DATUM POSITION. YOU MUST NOT EXCEED THESE READINGS OR DAMAGE TO ENGINE COMPONENTS WILL OCCUR.

        Make sure the dial test indicator readings agree with the final readings taken in TASK 72-41-00-040-001-C00.

      2. CAUTION

        DURING THE REMOVAL AND INSTALLATION OF THE HP COMPRESSOR FRONT HALF CASES TAKE CARE NOT TO DAMAGE THE HP COMPRESSOR ROTOR BLADES. DO NOT USE EXCESSIVE OR MORE FORCE THAN IS NECESSARY.

        Support the split casings on detail 10 half rings. Move the cases carefully into position on detail 10 and then install and fully locate the split casings around the HP compressor assembly . Make sure that the casings do not touch and damage the HP compressor rotor blades.

      3. CAUTION

        THERE MUST NOT BE A DIFFERENCE OF MORE THAN 0.020 IN. (0.5 MM) BETWEEN THE READINGS OF EACH OF THE DIAL TEST INDICATORS. IF THE DIFFERENCE IS MORE THAN THIS LIMIT THEN DAMAGE MAY OCCUR TO HP MODULE COMPONENTS.

        CAUTION

        YOU MUST MAKE A RECORD OF THE DIAL TEST INDICATOR READINGS AFTER EACH INCREMENTAL MOVEMENT MADE.

        Refer to the readings taken in TASK 72-41-00-040-001-C00. During installation use the readings in a series of incremental steps to reverse and match those taken during the Disassembly procedure.

      4. Adjust the three jacking screws (detail 12) to make adjustments to the axial movement of the static components relative to the rotating components. Turn the jacking screws in an anti-clockwise direction to move the HP compressor rear cases forward (the rear cases move in a direction towards the base of the build stand). Make each adjustment so each of the dial test indicator readings are no more than 0.020 in. (0.5 mm) for each increment adjustment.

      5. Make sure that readings do not differ by more than 0.020 in. (0.5 mm) between dial test indicators. This is to make sure that the axial movement is adjusted evenly and equally and is the same as that recorded during Disassembly.

      6. The readings at stage 2 HP turbine position is the critical dimension to be monitored and represents the true axial movement between the static and rotating assemblies. The final reading must agree with that taken during Disassembly to make sure that the original axial displacement is correctly restored.

      7. Remove the instrumentation.

      8. Move the retaining clamp plate assembly into position to make contact with the the three jacking screws (detail 12). Adjust and tighten the locknut on the heel pin (detail 15) but do not fully torque the lock nut. Tighten the hand knob (detail 22) to hold the assembly firmly.

      9. Tighten the locknut on the tie-rod adapter (installed through the center of the HP module) to prevent the axial movement of the static and rotating parts.

    2. SUBTASK 72-41-00-440-200-A00 Install the HP Compressor Front Cases (Pre SBE 72-0027)

    1. Refer to Figure and Figure. SBE 72-0027

    2. Do this assembly procedure in conjunction with Step.

      3. Install the stage 3, 4, 5 and 6 sealing strips.

      1. Install the two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-677) at the stage 3 rotor path ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-685). Install the sealing strips at the opposite split line flanges.

      2. Install the two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-678) at the stage 4 rotor path ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-690). Install the sealing strips at the opposite split line flanges.

      3. Install the two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-679) at the stage 5 rotor path ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-695). Install the sealing strips at the opposite split line flanges.

      4. Install the two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-680) at the stage 6 rotor path ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700). Install the sealing strips at the opposite split line flanges.

      4. Install the upper and lower half HP compressor front case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400).

      1. Carefully put the upper and lower half HP compressor front cases on to the build stand.

      2. Align the pin holes in the HP compressor front cases rear flange with the correct holes in the compressor rear outer case.

      3. The pin holes at TDC and BDC are off set.

      4. Make sure the two large and two small locating pins in the support ring are engaged in the correct holes in the HP compressor front cases.

      5. Align the split line flanges. Make sure the stage 3, 4, 5 and 6 sealing strips are correctly engaged in the opposite rotor path ring segment.

      5. CAUTION

        THE BOLTS ARE A CLOSE TOLERANCE FIT. THEY MUST NOT BE TURNED WHEN BEING INSTALLED.

        Install the HP compressor front case split line flange bolts, spacers and nuts.

      1. NOTE

        Do not install a bolt, nut and spacer at the bolt positions 13 and 31.

        Install the 30 bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-108) the 30 spacers ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-104) and the 30 nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-102) at the split line flanges.

        2. At the bolts positions 13 and 31 install the upper and lower support brackets ENGINE-SECURING FEATURES-HP COMPRESSOR CASESand ENGINE-SECURING FEATURES-HP COMPRESSOR CASES 04-650).

        1. Install the bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-112) through the upper and lower support brackets and the split line flange.

        2. Install the nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-101) on to the bolt.

      3. Torque the nuts to 180 to 220 lbfin (20.00 to 25.00 Nm).

      4. Make sure the dowel pin holes are aligned and the HP compressor rear outer case touches the HP compressor front case.

    3. SUBTASK 72-41-00-440-200-B00 Install the HP Compressor Front Cases (SBE 72-0027)

    1. Refer to Figure and Figure. SBE 72-0027.

      2. Install the stage 5 and 6 sealing strips.

      1. Install the two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-679) at the stage 5 rotor path ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-695). Install the sealing strips at the opposite split line flanges.

      2. Install the two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-680) at the stage 6 rotor path ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700). Install the sealing strips at the opposite split line flanges.

      3. Install the upper and lower half half HP compressor front case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400).

      1. Carefully put the upper and lower half HP compressor front cases on to the build stand.

      2. Align the pin holes in the HP compressor front cases rear flange with the correct holes in the compressor rear outer case.

      3. The pin holes at TDC and BDC are off set.

      4. Make sure the two large and two small locating pins in the support ring are engaged in the correct holes in the HP compressor front cases.

      5. Align the split line flanges. Make sure the stage 5 and 6 sealing strips are correctly engaged in the opposite rotor path ring segment.

      4. CAUTION

        THE BOLTS ARE A CLOSE TOLERANCE FIT. THEY MUST NOT BE TURNED WHEN BEING INSTALLED.

        Install the HP compressor front case split line flange bolts, spacers and nuts.

      1. NOTE

        Do not install a bolt, nut and spacer at the bolt positions 12 and 32.

        Install the 30 bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-108) the 30 spacers ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-104) and the 30 nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-102) at the split line flanges.

        2. At the bolts positions 12 and 32 install the upper and lower support brackets ENGINE-SECURING FEATURES-HP COMPRESSOR CASES and ENGINE-SECURING FEATURES-HP COMPRESSOR CASES(72-41-00, 04-600 and 04-650).

        1. Install the bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-112) through the upper and lower support brackets and the split line flange.

        2. Install the nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-101) on to the bolt.

      3. Torque the nuts to 180 to 220 lbf.in (20.00 to 25.00 Nm).

      4. Make sure the dowel pin holes are aligned and the HP compressor rear outer case touches the HP compressor front case.

    4. SUBTASK 72-41-00-440-201 Install the HP Compressor Front Case Rear Flange Attach Parts (Pre SBE 72-0080, Pre SBE 72-0119, Pre SBE 72-0132, Pre SBE 72-0223, SBE 72-0080, SBE 72-0119, SBE 72-0132, SBE 72-0176, SBE 72-0223)

    1. Refer to Figure, Figure and Figure. SBE 72-0080SBE 72-0119SBE 72-0132SBE 72-0176SBE 72-0223

    2. Install the 10 pins ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-322) and the 10 lock plates ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-320) together with 10 bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the 10 nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302). Lightly tighten the nuts at the positions A.

