DMC:V2500-A0-72-41-1000-00C-530A-B|Issue No:007|Issue Date:2020-02-01

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

All

Common Information

TASK 72-41-10-040-001-B00 HPC Rotor Assembly - Disassemble The Rotor Assembly, Disassembly-001

General

This TASK gives the procedure to disassemble the HP compressor rotor assembly. It includes the procedure to measure the seal and stator path diameters and the blade lengths before removal.

Make sure the tip check and seal check equipment has been calibrated before you use it. Refer to the Illustrated Tools and Equipment Manual, Pub ref ITE-V2500-1IA.

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.

Apply the approved penetrating oil before the removal of threaded parts and parts with an interference fit. Let the parts soak before removal. For the approved oils and procedures, refer to SPM TASK 70-64-00-640-501.

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

Name	Manufacturer	Part Number / Identification	Quantity
Digital read out equipment	LOCAL	Digital read out equipment
Grinding Machine	LOCAL	Grinding Machine
Snap-on TM70B wrench	LOCAL	Snap-on TM70B wrench
Snap-on TMX60 extension	LOCAL	Snap-on TMX60 extension
IAE 1P18865 Immobilizer tool	LOCAL	IAE 1P18865
IAE 1P18865-1 Retention Blocks	LOCAL	IAE 1P18865-1
IAE 1P18865-2 Retention Block	LOCAL	IAE 1P18865-2
IAE 1F10026 Hydraulic hand pump	0AM53	IAE 1F10026	1
IAE 1R18020 Build stand	0AM53	IAE 1R18020	1
IAE 1R18021 Support ring	0AM53	IAE 1R18021	1
IAE 1R18024 Geared indexing spanner	0AM53	IAE 1R18024	1
IAE 1R18025 Turnover stand adapter	0AM53	IAE 1R18025	1
IAE 1R18029 Blanking tool	0AM53	IAE 1R18029	1
IAE 1R18059 Trolley	0AM53	IAE 1R18059	1
IAE 1R18061 Rail	0AM53	IAE 1R18061	2
IAE 1R18065 Lifter	0AM53	IAE 1R18065	1
IAE 1R18067 Extractor	0AM53	IAE 1R18067	1
IAE 1R18079 Drift	0AM53	IAE 1R18079	1
IAE 1R18080 Drift	0AM53	IAE 1R18080	1
IAE 1R18081 Beam sling	0AM53	IAE 1R18081	1
IAE 1R18089 Lifting adapter	0AM53	IAE 1R18089	1
IAE 1R18090 Safety support stand	0AM53	IAE 1R18090	1
IAE 1R18091 Support stand	0AM53	IAE 1R18091	1
IAE 1R18092 Support tool	0AM53	IAE 1R18092	1
IAE 1R18095 Universal slinging adapter	0AM53	IAE 1R18095	2
IAE 1R18097 Drift	0AM53	IAE 1R18097	1
IAE 1R18322 Turnover stand	0AM53	IAE 1R18322	1
IAE 1R18400 Protection sleeve	0AM53	IAE 1R18400	1
IAE 1R18441 Lifting adapter	0AM53	IAE 1R18441	1
IAE 1R18443 Puller	0AM53	IAE 1R18443	1
IAE 1R18451 Tip check fixture	0AM53	IAE 1R18451	1
IAE 1R18452 Bearing housing (rear)	0AM53	IAE 1R18452	1
IAE 1R18453 Bearing housing (front)	0AM53	IAE 1R18453	1
IAE 1R18454 Location block	0AM53	IAE 1R18454	1
IAE 1R18455 Location block	0AM53	IAE 1R18455	2
IAE 1R18458 Brake strap	0AM53	IAE 1R18458	1
IAE 1R18459 Axial setting gage	0AM53	IAE 1R18459	1
IAE 1R18460 Transducer carrier	0AM53	IAE 1R18460	1
IAE 1R18461 Transducer carrier	0AM53	IAE 1R18461	1
IAE 1R18462 Transducer carrier	0AM53	IAE 1R18462	1
IAE 1R18463 Transducer carrier	0AM53	IAE 1R18463	1
IAE 1R18464 Transducer carrier	0AM53	IAE 1R18464	1
IAE 1R18466 Thruster plate	0AM53	IAE 1R18466	1
IAE 1R18467 Setting block	0AM53	IAE 1R18467	1
IAE 1R18590 Socket end	0AM53	IAE 1R18590	1
IAE 1R18691 Lifting fixture	0AM53	IAE 1R18691	1
IAE 1R18692 Indexing ring	0AM53	IAE 1R18692	1
IAE 1R18708 Protection cover	0AM53	IAE 1R18708	1
IAE 1R18714 Checking beam	0AM53	IAE 1R18714	1
IAE 1R18776 Spacer	0AM53	IAE 1R18776
IAE 1R18794 Setting gage	0AM53	IAE 1R18794	1
IAE 1R18795 Transducer carrier	0AM53	IAE 1R18795	1
IAE 1R19006 Extractor	0AM53	IAE 1R19006	1
IAE 1R19008 Puller	0AM53	IAE 1R19008	1
Hydraulic jack	0AM53	ENERPAC 102	1
IAE 1R18911 Drill	0AM53	IAE 1R18911	1
IAE 1R18914 Setting gage	0AM53	IAE 1R18914	1
IAE 1R18913 Setting gage	0AM53	IAE 1R18913	1
IAE 1R18912 Setting gage	0AM53	IAE 1R18912	1
IAE 1R18201 Torque spanner	0AM53	IAE 1R18201	1
IAE 1R18204 Location ring	0AM53	IAE 1R18204
IAE 1R18673 Dummy stub shaft	0AM53	IAE 1R18673
IAE 18914 Setting gage	0AM53	IAE 18914
IAE 18913 Setting gage	0AM53	IAE 18913

