TASK 72-50-30-440-005-A00 LPT Stage 7 Rotor Assembly - Assemble, Assembly-005

DMC:V2500-A1-72-50-3007-00A-710A-B|Issue No:004.00|Issue Date:2020-11-01

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 72-50-30-440-005-A00 LPT Stage 7 Rotor Assembly - Assemble, Assembly-005

General

Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.

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

For standard torque data and procedures, refer to the 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 abutment faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS, unless other lubricants are referred to in the procedure.

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

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

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

The abbreviation Intf. shows an interference or light fit. This cause REJECT IF MORE THAN to become REJECT IF LESS THAN. The abbreviation Clear shows a clearance fit.

NOTE

To identify the consumable materials refer to the PCI.

NOTE

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

NOTE

During assembly, it is not necessary to measure, calculate and record the fits and clearances if:
a) Both parts are new, or
b) Used parts (inspected and/or repaired) are within limits.
Above is valid for any combinations of a) and b), except for "Selected Fit" parts.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Balancing machineLOCALBalancing machine
Blade distribution systemLOCALBlade distribution system
Feeler gageLOCALFeeler gage
IAE 1M14015 Blade holder0AM53IAE 1M140151
IAE 1M14019 Mounting adapter0AM53IAE 1M140191
IAE 1M14020 Balancing base plate0AM53IAE 1M140201
IAE 1M14025 Balancing fixture disk0AM53IAE 1M140251
IAE 1M14026 Balancing fixture sleeve0AM53IAE 1M140261
IAE 1M14030 Assembly trolley0AM53IAE 1M140301
IAE 1M14079 Plastic wedge0AM53IAE 1M140791
IAE 1M14091 Position retainer0AM53IAE 1M140911
IAE 1M14132 Guide pin0AM53IAE 1M141321
IAE 1M14153 Assy/disassy stand0AM53IAE 1M141531
IAE 1M14154 Assy/disassy stand0AM53IAE 1M141541
IAE 1M14155 Clamping ring0AM53IAE 1M141551
IAE 1M14156 Lifting fixture0AM53IAE 1M141561
MalletLOCALMallet

Soft head

Moment weighing equipmentLOCALMoment weighing equipment
OvenLOCALOven
Rack palletLOCALRack pallet
Torch lightLOCALTorch light

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-031 ACETONE (CH3)2COLOCALCoMat 01-031
CoMat 02-069 DISPOSABLE CLEANING TISSUES33591CoMat 02-069
CoMat 02-129 MARKERIAE28CoMat 02-129
CoMat 07-038 AIR DRYING ENAMELK3504CoMat 07-038
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-50-30-220-055-A00 Make sure that the Fits and Clearances between the Stage 7 Disk and the Stage 7 Air Seal are in the Limits given at Location 3364 (Pre SBE 72-0003 and Pre SBE 72-0138)

    1. Refer to Figure.

    2. Calculate the clearance at location 3364.

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

      NEW PART

      DIMENSIONS

      WORN PART

      DIMENSIONS

      REJECT IF

      PART IDENT

      Size

      Clearance

      (Non-select)

      MORE THAN

      LOCATION 3364

      Stage 7 air seal ENGINE-LP TURBINE ROTATING SEALS (72-50-33,01-010)

      to stage 7 turbine disk

      ENGINE-LP TURBINE DISCS (72-50-31,01-010)

      Disk dia

      19.1417

      19.1378

      Intf

      0.0157

      Intf

      0.0177

      Air seal dia

      19.1299

      19.1260

      0.0079

      0.0020

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

      NEW PART

      DIMENSIONS

      WORN PART

      DIMENSIONS

      REJECT IF

      PART IDENT

      Size

      Clearance

      (Non-select)

      MORE THAN

      LOCATION 3364

      Stage 7 air seal ENGINE-LP TURBINE ROTATING SEALS (72-50-33,01-010)

      to stage 7 turbine disk

      ENGINE-LP TURBINE DISCS (72-50-31,01-010)

      Disk dia

      486.2

      486.1

      Intf

      0.4

      Intf

      0.45

      Air seal dia

      485.9

      485.8

      0.2

      0.05

    2. SUBTASK 72-50-30-220-055-B00 Make sure that the Fits and Clearances between the Stage 7 Disk and the Stage 7 Air Seal are in the Limits given at Location 3364 (SBE 72-0003 and Pre SBE 72-0138)