      3. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-780).

      1. Put the bracket into position on the HP compressor front case rear flange at the bolt positions 3 and 4.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      4. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-240).

      1. Put the bracket into position on the compressor rear outer case front flange at the bolt positions 5 and 6.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      5. SBE 72-0132: Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-260).

      1. Put the bracket into postion on the compressor rear outer case front flange at the bolt position 7 and 8.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      6. Install the rear upper bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-280).

      1. Put the bracket into position on the HP compressor front case rear flange at the bolt positions 10 and 11.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      7. NOTE

        Do this part of the procedure if applicable during Surgical Strike procedures.

        SBE 72-0176: Install the HP system module serial number identification plate and bracket.

      1. Apply CoMat 08-013 COLD CURING SILICONE COMPOUND to the identification plate ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00,03-010) and bond the plate to the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00,03-020). Refer to SPM TASK 70-36-02-360-501, SUBTASK 70-36-02-360-020.

      2. Attach the plate to the bracket with the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-014) the two washers ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-013) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-012). Torque tighten the bolts 36 to 45 lbfin (4 to 5 Nm.).

      3. NOTE

        The bolt and nut at position 11 was installed during installation of bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00,03-280).

        Put the plate/bracket assembly into position on the compressor rear outer case front flange at bolt positions 11 and 12.

      4. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the assembly the flange rear face.

      8. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-320).

      1. Pre SBE 72-0080: Put the bracket into position on the compressor rear outer case front flange at the bolt positions 16 and 17.

      2. SBE 72-0080: Put the bracket into position on the HP compressor front case rear flange at the bolt positions 16 and 17.

      3. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      4. Lightly tighten the two nuts.

      9. Install the front upper bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-310).

      1. Put the bracket into position on the HP compressor front case rear flange at the bolt positions 18 and 19.

      2. Install the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the nut ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the bolt position 18.

      3. Lightly tighten the nut.

      10. Pre SBE 72-0119: Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-400).

      1. Install the bracket into position on the compressor rear outer case flange at the bolt positions 19 to 21.

      2. Install the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the nut ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the position 19. Install the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) at the bolt position 20.

      3. Lightly tighten the nut.

      4. Lightly tighten the bolt at bolt position 20.

      11. SBE 72-0119: Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-400).

      1. Install the bracket into position on the compressor rear outer case flange at the bolt positions 20 and 21.

      2. Install the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the nut ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the position 20.

      3. Lightly tighten the nut.

      12. Install the actuator rear bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-380).

      1. Put the bracket into position on the HP compressor front case at the bolt positions 21 and 22.

      2. Install the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-314) and the nut ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the position 21.

      3. Lightly tighten the nut.

      13. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-350).

      1. Put the bracket into position on the compressor rear outer case front flange at the bolt positions 22 and 23.

      2. Install the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-314) and the nut ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the bolt position 22. Install the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the nut ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the bolt position 23.

      3. Lightly tighten the two nuts.

      14. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-360).

      1. Put the bracket into position on the compressor rear outer case front flange at the bolt positions 25 and 26.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      15. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-510).

      1. Put the bracket into position on the compressor rear outer case front flange at the bolt position 30 and 31.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      16. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-530).

      1. Put the bracket into position on the HP compressor front case rear flange at the bolt positions 35 and 36.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      17. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-550).

      1. Put the bracket into position on the HP compressor front case rear flange at the bolt positions 38 and 39.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      18. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-720).

      1. Put the bracket into position on the compressor rear outer case front flange at the bolt holes 43 and 44.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      19. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-800).

      1. Put the bracket into position on the HP compressor rear outer case rear flange at the bolt holes 46 and 47.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      20. Pre SBE 72-0223: Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASESand ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-760).

      1. Put the two brackets into position on the compressor rear outer case front flange at the bolt holes 48 and 49. Bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-760) goes on the rear of the flange.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the brackets to the flange.

      3. Lightly tighten the two nuts.

      1. Put the two brackets into position on the compressor rear outer case front flange at the bolt holes 48 and 49. Bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-760) goes on the rear of the flange.

      2. Install the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the nut ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the bolt position 48 and the bolt ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-314) and the nut ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the bolt position 49 to attach the brackets to the flange.

      3. Lightly tighten the two nuts.

      22. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-800).

      1. Put the bracket into position on the HP compressor rear outer case rear flange at the bolt holes 50 and 51.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      23. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-770).

      1. Put the bracket into position on the compressor rear outer case front flange at the bolt holes 52 and 53.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-314) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

      24. Install the bracket ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 03-790).

      1. Put the bracket into position on the compressor rear outer case front flange at the bolt holes 54 and 1.

      2. Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the two nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) to attach the bracket to the flange.

      3. Lightly tighten the two nuts.

    25. Install the remaining bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-308) and the nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-302) at the remaining bolt holes.

    26. Pre SBE 72-0119: Torque the 53 nuts to 180 to 220 lbf.in (20.00 to 25.00 Nm).

    27. Torque the bolt at bolt position 20 to 180 to 220 lbfin (20.00 to 25.00 Nm).

    28. SBE 72-0119: Torque the 54 nuts to 180 to 220 lbf.in (20.00 to 25.00 Nm).

    5. SUBTASK 72-41-00-440-202-A00 Install the Variable Inlet Guide Vane Connectors (Pre SBE 72-0402, SBE 70-0813, Pre SBE 72-0385 or SBE 72-0416:, SBE 72-0385 or SBE 72-0416:)

    1. Refer to Figure and Figure.SBE 72-0402SBE 70-0813SBE 72-0385SBE 72-0416

      2. Install the variable inlet guide vane connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-200).

      1. Remove the four nuts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-123) and the four actuating levers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-120) from the inlet guide vanes at the positions 1, 2, 39 and 40.

      2. Put the left hand connector in to position on the upper and lower actuating rings.

      3. Pre SBE 72-0385 or SBE 72-0416: Install the three hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-206) and the three bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-202), which attach the left hand VIGV connector to the upper and lower actuating rings. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      4. SBE 72-0385: Install the three bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-202), which attach the left hand VIGV connector to the upper and lower actuating rings. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      5. SBE 72-0416: Install the three bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-202) and the three washers (72-41-34. 02-205), which attach the left hand VIGV connector to the upper and lower actuating rings. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      6. Pre SBE 72-0385 or SBE 72-0416: Install the hollow dowel ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-208) and the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-203), which attach the left hand VIGV connector to the lower actuating ring. Torque the bolt to 180 to 220 lbfin (20 to 25 Nm). Safety the bolt with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT or CoMat 02-126 LOCKWIRE .

      7. SBE 72-0385: Install the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-203), which attach the left hand VIGV connector to the lower actuating ring. Torque the bolt to 180 to 220 lbfin (20 to 25 Nm). Safety the bolt with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT or CoMat 02-126 LOCKWIRE .

      8. SBE 72-0416: Install the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-203) and the washer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-207) which attach the left hand VIGV connector to the lower actuating ring. Torque the bolt to 180 to 220 lbfin (20 to 25 Nm). Safety the bolt with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT or CoMat 02-126 LOCKWIRE .

      9. Install the remaining connector as given in steps A.(2) to (8) on to the actuating rings adjacent to the inlet guide vanes at the positions 19 thru 22.

      3. Install the actuating levers on to the inlet guide vanes and bridge pieces. These were removed in step A.

      1. Install the actuating levers on to the inlet guide vanes at the positions 1, 2, 19 to 22, 39 and 40. Install the pins of the actuating levers in to the correct location in the connectors.

      2. Install the nuts on to the inlet guide vane spindles. These were removed in step A.

      3. Set the inlet guide vane actuating levers parallel with the HP compressor assembly centre line. This is the null position.