Consumables, Materials and Expendables

Name	Manufacturer	Part Number / Identification
CoMat 02-121 TEMPORARY MARKER PENCIL/CRAYON	IE304	CoMat 02-121
CoMat 02-122 TEMPORARY MARKER PENCIL/CRAYON	K6835	CoMat 02-122
DELETED	LOCAL	DELETED

Spares

NONE

Safety Requirements

NONE

Procedure

1. Refer to Figure, Figure, Figure and Figure.
2. Install IAE 1R18454 Location block 1 off on to the rear pedestal of IAE 1R18451 Tip check fixture 1 off and safety.
3. Install IAE 1R18455 Location block 1 off on to the front pedestal of the tip check fixture and safety.
4. Install the IAE 1R18453 Bearing housing (front) 1 off and safety with the two keep plates.
5. Install the IAE 1R18452 Bearing housing (rear) 1 off and safety with the two keep plates.
6. Turn the quarter turn screw, in the front bracket, 90 degrees and move the front bracket down on to the stop plate.
7. Do step E. again for the rear bracket.
1. Refer to Figure, Figure, Figure, Figure, Figure, Figure, Figure and Figure.
2. 1. Put the cover over the compressor shaft and move the cover down the shaft.
  2. Engage the cover over the rotating air seal. Make sure the cover is correctly installed.
  3. Attach the O-ring on to the O-ring location to safety the cover.
3. Install the IAE 1R18089 Lifting adapter 1 off on to the end of the compressor shaft and tighten.
4. 1. Lift pin E and put the adapter end of the tool in to the lifting adapter. Turn the tool to engage it and lower the pin E.
  2. Install the lifting end of the tool in to the adapter end. Install the trunnion pin through both parts of the tool and tighten it.
  3. Tighten the locknut on to the lifting adapter attach a hoist to the lift eye.
5. CAUTION
  YOU MUST NOT LET THE COMPRESSOR ROTOR ASSEMBLY HIT THE BUILD STAND.
  Remove the compressor rotor assembly from the build stand.
6. 1. Install the IAE 1R18091 Support stand 1 off on to IAE 1R18090 Safety support stand 1 off.
  2. Install the compressor rotor assembly on to the safety support stand.
  3. Attach the universal slinging adapter on to the dummy stub shaft. Refer to step C.(1) thru C.(3).
7. Lift the compressor rotor assembly off the safety support stand.
8. CAUTION
  YOU MUST NOT LET THE COMPRESSOR ROTOR ASSEMBLY HIT THE TIP CHECK FIXTURE.
  Install the compressor rotor assembly in to the IAE 1R18451 Tip check fixture 1 off. Make sure the dummy stub shaft is correctly located in the front bearing housing.
9. Remove the universal slinging adapter and the lifting adapter from the compressor shaft and the universal slinging adapter from the dummy stub shaft.
10. Install the IAE 1R18466 Thruster plate 1 off in to the compressor shaft.
11. Adjust the handwheels on the front and rear brackets to make sure the thruster brackets are fully retracted.
12. Lift the front and rear brackets up in to position and safety with the quarter turn screws.
1. Refer to Figure and Figure.
2. Install the IAE 1R18459 Axial setting gage 1 off on to the front pedestal.
3. With IAE 1R18467 Setting block 1 off adjust the IAE 1R18460 Transducer carrier 1 off to the applicable zero setting on the digital read out equipment.
4. Install the transducer in to the axial setting gage and hand tighten the knurled nut.
5. With the front and rear handwheels, adjust the position of the compressor rotor assembly in the fixture until the dummy stub shaft front face causes the transducer plunger to operate. Continue to adjust the position of the rotor until the transducer gives the initial zero reading.
6. Remove the transducer carrier and the axial setting gage.
7. 1. Locate the two dowels and safety the beam in position with the two bolts and washers.
8. Install the IAE 1R18458 Brake strap 1 off on to the front pedestal and adjust.
1. Refer to Figure and Figure.
2. With standard workshop equipment measure the swash at face A; the swash must not be more than 0.0051 in. (0.130 mm). Measure the concentricity at diameter B; the concentricity must not be more than 0.0031 in. (0.080 mm).
1. Refer to Figure.
2. 1. Connect the transducer carrier to the digital read out equipment.
  2. Loosen the two setscrews that safety the transducer in to the rear transducer block.
  3. Install the transducer carrier on to IAE 1R18794 Setting gage 1 off.
    Align the transducer with the correct setting block and at the same time locate the two location plates of the transducer carrier in to the location slot in the setting gage.
    Make sure that the transducer carrier rear anvil touches the front stop on the setting gage.
  4. Adjust the position of the transducer in the rear transducer block until the roller touches the setting block and the transducer is approximately in the middle of its range of movement.
  5. Tighten the two setscrews to safety the transducer in position in the rear transducer block.
  6. Set the display of the resolver angle position unit to read zero and make sure that a positive (+) reading is given when the plunger moves in to the transducer.
  7. Remove the transducer carrier from the setting gage.