    1. Refer to Figure.

    2. SBE 72-0003: Introduce a Weight Reduced Stage 7 LPT Air Seal

    3. Calculate the clearance at location 3364.

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

      NEW PART

      DIMENSIONS

      WORN PART

      DIMENSIONS

      REJECT IF

      PART IDENT

      Size

      Clearance

      (Non-select)

      MORE THAN

      LOCATION 3364

      Stage 7 air seal ENGINE-LP TURBINE ROTATING SEALS (72-50-33,01-010)

      to stage 7 turbine disk

      ENGINE-LP TURBINE DISCS (72-50-31,01-010)

      Disk dia

      19.1417

      19.1378

      Intf

      0.0236

      Intf

      0.0255

      Air seal dia

      19.1221

      19.1181

      0.0157

      0.0119

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

      NEW PART

      DIMENSIONS

      WORN PART

      DIMENSIONS

      REJECT IF

      PART IDENT

      Size

      Clearance

      (Non-select)

      MORE THAN

      LOCATION 3364

      Stage 7 air seal ENGINE-LP TURBINE ROTATING SEALS (72-50-33,01-010)

      to stage 7 turbine disk

      ENGINE-LP TURBINE DISCS (72-50-31,01-010)

      Disk dia

      486.2

      486.1

      Intf

      0.6

      Intf

      0.65

      Air seal dia

      485.7

      485.6

      0.4

      0.30

    3. SUBTASK 72-50-30-220-055-C00 Make Sure that the Fits and Clearances between the Stage 7 Disk and the Stage 7 Air Seal are in the Limits given at Location 3664 (SBE 70-0707, SBE 72-0003 and SBE 72-0138)

    1. Refer to Figure.

    2. SBE 72-0138: Rotor and stator assembly introduce new LP turbine blades and vanes

    3. Calculate the clearance at location 3664.

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

      NEW PART

      DIMENSIONS

      WORN PART

      DIMENSIONS

      REJECT IF

      PART IDENT

      Size

      Clearance

      (Non-select)

      MORE THAN

      LOCATION 3664

      Stage 7 air seal ENGINE-LP TURBINE ROTATING SEALS (72-50-33,01-010)

      to stage 7 turbine disk

      ENGINE-LP TURBINE DISCS (72-50-31,01-010)

      Disk dia

      19.1417

      19.1378

      Intf

      0.0236

      Intf

      0.0255

      Air seal dia

      19.1221

      19.1181

      0.0157

      0.0119

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

      NEW PART

      DIMENSIONS

      WORN PART

      DIMENSIONS

      REJECT IF

      PART IDENT

      Size

      Clearance

      (Non-select)

      MORE THAN

      LOCATION 3664

      Stage 7 air seal ENGINE-LP TURBINE ROTATING SEALS (72-50-33,01-010)

      to stage 7 turbine disk

      ENGINE-LP TURBINE DISCS (72-50-31,01-010)

      Disk dia

      486.2

      486.1

      Intf

      0.6

      Intf

      0.65

      Air seal dia

      485.7

      485.6

      0.4

      0.30

    4. SUBTASK 72-50-30-440-091 Calibrate the Moment Weight Equipment

      NOTE

      To get constantly correct results during the moment weight of the LP turbine blades obey the following procedures Step to Step.

    1. Refer to Figure.

    2. Protect the moment weight equipment for environmental effect.

    3. Install the moment weight equipment on a surface plate which is free from vibrations.

    4. Do not change the adjustment of the hydraulic stabilizer at the moment weight equipment.

    5. Make sure that during the moment weight of the blades no tension or load will be applied to the moment weight equipment.

    6. Balance the moment weight equipment with the adjusting screw and the spirit level.

    7. Install the blade distribution system to the moment weight equipment.

    8. Install the IAE 1M14019 Mounting adapter 1 off with the four screws on to the mounting flange of the moment weight equipment.