      4. Torque the eight nuts, installed in step C.(2) to 85 to 105 lbfin (10.00 to 12.00 Nm).

    6. SUBTASK 72-41-00-440-202-B00 Install the Variable Inlet Guide Vane Connectors (SBE 72-0402, SBE 70-0813, Pre SBE 72-0385 or SBE 72-0416:, SBE 72-0385 or SBE 72-0416:)

    1. Refer to Figure and Figure. SBE 72-0402SBE 70-0813SBE 72-0385SBE 72-0416

    2. Install the variable inlet guide vane connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-200).

      1. Remove the four nuts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-123) and the four actuating levers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-120) from the inlet guide vanes at the positions 1, 2, 39 and 40, Figure.

      2. Put the left hand connector in to position on the upper and lower actuating rings.

      3. Pre SBE 72-0385 or SBE 72-0416: Install the three hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-206) and the three bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-202), which attach the left hand VIGV connector to the upper and lower actuating rings. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      4. SBE 72-0385: Install the three bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-202), which attach the left hand VIGV connector to the upper and lower actuating rings. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      5. SBE 72-0416: Install the three bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-202) and the washer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-205) which attach the left hand VIGV connector to the upper and lower actuating rings. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      6. Pre SBE 72-0385 or SBE 72-0416: Install the hollow dowel ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-208) and the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-203), which attach the left hand VIGV connector to the lower actuating ring. Torque the bolt to 180 to 220 lbfin (20 to 25 Nm). Safety the bolt with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT or CoMat 02-126 LOCKWIRE .

      7. SBE 72-0385: Install the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-203), which attach the left hand VIGV connector to the lower actuating ring. Torque the bolt to 180 to 220 lbfin (20 to 25 Nm). Safety the bolt with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT or CoMat 02-126 LOCKWIRE .

      8. SBE 72-0416: Install the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-203) and the washer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 02-207) which attach the left hand VIGV connector to the lower actuating ring. Torque the bolt to 180 to 220 lbfin (20 to 25 Nm). Safety the bolt with CoMat 02-274 SAFETY CABLE KIT or CoMat 02-275 SAFETY CABLE KIT or CoMat 02-126 LOCKWIRE .

      9. Install the remaining connector as given in steps A. (2) to (8) on to the actuating rings adjacent to the inlet guide vanes at the positions 19 thru 22.

      10. Pre SBE 72-0385 or SBE 72-0416: After the installation of the connectors make sure that the dowels are correctly installed, refer to Step.

      4. Install the actuating levers on to the inlet guide vanes and bridge pieces. These were removed in step A.

      1. Install the actuating levers on to the inlet guide vanes at the positions 1, 2, 19 to 22, 39 and 40. Install the pins of the actuating levers in to the correct location in the connectors.

      2. Install the nuts on to the inlet guide vane spindles. These were removed in step A.

      3. Set the inlet guide vane actuating levers parallel with the HP compressor assembly centre line. This is the null position.

      4. Torque the eight nuts, installed in step C.(2) to 85 to 105 lbfin (10.00 to 12.00 Nm).

    7. SUBTASK 72-41-00-440-203-A00 Install the Stage 3 Actuating Ring Connectors (Pre SBE 72-0402, Pre SBE 72-0385 or SBE 72-0416:, SBE 72-0385 or SBE 72-0416:)

      Figure and FigureSBE 72-0402SBE 72-0385SBE 72-0416

      1. Put the right hand connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-280) in to position on the upper and lower actuating rings adjacent to the stator vanes at the positions 1, 2, 31 and 32. Engage the connector on the pins of the stator vanes actuating levers. Make sure the actuating levers pins are correctly engaged in the connector.

      2. Pre SBE 72-0385 or SBE 72-0416: Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-286) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-282) which attach the RH stage 3 connector to the stage 3 stator vane upper and lower actuating rings..

      3. SBE 72-0385: Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-282) which attach the RH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      4. SBE 72-0416: Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-282) and the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-285) which attach the RH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      5. Pre SBE 72-0385 or SBE 72-0416: Install the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-284) and dowel ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-288) which attaches the RH stage 3 connector to the stator vane lower actuating rings.

      6. SBE 72-0385 or SBE 72-0416: Install the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-284) and washer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-287) which attaches the RH stage 3 connector to the stator vane lower actuating rings.

      7. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      8. Install the left hand connector ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-200) as given in steps below on to the actuating rings adjacent to the stage 3 stator vanes at the positions 15 to 18.

      9. Pre SBE 72-0385 or SBE 72-0416: Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34,03-206) and four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34,03-202) which attach the LH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      10. SBE 72-0385: Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34,03-202) which attach the LH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      11. SBE 72-0416: Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34,03-202) and the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-205) which attach the LH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      12. Torque the four bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

        13. Torque the nuts which attach the actuating levers to the stage 3 stator vanes at the positions 1, 2, 15 thru 18, 31 and 32.

        1. Set the stage 3 actuating levers parallel with the HP compressor assembly centre line. This is the null position.

        2. Torque the eight nuts to 85 to 105 lbfin (10.00 to 12.00 Nm).

    8. SUBTASK 72-41-00-440-203-B00 Install the Stage 3 Actuating Ring Connectors (SBE 72-0402, Pre SBE 72-0385 or SBE 72-0416:, SBE 72-0385 or SBE 72-0416:)

    1. Refer to Figure and Figure. SBE 72-0402SBE 72-0385SBE 72-0416

      1. Put the right hand connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-280) in to position on the upper and lower actuating rings adjacent to the stator vanes at the positions 1, 2, 31 and 32. Engage the connector on the pins of the stator vanes actuating levers. Make sure the actuating levers pins are correctly engaged in the connector.

      2. Pre SBE 72-0385 or SBE 72-0416: Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-286) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-282). These attach the connector to the actuating rings.

      3. SBE 72-0385: Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-282) which attach the RH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      4. SBE 72-0416: Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-282) and the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-285) which attach the RH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      5. Pre SBE 72-0385 or SBE 72-0416: Install the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-284) and dowel ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-288) which attaches the RH stage 3 connector to the stator vane lower actuating rings.

      6. SBE 72-0385 or SBE 72-0416: Install the bolt ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-284) and washer ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-287) which attaches the RH stage 3 connector to the stator vane lower actuating rings.

      7. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      8. Install the left hand connector ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-200) as given in steps below on to the actuating rings adjacent to the stage 3 stator vanes at the positions 15 to 18.

      9. Pre SBE 72-0385 or SBE 72-0416: Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-206) and four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-202) which attach the LH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      10. SBE 72-0385: Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34,03-202) which attach the LH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      11. SBE 72-0416: Install the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34,03-202) and the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-205) which attach the LH stage 3 connector to the stage 3 stator vane upper and lower actuating rings.

      12. Torque the four bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      13. Pre SBE 72-0385 or SBE 72-0416: After the installation of the connectors make sure that the dowels are correctly installed, refer to Step.

        14. Torque the nuts which attach the actuating levers to the stage 3 stator vanes at the positions 1, 2, 15 thru 18, 31 and 32.

        1. Set the stage 3 actuating levers parallel with the HP compressor assembly centre line. This is the null position.

        2. Torque the eight nuts to 85 to 105 lbfin (10.00 to 12.00 Nm).

    9. SUBTASK 72-41-00-440-204-A00 Install the Stage 4 Actuating Ring Connectors (Pre SBE 72-0402, Pre SBE 72-0348, Pre SBE 72-0385 or SBE 72-0416:, SBE 72-0348, SBE 72-0385 or SBE 72-0416:)

      Figure and FigureSBE 72-0402SBE 72-0348SBE 72-0385SBE 72-0416

      1. Install the two connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-200).

      1. Put the right hand connector into position on the upper and lower actuating rings adjacent to the stator vanes at the positions 1, 2, 49 and 50. Engage the connector on the pins of the stator vanes actuating levers. Make sure the actuating lever pins are correctly engaged in the connector.