SUBTASK 72-41-10-040-088 Measure and Calculate the Stage 3 to 4 Seal Fin Diameters at Location 1001

Refer to Figure and Figure.
1. 1. Carefully locate the transducer roller on the first seal fin and at the same time locate the transducer carriers two location plates in to the slot in the seal check beam.
  2. Move the transducer carrier in the location slot until the rear anvil touches the threaded stop on the seal check beam.
2. Turn the HP compressor rotor smoothly in a clockwise direction.
3. Write down the minimum and maximum values given on the transducer display. Also record the values as a negative or positive reading.
4. Carefully move the front transducer block until the transducer roller is located on the second seal fin.
5. Do steps A.(2) and A.(3) again.
6. Carefully move the front transducer block until the transducer roller is located on the third seal fin.
7. Do steps A.(2) and A.(3) again.
8. Carefully move the front transducer block until the transducer roller is located on the fourth seal fin.
9. Do steps A.(2) and A.(3) again.
10. Remove the transducer carrier from the seal check beam.

Calculate the stage 3 to 4 seal fin diameters at location 1001.

Calculate the diameter of each of the four seal fins as follows:

Seal fin diameter = 2 (A+B)

where, A = Tool setting radius = 5.1646 in. (131.18 mm)

B = Transducer reading

Example 1, where B = -0.046 in.

Seal fin diameter = 2 (5.1646 + -0.046)

= 10.237 in.

Example 2, where B = 0.046 in.

Seal fin diameter = 2 (5.1646 + 0.046)

= 10.421 in.

Write down the calculated minimum and maximum diameters for each of the four seal fins. This data is to be used in the INSPECTION/CHECK of the 3 to 8 compressor disks. Refer to TASK 72-41-11-200-000 (INSPECTION/CHECK-000).