    9. Install the IAE 1M14015 Blade holder 1 off with the four screws on to the mounting adapter.

    10. Put the required weights from the weight set on to the counter weight scale. Set the moment weight equipment in accordance with the manufacturers instructions to zero. For fine adjustment use the movable weight at the moment weight equipment.

    5. SUBTASK 72-50-30-440-092 Weigh the Stage 7 Turbine Blades

    1. Refer to Figure.

    2. Before you weigh the stage 7 turbine blades, examine if a unbalance value is engraved on the stage 7 turbine disk. Refer to Figure. If there is a unbalanced value engraved on the disk, use this value on the disk for technical data to blade distribution in Step.

    3. Turn on the installed blade distribution system.

    4. Use the blade distribution diskette and put it in to the computer.

    5. Make the input for all required technical data to do blade distribution in accordance with the computer manual in to the blade distribution system.

    6. Put a 10.582 oz (300 g) weight from the weight set on the counter weight scale.

    7. Identify the stage 7 turbine blades with number one to 89. Use CoMat 02-129 MARKER.

    8. Install the stage 7 turbine blade with number one on to the blade holder.

    9. After the blade distribution system has read the moment weight of the blade, remove the blade from the blade holder. Put the blade in to a storage box.

    10. Repeat Step and Step until all stage 7 turbine blade moment weights are specified.

    11. Operate the blade distribution system to get a blade distribution protocol for the stage 7 turbine blades.

    12. Remove the weights from the counter weight scale.

    13. Remove the blade holder and the radius adapter from the mounting adapter.

    6. SUBTASK 72-50-30-440-093 Install the Stage 7 Turbine Blades to the Stage 7 Turbine Disk

    1. Refer to Figure and Figure.

      NOTE

      1. The IAE 1M14153 Assy/disassy stand 1 off must only be used for stage 7 turbine disk with P/N 3A0717.

      2. Make sure that you use the correct locating ring and support ring of the IAE 1M14153 Assy/disassy stand 1 off for the stage 7 disk.

    2. Put the stage 7 turbine disk on the assy/disassy stand, turbine disk front flange upwards.

      NOTE

      1. The IAE 1M14154 Assy/disassy stand 1 off must only be used for stage 7 turbine disk with P/N 3A2514.

      2. Make sure that you use the correct locating ring and support ring of the IAE 1M14154 Assy/disassy stand 1 off for the stage 7 disk.

    3. Put the stage 7 turbine disk on the assy/disassy stand, turbine disk front flange upwards.

      NOTE

      The turbine blade identification number is the same as the blade identification number at the blade distribution protocol.

    4. Identify the disk slot with the disk serial number. The serial number is vibrograved on the front face of the disk. The groove number one is the first groove at the left side of the serial number. Make a mark to the number one. Use CoMat 02-129 MARKER.

    5. Insert the first stage 7 turbine blade in accordance with the blade distribution protocol in to the groove number one.

    6. Insert the remaining turbine blades in accordance with the blade distribution protocol. Work in a counterclockwise direction look to the front side of the disk and insert the blades helical in to the grooves.

    7. Lightly hit the blades at the blade roots. Operate stepwise and in counter clockwise direction to engage the blades. Move stepwise the support of the assy/disassy stand upwards. Use the IAE 1M14079 Plastic wedge 1 off and a soft headed mallet.

    8. Repeat Step until all the blades are fully engaged in to the grooves of the disk. Make sure that the hook from each turbine blade root is in contact with the turbine disk front face.

    9. Inspect the gap at the stage 7 turbine blade inner platforms. Use a torch light. If you can not see a gap, use a feeler gage to measure the correct gap (minimum thickness 0.00118 in. (0.03 mm)).

    7. SUBTASK 72-50-30-440-094 Install the Clamping Ring on to the Stage 7 Turbine Disk

    1. Refer to Figure.

    2. Install the two halves of the IAE 1M14155 Clamping ring 1 off to the stage 7 turbine disk.

    3. Connect the two halves with the single acting ball lock pin.

    4. Attach the clamping ring with the hand knob.

    5. Tighten the hand knob.

    8. SUBTASK 72-50-30-440-095 Install the Stage 7 Turbine Disk on to the Balancing Machine

    1. Refer to Figure.

    2. Use hoist equipment. Lower the balancing base plate on rack pallet. Remove hoist equipment.

      NOTE

      1. The balancing fixture sleeve is used to safety the LP turbine rotor assembly in radial position. This is achieved when the balancing fixture disk is pulled at the inner diameter from the balancing base plate. The caused increase of the balancing fixture disk goes to a small diameter reduction at the abutment face to the LPT rotor disk front snap diameter. Correct adjustment of the adjusting nut, part of the balancing fixture sleeve prevents overstressing.