      2. Pre SBE 72-0348: Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-206) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-202), which attach the right hand stage 4 connector and connector housings to the stage 4 upper and lower actuating rings.

      3. SBE 72-0348: Install the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-202), which attach the right hand stage 4 connector and connector housings to the stage 4 upper and lower actuating rings.

      4. Pre SBE 72-0385 or SBE 72-0416: Install the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-202), which attach the right hand stage 4 connector and connector housings to the stage 4 upper and lower actuating rings.

      5. SBE 72-0385 or SBE 72-0416: Install the two washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-202), which attach the right hand stage 4 connector and connector housings to the stage 4 upper and lower actuating rings.

      6. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      7. Install the left connector piece as given in steps A.(1) to (7) on to the actuating rings adjacent to the stage 4 stator vanes at the positions 24 thru 27.

      2. Torque the nuts which attach the actuating levers to the stage 4 stator vanes at the positions 1, 2, 24 thru 27, 49 and 50.

      1. Set the stage 4 actuating levers parallel with the HP compressor assembly centre line. This is the null position.

      2. Torque the eight nuts to 85 to 105 lbfin (10.00 to 12.00 Nm).

    10. SUBTASK 72-41-00-440-204-B00 Install the Stage 4 Actuating Ring Connectors (SBE 72-0402, Pre SBE 72-0348, Pre SBE 72-0385 or SBE 72-0416:, SBE 72-0348, SBE 72-0385 or SBE 72-0416:)

    1. Refer to Figure and Figure. SBE 72-0402SBE 72-0348SBE 72-0385SBE 72-0416

      2. Install the two connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-200).

      1. Put the right hand connector into position on the upper and lower actuating rings adjacent to the stator vanes at the positions 1, 2, 49 and 50. Engage the connector on the pins of the stator vanes actuating levers. Make sure the actuating lever pins are correctly engaged in the connector.

      2. Pre SBE 72-0348: Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-206) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-202), which attach the right hand stage 4 connector and connector housings to the stage 4 upper and lower actuating rings.

      3. SBE 72-0348: Install the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-202), which attach the right hand stage 4 connector and connector housings to the stage 4 upper and lower actuating rings.

      4. Pre SBE 72-0385 or SBE 72-0416: Install the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-202), which attach the right hand stage 4 connector and connector housings to the stage 4 upper and lower actuating rings.

      5. SBE 72-0385 or SBE 72-0416: Install the two washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 04-202), which attach the right hand stage 4 connector and connector housings to the stage 4 upper and lower actuating rings.

      6. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      7. Install the left connector piece as given in steps A.(1) to (7) on to the actuating rings adjacent to the stage 4 stator vanes at the positions 24 thru 27.

      8. Pre SBE 72-0385 or SBE 72-0416: After the installation of the connectors make sure that the dowels are correctly installed, refer to Step.

      3. Torque the nuts which attach the actuating levers to the stage 4 stator vanes at the positions 1, 2, 24 thru 27, 49 and 50.

      1. Set the stage 4 actuating levers parallel with the HP compressor assembly centre line. This is the null position.

      2. Torque the eight nuts to 85 to 105 lbfin (10.00 to 12.00 Nm).

    11. SUBTASK 72-41-00-440-205-A00 Install the Stage 5 Actuating Ring Connectors (Pre SBE 72-0402, Pre SBE 72-0348, Pre SBE 72-0385 or SBE 72-0416:, SBE 72-0348, SBE 72-0385 or SBE 72-0416:)

    1. Refer to Figure and Fig-72-41-00-990-282-002SBE 72-0402SBE 72-0348SBE 72-0385SBE 72-0416

      2. Install the two connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-200).

      1. Put the right hand connector into position on the upper and lower actuating rings adjacent to the stator vanes at the positions 1 thru 3 and 62 thru 64. Engage the connector on the pins of the stator vanes actuating levers. Make sure the actuating lever pins are correctly engaged in the connector.

      2. Pre SBE 72-0348: Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-206) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-202), which attach the right hand stage 5 connector and connector housings to the stage 5 upper and lower actuating ring.

      3. SBE 72-0348: Install the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-202), which attach the right hand stage 5 connector and connector housings to the stage 5 upper and lower actuating ring.

      4. Pre SBE 72-0385 or SBE 72-0416: Install the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-202), which attach the right hand stage 5 connector and connector housings to the stage 5 upper and lower actuating ring.

      5. SBE 72-0385 or SBE 72-0416: Install the two washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-202), which attach the right hand stage 5 connector and connector housings to the stage 5 upper and lower actuating ring.

      6. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      7. Install the left hand connector as given in steps A.(1) thru (7) on to the actuating rings adjacent to the stage 5 stator vanes at the positions 30 thru 35.

      3. Torque the nuts which attach the actuating levers to the stage 5 stator vanes at the positions 1 thru 3, 30 thru 35 and 62 thru 64.

      1. Set the stage 5 actuating levers parallel with the HP compressor assembly centre line. This is the null position.

      2. Torque the 12 nuts to 85 to 105 lbfin (10.00 to 12.00 Nm).

    12. SUBTASK 72-41-00-440-205-B00 Install the Stage 5 Actuating Ring Connectors (SBE 72-0402, Pre SBE 72-0348, Pre SBE 72-0385 or SBE 72-0416:, SBE 72-0348, SBE 72-0385 or SBE 72-0416:)

    1. Refer to Figure and Fig-72-41-00-990-282-002SBE 72-0402SBE 72-0348SBE 72-0385SBE 72-0416

      2. Install the two connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-200).

      1. Put the right hand connector into position on the upper and lower actuating rings adjacent to the stator vanes at the positions 1 thru 3 and 62 thru 64. Engage the connector on the pins of the stator vanes actuating levers. Make sure the actuating lever pins are correctly engaged in the connector.

      2. Pre SBE 72-0348: Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-206) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-202), which attach the right hand stage 5 connector and connector housings to the stage 5 upper and lower actuating.

      3. SBE 72-0348: Install the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-202), which attach the right hand stage 5 connector and connector housings to the stage 5 upper and lower actuating ring.

      4. Pre SBE 72-0385 or SBE 72-0416: Install the four washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-202), which attach the right hand stage 5 connector and connector housings to the stage 5 upper and lower actuating ring.

      5. SBE 72-0385 or SBE 72-0416: Install the two washers ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-204) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 05-202), which attach the right hand stage 5 connector and connector housings to the stage 5 upper and lower actuating ring.

      6. Torque the bolts to 85 to 105 lbfin (10.00 to 12.00 Nm).

      7. Install the left hand connector as given in steps A.(1) thru (7) on to the actuating rings adjacent to the stage 5 stator vanes at the positions 30 thru 35.

      8. Pre SBE 72-0385 or SBE 72-0416: After the installation of the connectors make sure that the dowels are correctly installed, refer to Step.

      3. Torque the nuts which attach the actuating levers to the stage 5 stator vanes at the positions 1 thru 3, 30 thru 35 and 62 thru 64.

      1. Set the stage 5 actuating levers parallel with the HP compressor assembly centre line. This is the null position.

      2. Torque the 12 nuts to 85 to 105 lbfin (10.00 to 12.00 Nm).

    13. SUBTASK 72-41-00-440-210-A00 Install the Stage 6 Actuating Ring Connectors

    1. Refer to Figure and Figure.

      2. Install the stage 6 connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 06-200).

      1. Put the right hand connector into position on the upper and lower actuating rings adjacent to the stator vanes at the positions 1 to 4 and 81 to 84. Engage the connector on the pins of the stator vanes actuating levers. Make sure the actuating lever pins are correctly engaged in the connector.

      2. Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 06-206) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 06-202). These attach the connector to the actuating rings.

      3. Torque the bolts to 35 to 45 lbfin (4.00 to 5.00 Nm).

      4. Install the left hand connector as given in step A.(1) thru (3) on to the actuating rings adjacent to the stage 6 stator vanes at the positions 39 thru 46.

      3. Torque the nuts which attach the actuating levers to the stage 6 stator vanes at the positions 1 thru 4, 39 thru 46 and 81 thru 84.

      1. Set the stage 6 actuating levers parallel with the HP compressor assembly centre line. This is the null position.

      2. Torque the 16 nuts to 85 to 105 lbfin (10.00 to 12.00 Nm).

    14. SUBTASK 72-41-00-440-210-B00 Install the Stage 6 Actuating Ring Connectors (SBE 72-0402)

    1. Refer to Figure and Figure. SBE 72-0402

      2. Install the stage 6 connectors ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 06-200).

      1. Put the right hand connector into position on the upper and lower actuating rings adjacent to the stator vanes at the positions 1 to 4 and 81 to 84. Engage the connector on the pins of the stator vanes actuating levers. Make sure the actuating lever pins are correctly engaged in the connector.

      2. Install the four hollow dowels ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 06-206) and the four bolts ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 06-202). These attach the connector to the actuating rings.

      3. Torque the bolts to 35 to 45 lbfin (4.00 to 5.00 Nm).

      4. Install the left hand connector as given in step A.(1) thru (3) on to the actuating rings adjacent to the stage 6 stator vanes at the positions 39 thru 46.

      5. Pre SBE 72-0385 or SBE 72-0416: After the installation of the connectors make sure that the dowels are correctly installed, refer to Step.

      3. Torque the nuts which attach the actuating levers to the stage 6 stator vanes at the positions 1 thru 4, 39 thru 46 and 81 thru 84.

      1. Set the stage 6 actuating levers parallel with the HP compressor assembly centre line. This is the null position.

      2. Torque the 16 nuts to 85 to 105 lbfin (10.00 to 12.00 Nm).

    15. SUBTASK 72-41-00-220-193 Check the Installation of the Left and Right Hand Connectors and VSV Actuating Ring Assembly (SBE 72-0402)

    1. Refer to Figure. SBE 72-0402

    2. This check must be done after each time the connectors are installed to the VSV actuating ring assemblies.

      3. This is the general procedure to make sure that the left and right hand connectors which are installed to the upper and lower actuating rings are installed correctly. The check will make sure that the dowels which hold the connectors to the actuating ring are installed correctly and are not mis-seated. The following gives the causes of an incorrectly installed assembly and what to look for :-.

      1. It is not easy to decide if the connectors for a particular stage is installed incorrectly. An incorrect installation can occur if a dowel is not installed correctly in a mating hole of an actuating ring and instead touches the mating face of the actuating ring.

        The wall of the actuating ring can become clamped between the dowel and the internal actuating ring boss, when this occurs the bridge piece is not held. The head of the mis-seated dowel can be visible above the connector and/or the connector could be offset from the actuating ring.

        No indication of misaligned connectors is evident when the bolt(s) are torque tightened because of a 'cross-keying' action of the dowels in the connectors.

      4. Inspect the left hand and right hand actuating ring and connector joint for each stage.

      1. Check the clearance between the connector and the actuating ring, it should be possible to put a 0.001 in. or 0.002 in. (0.025 mm. or 0.05 mm) feeler gauge in the clearance. If this is not possible do step (2).

      2. For the left hand and/or right hand joint (as applicable) examine the dowel heads, use a torch if necessary. Make a comparison in the position of each dowel. Look for differences in radial distances between the connector and the upper and lower actuating ring, all the distances should be the same. If there is a distance which does not appear regular then do steps (3) to (5).

      3. Remove the connector and look for new marks on the actuating ring adjacent to the dowel mating hole caused by a mis-aligned dowel.

      4. Install the connector and make sure the dowels are correctly seated before you torque tighten the bolts.

    16. SUBTASK 72-41-00-440-206 Connect the Stage 3 VSV Control Rod

    1. Refer to Figure.

      2. Install the stage 3 control rod assembly V2500-A1-72-41-34-01A-941A-D (72-41-34, 01-250).

      1. Locate the left hand bearing V2500-A1-72-41-34-01A-941A-D (72-41-34, 01-240) in the connector on the lower stage 3 actuating ring ACTUATING MECHANISM HP COMPRESSOR VARIABLE VANES (72-41-34, 03-540).

      2. Install the bolt V2500-A1-72-41-34-01A-941A-D (72-41-34, 01-236) and the nut V2500-A1-72-41-34-01A-941A-D (72-41-34, 01-232) to attach the stage 3 control rod to the stage 3 unison ring.

      3. Torque the nut to 180 to 220 lbfin (20 to 25 Nm).

    17. SUBTASK 72-41-00-560-016 Install the HP Compressor Support Rods

    1. Make sure that the variable stator vanes (VSV) are in the low speed position.

    2. Install IAE 1R18247 Rigging pin 1 off through the bracket and into the HP compressor cases to lock the VSV's.

    3. Remove the six bolts ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-122), the two brackets ENGINE-HP COMPRESSOR SPLIT CASES and ENGINE-HP COMPRESSOR SPLIT CASES (72-41-00, 01-118) and the three blanks ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-120) from the HP compressor front cases.

      4. Install IAE 1R18234 Support rod 1 off into the holes in the split cases.

      1. Turn the adjustment handle to retract the blade of the tool.

      2. Install the support rods through the holes in the HP compressor split case. Make sure the tool blades are rearwards.

      3. Safety the support rods to the HP compressor split cases with the six tool bolts.

      4. Turn the adjustment handles until the tool blades touch the HP compressor stage 3 disk then hand tighten the handles.

    18. SUBTASK 72-41-00-560-017-0 Install the Trunnion Assemblies on to the HP System Module

    1. Refer to Figure and Figure.

    2. NOTE

      Keep the 10 nuts removed in step A. so that they can be used to install the trunnion assemblies.

      Remove the 10 nuts and the 10 bolts from the HP compressor front and rear cases splitline at the No. 8, 10, 16, 17, 19, 35, 37, 38, 44 and 46 positions. The No. 1 hole position is to the right of TDC.

      1. Locate the right hand trunnion assembly on to the HP compressor front and rear cases splitline. Make sure the clearance holes engage on the head of the bolts at the No. 9 and 18 positions.

      2. Attach the trunnion assembly to the module with the five tool bolts and five of the nuts removed in step A. Tighten the nuts to safety the trunnion assembly.

      3. Locate the left hand trunnion assembly on to the HP compressor front and rear cases splitline. Make sure the clearance holes engage on the head of the bolts at the No. 36 and 45 positions.

      4. Attach the trunnion assembly to the module with the five tool bolts and the other five nuts removed in step A. Tighten the nuts to safety the trunnion assembly.

    19. SUBTASK 72-41-00-440-207 Remove the HP Compressor Assembly from the Build Stand IAE 1R19463

    1. Refer to Figure, Figure and Figure.

    2. Attach a hoist to the lift eye on IAE 1F10052 Two cables sling 1 off.

      3. Attach the lift sling to the IAE 1P16046 Removal/Installation fixture or IAE 1P16543 Removal/Installation fixture 1 off trunnions, refer to Figure.

      1. Use the hoist to position the lift sling over the HP system module.

      2. Adjust the height of the lift sling to permit the hook and bolt plate to be attached to the remove/install fixture trunnions.