      2. Do not tighten the balancing fixture sleeve bolt at this moment.

    3. Remove the set screw on the balancing baseplate. Install the IAE 1M14026 Balancing fixture sleeve 1 off to the IAE 1M14020 Balancing base plate 1 off. Install the adjusting nut and the counter nut. Make sure that the set dimension of the adjusting nut, part of the balancing fixture sleeve is correct adjusted.

    4. Use hoist equipment. Install the balancing base plate with three bolts to the balancing machine. Align the TOP marks. Install the three bolts. Tighten the bolts.

    5. Use hoist equipment. Install the IAE 1M14025 Balancing fixture disk 1 off above the balancing fixture sleeve on to the balancing base plate. Align the TOP marks.

    6. Align the installation groove of the balancing fixture sleeve with the dowel pin of the balancing fixture disk.

    7. Attach the balancing fixture disk with the 12 screws to the balancing base plate. Tighten the screws.

    8. Move the three slide blocks, part of the balancing fixture disk in the inner position.

    9. Install the IAE 1M14156 Lifting fixture 1 off to hoist equipment.

    10. Attach the lifting fixture to the IAE 1M14155 Clamping ring 1 off. Lift the stage 7 turbine disk carefully above the installed balancing tool assembly. Turn the stage 7 turbine disk front flange down. Lower it carefully on to the installed balancing fixture disk.

    11. Align the serial number (TOP mark of the turbine disk) to the TOP mark of the balancing fixture disk.

      NOTE

      Do not apply too much force to the stage 7 turbine disk.

    12. Make sure that the three dowel pins of the balancing fixture disk are correctly engaged in to the turbine disk bolt holes.

    13. Tighten the bolt of the balancing fixture sleeve until the adjusting nut touches the balancing base plate.

    14. Move the three slide blocks, part of the balancing fixture disk in the outer position.

    9. SUBTASK 72-50-30-440-096 Remove the Clamping Ring from the Stage 7 Turbine Disk

    1. Refer to Figure.

    2. Remove the lifting fixture and the hoist equipment from the clamping ring.

    3. Loosen the hand knob and disconnect the single acting ball lock pin at the clamping ring.

    4. Remove the two halves of the clamping ring from the stage 7 turbine disk.

    10. SUBTASK 72-50-30-440-097 Balance the Stage 7 Turbine Disk

    1. Make sure that all tools are correctly installed on to the balancing machine.

    2. Adjust the balance radius for the stage 7 turbine disk 13.70 in. (348.0 mm) at the balancing machine.

      NOTE

      The direction of the revolution on the balancing machine must be in clockwise direction.

    3. Do a static unbalance check of the stage 7 turbine disk at 900 rpm.

    4. Install the IAE 1M14155 Clamping ring 1 off on to the stage 7 turbine disk. Refer to Step.

    5. Install the IAE 1M14156 Lifting fixture 1 off to the clamping ring. Use hoist equipment.

    6. Move the three slide blocks of the balancing fixture disk in the inner position.

    7. Loosen the bolt of the balancing fixture sleeve.

    8. Make sure that the stage 7 turbine disk is free from the tool assembly.

    9. Lift the stage 7 turbine disk carefully above of the tool assembly. Lower the stage 7 turbine disk and install it 180 degrees opposite of the balance position in to the tool assembly.

    10. Remove the lifting fixture from the clamping ring. Remove the clamping ring. Refer to Step.

    11. Tighten the bolt of the balancing fixture sleeve.

    12. Move the slide blocks of the balancing fixture disk in the outer position.

    13. Repeat Step.

      14. Remaining unbalance must not be more than 1.0 ozin (720 gmm). If the unbalance is within the limits, continue with Step. If not, correct the unbalance by blade selection as follows:

      1. Use CoMat 02-129 MARKER to mark the unbalance and the position on the blades.

      2. Release the stage 7 turbine disk from the balancing machine. Refer to Step through Step.

      3. Lift the stage 7 turbine disk carefully from the balancing machine and put it on the assy/disassy stand, front flange upwards.