      3. Attach the hook and bolt plate to the remove/install fixture trunnions.

    4. Disassemble and remove the three hand knobs, pins, plain washers and studs (details 22, 27, 16 and 14). Loosen the locknut on the heel pin (detail 15). Remove three retaining clamp plates (detail 5).

    5. CAUTION

      YOU MUST KEEP THE WEIGHT OF THE MODULE ON THE HOIST WHEN THE SLIDE IN-RIGGERS ARE LOOSENED AND MOVED FROM THEIR SECURING POSITIONS. THE HP CASES COULD MOVE RELATIVE TO THE HP ROTOR AND CAUSE DAMAGE TO ENGINE COMPONENTS.

      Take up the weight of the module on the hoist and slightly loosen the 12 nuts (detail 24) which secure the three in-riggers, remove the three jacking screws (detail 12) from through the three support plates (detail 4). Slide the in-riggers (detail 6,7 and 8) outwards from their positions.

    6. Remove the six bolts (detail 17) at positions 1, 8, 9, 17, 18 and 25 which secure the three support plates (detail 4) to the IAE 1P16046 Removal/Installation fixture or IAE 1P16543 Removal/Installation fixture and module rear flange. Remove the three support plates.

    7. Install the six bolts, nuts and washers at positions 1, 8,9, 17, 18 and 25. Tighten the bolts.

    8. Make sure that the remove/install fixture lifting eyes are stowed securely so as not to interfere with the surgical strike tooling when the module is lifted from the stand.

    9. Slowly and carefully lift the module so the dummy stub shaft is clear of the location pot. Remove the HP system module from the build stand.

    20. SUBTASK 72-41-00-440-208-A00 Install the Variable Inlet Guide Vane Front Shroud (Pre SBE 72-0402, Pre SBE 72-0422, SBE 72-0422)

    1. Refer to Figure. SBE 72-0402SBE 72-0422

      2. Install the variable inlet guide vane front half shroud ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-200).

      1. Remove the six bolts and the six nuts which attach the split ring assembly to the variable inlet guide vane rear half shroud.

      2. Pre SBE 72-0422: Remove the two halves of the IAE 1R18250 Split ring assembly1 off.

      3. Apply a thin layer of CoMat 04-007 SILICONE GREASE to the 40 half bushes ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190) outer surface.

      4. Install the 40 half bushes in to the variable inlet guide vane front half shroud.

      5. NOTE

        The inlet guide vane rear upper half shroud has four location dowels.

        Align the variable inlet guide vane front and rear half shrouds.

      6. Install the 20 bolts ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-138), the 40 dee-headed washers ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-134) and the 20 nuts ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-130). These attach the two halves of the inlet guide vane front shroud.

      7. Torque the 20 nuts to 36 to 45 lbfin (4.00 to 5.00 Nm).

      8. SBE 72-0422: Remove the two halves of the IAE 1R19633 Split ring assembly 1 off. Make sure the 40 one piece bushes are attached to the stator vanes.

      9. Apply a thin layer of CoMat 04-007 SILICONE GREASE to the 40 bushes ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190) outer surface.

      10. NOTE

        The inlet guide vane rear upper half shroud has four location dowels.

        Align the variable inlet guide vane front and rear half shrouds.

      11. Install the 20 bolts ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-138), the 40 dee-headed washers ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-134) and the 20 nuts ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-130). These attach the two halves of the inlet guide vane front shroud.

      12. Torque the 20 nuts to 36 to 45 lbfin (4.00 to 5.00 Nm).

    21. SUBTASK 72-41-00-440-208-B00 Install the Variable Inlet Guide Vane Front Half Shroud (SBE 72-0402, Pre SBE 72-0422, SBE 72-0422)

    1. Refer to Figure. SBE 72-0402SBE 72-0422

      2. Install the variable inlet guide vane front half shroud ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-200).

      1. Remove the six bolts and the six nuts which attach the IAE 1R18250 Split ring assembly 1 off to the variable inlet guide vane rear half shroud, Figure.

      2. Pre SBE 72-0422: Remove the two halves of the IAE 1R18250 Split ring assembly 1 off.

      3. Apply a thin layer of CoMat 04-007 SILICONE GREASE to the 40 half bushes ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190) outer surface.

      4. Install the 40 half bushes into the variable inlet guide vane front half shroud.

      5. NOTE

        The inlet guide vane rear upper half shroud has four location dowels.

        Align the variable inlet guide vane front and rear half shrouds.

      6. Install the 20 bolts ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-138), the 40 dee-headed washers ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-134) and the 20 nuts ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-130). These attach the two halves of the inlet guide vane front shroud.

      7. Torque the 20 nuts to 36 to 45 lbfin (4.00 to 5.00 Nm).

      8. SBE 72-0422: Remove the two halves of the IAE 1R19633 Split ring assembly 1 off. Make sure the 40 one piece bushes are attached to the stator vanes.

      9. Apply a thin layer of CoMat 04-007 SILICONE GREASE to the 40 bushes ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-190) outer surface.

      10. NOTE

        The inlet guide vane rear upper half shroud has four location dowels.

        Align the variable inlet guide vane front and rear half shrouds.

      11. Install the 20 bolts ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-138), the 40 dee-headed washers ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-134) and the 20 nuts ENGINE-HP COMPRESSOR VARIABLE VANE INNER SHROUDS (72-41-33, 01-130). These attach the two halves of the inlet guide vane front shroud.

      12. Torque the 20 nuts to 36 to 45 lbfin (4.00 to 5.00 Nm).

    22. SUBTASK 72-41-00-560-018 Turn the HP System Module and Install on to the Support Posts and Cradle Pedestal

    1. Refer to Figure and Figure.

    2. Attach a hoist to the lift eye on a second IAE 1F10052 Two cables sling 1 off. Refer to Figure .

      3. Attach the lift sling to the HP compressor trunnion assemblies.

      1. Use the hoist to position the lift sling adjacent to the HP system module.

      2. Adjust the height of the lift sling so that the hook and bolt plate can be attached to the HP compressor trunnion assemblies.

      3. Attach the hook and bolt plate to the trunnions, safety the hook and bolt plate with the safety clip.

    4. Use the forward lift sling to move the HP system module in to the horizontal position.

      5. Install the HP system module on to the support posts and cradle pedestal.

      1. Make sure that the trunnion support brackets, part of IAE 1F10028 Support Pedestal 1 off are at their lowest position.

      2. Put the support posts adjacent to the trunnion assemblies with the trunnion supports below the trunnions.

      3. CAUTION

        YOU MUST MAKE SURE THAT THE HEIGHT OF THE MODULE IS SUFFICIENT FOR THE CRADLE PEDESTAL TO BE INSTALLED.

        Move the trunnion support brackets up the support posts until they touch the trunnions.

      4. Look at the holes in the trunnion support brackets and the support posts to see if they are aligned.

      5. If necessary adjust the height of the HP system module to make the holes align.

      6. Install the retaining pins through the holes.

      7. Put IAE 1P16002 Cradle pedestal 1 off under the HP system module with the support bracket slightly forward of the diffuser case rear flange. Make sure that the large face of the support bracket is forward.

      8. Turn the adjustment handle on the cradle pedestal to move the support bracket upwards. When the cradle pedestal has taken the weight of the module stop the procedure.

      9. Remove the retaining pins from the lift sling hook and bolt plates.

      10. Adjust the height of the lift slings so that the hook and bolt plates can be removed.

      11. Remove the hook and bolt plates from the trunnions.

      12. Put the lift slings on an applicable work surface.

      13. Remove the hoists from the lift slings.

    23. SUBTASK 72-41-00-560-019 Remove the Remove/Install Fixture and the Tie-Rod Adapter from the Rear of the HP System Module

    1. Refer to Figure.

    2. NOTE

      If continuing with TASK 72-00-40-002-A00, Install the HP system module (horizontal) then the remove/install fixture need not be removed.

      Attach a hoist to the lift eye on the remove/install fixture and adjust the hoist to hold the remove/install fixture.

    3. Remove the 25 nuts and the 25 bolts which safety the remove/install fixture to the HP Turbine case. Remove the two split rings.

    4. Release the locknut on the end of the tie-rod shaft. Do not remove the locknut.

    5. Remove the two screws that safety the tie-rod adapter on to the remove/install fixture.

    6. Move the shaft in to the engine to disengage the puck from the HP compressor shaft front shoulder.

    7. Remove the tie-rod adapter from the module.

    8. Remove the remove/install fixture from the module and put it on an applicable work surface. Remove the hoist.

    24. SUBTASK 72-41-00-220-201 Examine the HPC Rear Shaft for Surface Damage

    1. Refer to Figure.

      2. Examine the rear shaft inner bore at locations 15 for surface damage. Refer to TASK 72-41-13, Inspection/Check-00.

        1. Surface damage not more than 0.0030 in. (0.076 mm) in depth.

        1. Accept.

        2. Other than Step.

        1. Reject.

    25. SUBTASK 72-41-00-560-020 Remove the Dummy Stub Shaft from the HP System Module

    1. Refer to Figure.

    2. NOTE

      The 20 curvic coupling tool bolts remain with the dummy stub shaft.

      Release the 20 curvic coupling tool bolts.

    3. Remove the dummy stub shaft from the curvic coupling.

      4. Install the curvic protector on to the dummy stub shaft.

      1. Align the location pins on the dummy stub shaft with the applicable location holes in the curvic protector.

      2. Secure the curvic protector with four of the dummy stub shaft curvic coupling bolts and the curvic protector nuts.

      3. Put the dummy stub shaft on to an applicable work surface.

    5. Install the curvic protector on to the stage 3 disk curvic coupling.

    26. SUBTASK 72-41-00-440-209 Install the Modules

      1. Install the HP stack.

      1. Install the HP system module (horizontal). Refer to TASK 72-00-40-420-002-A00.

      2. Install the components, the external harnesses and the tubes to the HP system module. Refer to TASK 72-00-40-420-005-A00, TASK 72-00-40-420-006-A00, TASK 72-00-40-420-007-A00, TASK 72-00-40-420-004 and associated TASKS.

      3. Turn the LP turbine module from vertical to horizontal. Refer to TASK 72-00-50-560-002.

      4. Install the LP turbine module. Refer to TASK 72-00-50-420-001.

      5. Install the components, the external harnesses and the tubes to the LP turbine module. Refer to TASK 72-00-50-420-005-A00.

    27. SUBTASK 72-41-00-720-004 Do a Check of the No.4 Front and Rear Bearing Compartment for Leaks

    1. Refer to Figure.

    2. Do a check on the No. 4 bearing chamber, if not disassembled.

    3. Install the IAE 1P16089 Leak check cap 1 off in the coupling nut of the pressure tube.

    4. Install the IAE 1P16088 Leak check adapter 1 off in the scavenge tube.

    5. Connect the IAE 6F10030 Vacuum test cart 1 off to the adapter.

    6. Adjust the vacuum on the cart to 20 in. HG and evacuate the bearing compartment. 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

    7. Check the air flow on the No. 4 front and rear bearing compartment. The air flow must be no more than 17 pph (7.71 Kgph). Make a record of the reading. The reading must agree with the vacuum check in TASK 72-41-00-040-001-C00.

    8. Decrease the vacuum to 0 in. Hg and disconnect the cart from the fixture.

    9. Remove the leak check cap from the pressure tube.

    10. Remove the leak check adapter from the scavenge tube.

    28. Figure: Set the True Axial Displacement of the HP Module Cases and Stage 2 HP Turbine

    Set the True Axial Displacement of the HP Module Cases and Stage 2 HP Turbine

    Figure: Pre SBE 72-0027: Install the HP compressor front case split line flange bolts

    Sheet 1

    Legend
    Pre SBE 72-0027: Install the HP compressor front case split line flange bolts

    Sheet 1

    Close

    Figure: SBE 72-0027: Install the HP compressor front case split line flange bolts

    Sheet 2

    Legend
    SBE 72-0027: Install the HP compressor front case split line flange bolts

    Sheet 2

    Close

    Figure: Install the HP compressor front case split line flange bolts

    Sheet 3

    Legend
    Install the HP compressor front case split line flange bolts

    Sheet 3

    Close

    Figure: Install the brackets, the pins, the bolts and the nuts at the HPcompressor front case to the compressor rear outer case flange

    Sheet 1

    Legend
    Install the brackets, the pins, the bolts and the nuts at the HPcompressor front case to the compressor rear outer case flange

    Sheet 1

    Close

    Figure: Install the brackets, the pins, the bolts and the nuts at the HPcompressor front case to the compressor rear outer case flange

    Sheet 2

    Legend
    Install the brackets, the pins, the bolts and the nuts at the HPcompressor front case to the compressor rear outer case flange

    Sheet 2

    Close

    Figure: Install the brackets, the pins, the bolts and the nuts at the HPcompressor front case to the compressor rear outer case flange

    Sheet 3

    Legend
    Install the brackets, the pins, the bolts and the nuts at the HPcompressor front case to the compressor rear outer case flange

    Sheet 3

    Close

    Figure: Install the inlet guide vane connectors

    Sheet 1

    Legend
    Install the inlet guide vane connectors

    Sheet 1

    Close

    Figure: Install the inlet guide vane connectors

    Sheet 2

    Legend
    Install the inlet guide vane connectors

    Sheet 2

    Close

    Figure: Install the stage 3 actuating ring connectors

    Sheet 1

    Legend
    Install the stage 3 actuating ring connectors

    Sheet 1

    Close

    Figure: Install the stage 3 actuating ring connectors

    Sheet 2

    Legend
    Install the stage 3 actuating ring connectors

    Sheet 2

    Close

    Figure: Install the stage 4 actuating ring connectors

    Sheet 1

    Legend
    Install the stage 4 actuating ring connectors

    Sheet 1

    Close

    Figure: Install the stage 4 actuating ring connectors

    Sheet 2

    Legend
    Install the stage 4 actuating ring connectors

    Sheet 2

    Close

    Figure: Install the stage 5 actuating ring connectors

    Sheet 1

    Legend
    Install the stage 5 actuating ring connectors

    Sheet 1

    Close

    Figure: Install the stage 6 actuating ring connectors

    Sheet 1

    Legend
    Install the stage 6 actuating ring connectors

    Sheet 1

    Close

    Figure: Install the stage 6 actuating ring connectors

    Sheet 2

    Legend
    Install the stage 6 actuating ring connectors

    Sheet 2

    Close

    Figure: Check the connector/bridge piece assemblies to VSV actuating ring installation for mis-seated dowels

    Check the connector/bridge piece assemblies to VSV actuating ring installation for mis-seated dowels

    Figure: VSV Crankshaft and unison rings - Connect stage 3 control rod

    VSV Crankshaft and unison rings - Connect stage 3 control rod

    Figure: Install the HP compressor support rods

    Sheet 1

    Legend
    Install the HP compressor support rods

    Sheet 1

    Close

    Figure: Install the HP compressor support rods

    Sheet 2

    Legend
    Install the HP compressor support rods

    Sheet 2

    Close

    Figure: Install the HP compressor trunnions

    Sheet 1

    Legend
    Install the HP compressor trunnions

    Sheet 1

    Close

    Figure: Install the HP compressor trunnions

    Sheet 2

    Legend
    Install the HP compressor trunnions

    Sheet 2

    Close

    Figure: Remove the HP compressor assembly from the build stand IAE 1R19463

    Sheet 1

    Legend
    Remove the HP compressor assembly from the build stand IAE 1R19463 Stand - Surgical strike