      4. Remove the lifting fixture, the hoist equipment and the clamping ring.

      5. Lightly hit the blades at the blade roots. Operate stepwise and in clockwise direction to disengage the blades. Use the IAE 1M14079 Plastic wedge 1 off and soft headed mallet.

      6. Change the blades marked before with the blades located 180 degrees on the opposite side of the disk.

      7. Insert the changed blades in to the disk grooves. Refer to Step through Step. Write the changed blades down to the blade distribution protocol.

      8. Install the clamping ring to the stage 7 turbine disk. Refer to Step. Remove the quick acting knob and the bar.

      9. Install the stage 7 turbine disk to the balancing machine. Refer to Step.

      10. Remove the clamping ring. Refer to Step.

      11. Repeat Step through Step.

    15. Write the unbalance down to the stage 7 turbine disk blade distribution protocol.

    11. SUBTASK 72-50-30-440-098 Remove the Stage 7 Turbine Disk from the Balancing Machine

    1. Move the slide blocks of the balancing fixture disk in the inner position.

    2. Remove the identification numbers from the turbine blades and the mark on the disk groove number one. Use CoMat 02-069 DISPOSABLE CLEANING TISSUES or clean cloth or clean cloth and CoMat 01-031 ACETONE (CH3)2CO.

    3. Loosen the bolt of the balancing fixture sleeve.

    4. Install the IAE 1M14155 Clamping ring 1 off to the stage 7 turbine disk. Refer to Step.

    5. Install the IAE 1M14156 Lifting fixture 1 off to the clamping ring. Use hoist equipment.

    6. Make sure that the stage 7 turbine disk is free from the tool assembly. Lift the turbine disk. Turn the turbine disk front flange in the upper position. Lower the turbine disk carefully on rack pallet.

    12. SUBTASK 72-50-30-440-099 Remove the Tools from the Balancing Machine

    1. Refer to Figure.

    2. Remove the 12 screws which attach the balancing fixture disk at the balancing base plate.

    3. Remove the balancing fixture disk from the balancing base plate.

    4. Use hoist equipment. Remove the three bolts which attach the balancing base plate to the balancing machine. Remove the balancing base plate from the balancing machine.

    5. Use hoist equipment. Remove the counter nut and the adjusting nut from the balancing fixture sleeve. Remove the balancing fixture sleeve from the balancing base plate. Install the set screw, part of the balancing base plate, to the base plate.

    13. SUBTASK 72-50-30-440-100 Install the Stage 7 Air Seal to the Stage 7 Turbine Disk

    1. Refer to Figure.

    2. Lift the stage 7 turbine disk above the IAE 1M14030 Assembly trolley 1 off. Use the IAE 1M14156 Lifting fixture 1 off with hoist equipment.

    3. Turn the turbine disk, front flange in the upper position. Lower the turbine disk on to the assembly trolley.

    4. Remove the lifting fixture and the hoist equipment.

    5. Remove the clamping ring from the stage 7 turbine disk. Refer to Step.

    6. Install the IAE 1M14132 Guide pin 1 off in to a bolt hole of the stage 7 turbine front flange. Safety the guide pin with the IAE 1M14091 Position retainer 1 off.

    7. Put the stage 7 air seal in to an oven.

    8. CAUTION

      DO NOT EXCEED MAXIMUM TEMPERATURE OF 464 DEG F (240 DEG C) OTHERWISE TURBINE SEALS CAN BE DAMAGED.

      Increase the temperature of the seal until a differential temperature to the ambient temperature of 180 deg F (100 deg C) is reached.

    9. WARNING

      USE PROTECTIVE GLOVES.

      NOTE

      1. The high point of the parts are identified by the delta symbol in a circle.

      2. The turbine disk stage 7 and the air seal stage 7 must be assembled so that the high points of the parts are 180 degrees apart.

      If the stage 7 air seal has the correct temperature remove it from the oven.

    10. Move the stage 7 air seal above the stage 7 turbine disk.

    11. Install the stage 7 air seal and the stage 7 turbine disk.

    12. CAUTION

      HOLD THE BOLTS IN THEIR POSITION WHEN YOU INSTALL THE NUTS ON TO THE BOLTS. DO NOT TURN THE BOLTS OR MAKE TO-AND-FROM MOVEMENTS. THE DISK-/INNER AIR SEAL FLANGES AND/OR THE BOLTS CAN BE DAMAGED BY SCORES.

      Install six work bolts and work nuts to safety the air seal on the disk. Tighten the nuts.

    13. Remove the position retainer and the guide pin from the stage 7 turbine disk.

    14. Let the temperature of all parts decrease to room temperature. Install the IAE 1M14155 Clamping ring 1 off to the stage 7 turbine disk. Refer to Step.

    15. Use CoMat 02-129 MARKER and mark a dash in a circle on the disk hub at the caused high point location at the stage 7 turbine disk hub.

    16. Install the IAE 1M14156 Lifting fixture 1 off to the installed clamping ring. Use hoist equipment.

    17. Lift the assembled stage 7 turbine disk from the assembly trolley. Lower it on to rack pallet or in to the rack pallet, air seal in the upper position. Remove the mounting plate from the assembly trolley.

    18. Remove the lifting fixture and the hoist equipment from the clamping ring.

    19. Remove the clamping ring. Refer to Step.

    14. Figure: Pre SBE 72-0138: The stage 7 Turbine Disk and the Stage 7 Air Seal - Fits and Clearances

    Sheet 1

    Legend
    Pre SBE 72-0138: The stage 7 Turbine Disk and the Stage 7 Air Seal - Fits and Clearances

    Sheet 1

    Close

    Figure: SBE 72-0138: The Stage 7 Turbine Disk and the Stage 7 Air Seal - Fits and Clearances

    Sheet 2

    Legend
    SBE 72-0138: The Stage 7 Turbine Disk and the Stage 7 Air Seal - Fits and Clearances

    Sheet 2

    Close

    Figure: Calibrate the Moment Weight Equipment

    Calibrate the Moment Weight Equipment

    Figure: Disk-marking Areas of the Stage 7 Turbine Disk

    Disk-marking Areas of the Stage 7 Turbine Disk

    Figure: Install the Stage 7 Turbine Blades

    Install the Stage 7 Turbine Blades

    Figure: Turn the Stage 7 Turbine Disk with the Clamping Ring

    Turn the Stage 7 Turbine Disk with the Clamping Ring

    Figure: Install the Stage 7 Turbine Disk to the Balancing Tool Assembly

    Install the Stage 7 Turbine Disk to the Balancing Tool Assembly

    Figure: Install the Stage 7 Air Seal to the Stage 7 Turbine Disk

    Install the Stage 7 Air Seal to the Stage 7 Turbine Disk

    Figure: Install the Stage 7 Turbine Blades to the Stage 7 Turbine Disk with P/N 3A0717

    Install the Stage 7 Turbine Blades to the Stage 7 Turbine Disk with P/N 3A0717

    Figure: Install the Stage 7 Turbine Blades to the Stage 7 Turbine Disk with P/N 3A2514

    Install the Stage 7 Turbine Blades to the Stage 7 Turbine Disk with P/N 3A2514

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised tool nomenclature. Revised consumable nomenclature. Added link. Revised procedural step. (Editorial)