    Sheet 1

    Close

    Figure: Remove the HP compressor assembly from the build stand IAE 1R19463

    Sheet 2

    Legend
    Remove the HP compressor assembly from the build stand IAE 1R19463 Stand - Surgical strike

    Sheet 2

    Close

    Figure: Remove the HP compressor assembly from the build stand IAE 1R19463

    Sheet 3

    Legend
    Remove the HP compressor assembly from the build stand IAE 1R19463 Stand - Surgical strike

    Sheet 3

    Close

    Figure: Remove the VIGV split ring IAE1R18250

    Remove the VIGV split ring IAE1R18250

    Figure: Install the variable inlet guide vane front shroud

    Install the variable inlet guide vane front shroud

    Figure: Install the forward lift sling to the HP compressor trunnions

    Install the forward lift sling to the HP compressor trunnions

    Figure: Install the lift slings on to the trunnions

    Install the lift slings on to the trunnions

    Figure: Remove the dummy stub shaft from the stage 3 disk curvic coupling

    Remove the dummy stub shaft from the stage 3 disk curvic coupling

    Figure: Remove the remove/install fixture and tie-rod adapter from thethe HP system module

    Remove the remove/install fixture and tie-rod adapter from thethe HP system module

    Figure: Check the No.4 front and rear bearing compartment for leaks

    Check the No.4 front and rear bearing compartment for leaks

    Figure: HPC Rear Shaft Inspection Location

    HPC Rear Shaft Inspection Location

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Correct tool pn and provide link (CAS-20822-G2C1H9)

Manufacturer Code:00BB6
Enterprise Name:INDESTRUCTIBLE PAINT INC
BU Name:INDESTRUCTIBLE PAINT INC
Street:1 INDEPENDENCE DRIVE
City:MONROE
State:CT
Zip Code:06468
Country:USA
Phone Number:1-203-880-9130
Fax Number:1-203-880-9133
Email:dave@indestructiblepaint.com
Internet:www.indestructiblepaint.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:39428
Enterprise Name:McMASTER-CARR SUPPLY CO.
BU Name:McMASTER-CARR SUPPLY CO.
Street:600 COUNTY LANE ROAD
City:ELMHURST
State:IL
Zip Code:60126-2081
Country:USA
Phone Number:1-630-833-0300, 1-630-600-3600
Fax Number:1-630-834-9427
Internet:www.mcmaster.com
Manufacturer Code:K6835
Enterprise Name:MED-LAB LTD
BU Name:MED-LAB LTD
Street:COPELAND ST
City:DERBY
Zip Code:DE1 2PU
Country:GREAT BRITAIN
Phone Number:44-1332-349094
Fax Number:44-1332-371237
Email:sales@med-lab.co.uk
Internet:www.med-lab.co.uk
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:X222X
Enterprise Name:N/A – REFER TO APPLICABLE COMAT SUFFIX
Manufacturer Code:X333X
Enterprise Name:REFER TO V2500 SB ENG-79-0108
Manufacturer Code:K6835
Supply Number:CoMat 02-123
Type:sp01
Supply Short Name:CoMat 02-123 LAY-OUT FLUID
Supply Name:CoMat 02-123 LAY-OUT FLUID
Specification Groups:
Doc NumberType
OMAT: 263KOLOMAR BLUE SQ9B
Suppliers:
ManufacturerRemarks
K6835
Manufacturer Code:K6835
Supply Number:CoMat 02-126
Type:sp01
Supply Short Name:CoMat 02-126 LOCKWIRE
Supply Name:CoMat 02-126 LOCKWIRE
Specification Groups:
Doc NumberType
DTD 189A, 0.028 TO 0.032 IN DIA
Suppliers:
ManufacturerRemarks
K6835
KB362
LOCAL
U06C8
Manufacturer Code:LOCAL
Supply Number:CoMat 02-274
Type:sp01
Supply Short Name:CoMat 02-274 SAFETY CABLE KIT
Supply Name:CoMat 02-274 SAFETY CABLE KIT
Specification Groups:
Doc NumberType
SAE AS3510-0218K (DIA 0,032 IN LENGTH 18IN)
Suppliers:
ManufacturerRemarks
LOCAL
11851
U0419
70958
H7503
SA221
V384V
Manufacturer Code:X111X
Supply Number:CoMat 02-275
Type:sp01
Supply Short Name:CoMat 02-275 SAFETY CABLE KIT
Supply Name:CoMat 02-275 SAFETY CABLE KIT
Specification Groups:
Doc NumberType
Deleted. Use CoMat 02-274.
Suppliers:
ManufacturerRemarks
X111X
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:X222X
Supply Number:CoMat 08-013
Type:sp01
Supply Short Name:CoMat 08-013 COLD CURING SILICONE COMPOUND
Supply Name:CoMat 08-013 COLD CURING SILICONE COMPOUND
Specification Groups:
Doc NumberType
If CoMat 08-013 is specified without an asterisk or a letter suffix, use one of the letter suffix alternative materials.
Suppliers:
ManufacturerRemarks
X222X
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:DELETED
Tool Name:DELETED
Manufacturer Code:LOCAL
Tool Number:Dial Test Indicators
Tool Name:Dial Test Indicators
Manufacturer Code:LOCAL
Tool Number:Dial test indicator stands/blocks and associated equipment
Tool Name:Dial test indicator stands/blocks and associated equipment
Manufacturer Code:LOCAL
Tool Number:Flashlight
Tool Name:Flashlight
Manufacturer Code:0AM53
Tool Number:IAE 1F10028
Tool Name:IAE 1F10028 Support Pedestal
Manufacturer Code:0AM53
Tool Number:IAE 1F10052
Tool Name:IAE 1F10052 Two cables sling
Manufacturer Code:0AM53
Tool Number:IAE 1P16002
Tool Name:IAE 1P16002 Cradle pedestal
Manufacturer Code:0AM53
Tool Number:IAE 1P16046
Tool Name:IAE 1P16046 Removal/Installation fixture
Manufacturer Code:0AM53
Tool Number:IAE 1P16088
Tool Name:IAE 1P16088 Leak check adapter
Manufacturer Code:0AM53
Tool Number:IAE 1P16089
Tool Name:IAE 1P16089 Leak check cap
Manufacturer Code:0AM53
Tool Number:IAE 1P16285
Tool Name:IAE 1P16285 Tie-rod adapter
Manufacturer Code:0AM53
Tool Number:IAE 1P16543
Tool Name:IAE 1P16543 Removal/Installation fixture
Manufacturer Code:0AM53
Tool Number:IAE 1R18234
Tool Name:IAE 1R18234 Support rod
Manufacturer Code:0AM53
Tool Number:IAE 1R18247
Tool Name:IAE 1R18247 Rigging pin
Manufacturer Code:0AM53
Tool Number:IAE 1R18250
Tool Name:IAE 1R18250 Split ring assembly
Manufacturer Code:0AM53
Tool Number:IAE 1R18325
Tool Name:IAE 1R18325 Trunnion assembly
Manufacturer Code:0AM53
Tool Number:IAE 1R18673
Tool Name:IAE 1R18673 Dummy stub shaft
Manufacturer Code:0AM53
Tool Number:IAE 1R19463
Tool Name:IAE 1R19463 Stand - Surgical strike
Manufacturer Code:0AM53
Tool Number:IAE 1R19633
Tool Name:IAE 1R19633 Split ring assembly
Manufacturer Code:0AM53
Tool Number:IAE 6F10030
Tool Name:IAE 6F10030 Vacuum test cart