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:33591
Enterprise Name:KIMBERLY-CLARK CORP
BU Name:KIMBERLY-CLARK CORP
Street:1400 HOLCOMB BRIDGE ROAD
City:ROSWELL
State:GA
Zip Code:30076-2199
Country:USA
Phone Number:1-215-888-0040
Fax Number:1-920-380-1303
Internet:www.kimberley-clark.com
Manufacturer Code:IAE28
Enterprise Name:DELETED
BU Name:DELETED, SEE CAGE CODE C4690
Manufacturer Code:K3504
Enterprise Name:INDESTRUCTIBLE PAINT CO LTD
BU Name:NULL
Street:25 PENTOS DRIVE
City:SPARKHILL
Province:BIRMINGHAM
Zip Code:B11 3TA
Country:GREAT BRITAIN
Phone Number:44-121-7022485
Fax Number:44-121-7784338
Email:sales@indestructible.co.uk
Internet:www.indestructible.co.uk
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:LOCAL
Supply Number:CoMat 01-031
Type:sp01
Supply Short Name:CoMat 01-031 ACETONE (CH3)2CO
Supply Name:CoMat 01-031 ACETONE (CH3)2CO
Specification Groups:
Doc NumberType
OMAT: 150 (RR REF)COMMERCIAL GRADE O-A-51
PMC 9008 (PW REF)COMMERCIAL GRADE O-A-51
JCR-041 (JAEC REF)COMMERCIAL GRADE O-A-51
MTH 169 (98%) (MTU REF)COMMERCIAL GRADE O-A-51
Suppliers:
ManufacturerRemarks
LOCAL
K6835
81348
K3504
U1185
24853
70657
Manufacturer Code:33591
Supply Number:CoMat 02-069
Type:sp01
Supply Short Name:CoMat 02-069 DISPOSABLE CLEANING TISSUES
Supply Name:CoMat 02-069 DISPOSABLE CLEANING TISSUES
Specification Groups:
Doc NumberType
OMAT: 2/67WORKHORSE / KIMWIPES NO. 7105
Suppliers:
ManufacturerRemarks
33591
IE319
IE320
IE321
K4182
LOCAL
Manufacturer Code:IAE28
Supply Number:CoMat 02-129
Type:sp01
Supply Short Name:CoMat 02-129 MARKER
Supply Name:CoMat 02-129 MARKER
Specification Groups:
Doc NumberType
MTH 557FELT PEN
MTH 558FELT PEN
Suppliers:
ManufacturerRemarks
IAE28
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:LOCAL
Tool Number:Balancing machine
Tool Name:Balancing machine
Manufacturer Code:LOCAL
Tool Number:Blade distribution system
Tool Name:Blade distribution system
Manufacturer Code:LOCAL
Tool Number:Feeler gage
Tool Name:Feeler gage
Manufacturer Code:0AM53
Tool Number:IAE 1M14015
Tool Name:IAE 1M14015 Blade holder
Manufacturer Code:0AM53
Tool Number:IAE 1M14019
Tool Name:IAE 1M14019 Mounting adapter
Manufacturer Code:0AM53
Tool Number:IAE 1M14020
Tool Name:IAE 1M14020 Balancing base plate
Manufacturer Code:0AM53
Tool Number:IAE 1M14025
Tool Name:IAE 1M14025 Balancing fixture disk
Manufacturer Code:0AM53
Tool Number:IAE 1M14026
Tool Name:IAE 1M14026 Balancing fixture sleeve
Manufacturer Code:0AM53
Tool Number:IAE 1M14030
Tool Name:IAE 1M14030 Assembly trolley
Manufacturer Code:0AM53
Tool Number:IAE 1M14079
Tool Name:IAE 1M14079 Plastic wedge
Manufacturer Code:0AM53
Tool Number:IAE 1M14091
Tool Name:IAE 1M14091 Position retainer
Manufacturer Code:0AM53
Tool Number:IAE 1M14132
Tool Name:IAE 1M14132 Guide pin
Manufacturer Code:0AM53
Tool Number:IAE 1M14153
Tool Name:IAE 1M14153 Assy/disassy stand
Manufacturer Code:0AM53
Tool Number:IAE 1M14154
Tool Name:IAE 1M14154 Assy/disassy stand
Manufacturer Code:0AM53
Tool Number:IAE 1M14155
Tool Name:IAE 1M14155 Clamping ring
Manufacturer Code:0AM53
Tool Number:IAE 1M14156
Tool Name:IAE 1M14156 Lifting fixture
Manufacturer Code:LOCAL
Tool Number:Mallet
Tool Name:Mallet
Manufacturer Code:LOCAL
Tool Number:Moment weighing equipment
Tool Name:Moment weighing equipment
Manufacturer Code:LOCAL
Tool Number:Oven
Tool Name:Oven
Manufacturer Code:LOCAL
Tool Number:Rack pallet
Tool Name:Rack pallet
Manufacturer Code:LOCAL
Tool Number:Torch light
Tool Name:Torch light