1. Refer to Figure and Figure.
2. 1. Do the procedure given in Step.
3. 1. Install the transducer carrier in the correct position on the seal check beam.
    Carefully locate the transducer roller on to the seal fin at Location 1002 and at the same time locate the transducer carriers two location plates in to the slot in the seal check beam.
    Move the transducer carrier in the location slot until the rear anvil touches the threaded stop on the seal check beam.
  2. Turn the HP compressor rotor smoothly in a clockwise direction.
  3. Write down the minimum and maximum values given on the transducer display. Also record the values as a negative or positive reading.
4. 1. Calculate the diameter of the seal fin as follows:
    Seal fin diameter = 2 (A + B)
    where A, = Tool setting radius = 5.9362 in. (150.78 mm)
    B = Transducer reading
  2. Refer to Step for calculation examples.
  3. Write down the calculated minimum and maximum diameter for the seal fin. This data is to be used in the INSPECTION/CHECK of the 3 to 8 compressor disks. Refer to TASK 72-41-11-200-000 (INSPECTION/CHECK-000).
5. 1. Remove IAE 1R18462 Transducer carrier from the seal check beam.
  2. Install the transducer carrier in the correct position on the seal check beam.
    Carefully locate the transducer roller on to the first seal fin at location 1003 and at the same time locate the transducer carriers two location plates in to the slot in the seal check beam.
    Move the transducer carrier in the location slot until the rear anvil touches the threaded stop on the seal check beam.
  3. Turn the HP compressor rotor smoothly in a clockwise direction.
  4. Write down the minimum and maximum values given on the transducer display. Also record the values as a negative or positive reading.
  5. Carefully move the front transducer block until the transducer roller is located on the second seal fin.
  6. Do steps D.(3) and D.(4) again.
  7. Remove the transducer carrier from the seal check beam.
6. 1. Calculate the diameter of each of the seal fins as follows:
    Seal fin diameter = 2 (A + B)
    where A, = Tool setting radius = 6.1252 in. (155.58 mm)
    B = Transducer reading
  2. Refer to Step for calculation examples.
  3. Write down the calculated minimum and maximum diameters for each of the two seal fins. This data is to be used in the INSPECTION/CHECK of the 3 to 8 compressor disks. Refer to TASK 72-41-11-200-000 (INSPECTION/CHECK-000).
1. Refer to Figure and Figure.
2. 1. Do the procedure given in Step.
3. 1. Install the transducer carrier in the correct position on the seal check beam.
    Carefully locate the transducer roller on to the first seal fin and at the same time locate the transducer carriers two location plates in to the slot in the seal check beam.
    Move the transducer carrier in the location slot until the rear anvil touches the threaded stop on the seal check beam.
  2. Turn the HP compressor rotor smoothly in a clockwise direction.
  3. Write down the minimum and maximum values given on the transducer display. Also record the values as a negative or positive reading.
  4. Carefully move the front transducer block until the transducer roller is located on the second seal fin.
  5. Do steps B.(2) and B.(3) again.
  6. Carefully move the front transducer block until the transducer roller is located on the third seal fin.
  7. Do steps B.(2) and B.(3) again.
  8. Remove the transducer carrier from the seal check beam.
4. 1. Calculate the diameter of each of the seal fins as follows:
    Seal fin diameter = 2 (A + B)
    where A, = Tool setting radius = 6.9382 in. (176.23 mm)
    B = Transducer reading
  2. Refer to Step for calculation examples.
  3. Write down the calculated minimum and maximum diameters for each of the four seal fins. This data is to be used in the INSPECTION/CHECK of the 3 to 8 compressor disks. Refer to TASK 72-41-11-200-000 (INSPECTION/CHECK-000).
1. Refer to Figure and Figure.
2. 1. Do the procedure given in Step.
3. 1. Install the transducer carrier in the correct position on the seal check beam.
    Carefully locate the transducer roller on to the vane path and at the same time locate the transducer carriers two location plates in to the slot in the seal check beam.
    Move the transducer carrier in the location slot until the rear anvil touches the threaded stop on the seal check beam.
  2. Turn the HP compressor rotor smoothly in a clockwise direction.
  3. Write down the minimum and maximum values given on the transducer display. Also record the values as a negative or positive reading.
  4. Remove the transducer carrier from the seal check beam.
4. 1. Do steps A.(1) and B.(1) thru B.(4) to measure the stage 7 to 8 stator vane path diameter.
5. 1. Do steps A.(1) and B.(1) thru B.(4) to measure the stage 8 to 9 stator vanes path diameter.
6. 1. Do steps A.(1) and B.(1) thru B.(4) to measure the stage 9 to 10 stator vane path diameter.
7. 1. Do steps A.(1) and B.(1) thru B.(4) to measure the stage 10 to 11 stator vane path diameter.
8. 1. Do steps A.(1) and B.(1) thru B.(4) to measure the stage 11 to 12 stator vane path diameter.
9. 1. Calculate the diameter of each of the stator vane paths as follows:
    Stator vane path diameter = 2 (A + B)
    where A, = Tool setting radius
    B = Transducer reading
    The tool setting radius values (A) used in the calculations for the different stator vane path diameters are as follows:
    A = 8.6047 in. (218.56 mm) for the stage 6 to 7 vane path (location 1056).
    A = 8.9387 in. (227.044 mm) for the stage 7 to 8 vane path (location 1057).
    A = 9.1530 in. (232.485 mm) for the stage 8 to 9 vane path (location 1058).
    A = 9.2891 in. (235.944 mm) for the stage 9 to 10 vane path (location 1059).
    A = 9.3117 in. (236.516 mm) for the stage 10 to 11 vane path (location 1060).
    A = 9.3147 in. (236.594 mm) for the stage 11 to 12 vane path (location 1061).
    Refer to Step for calculation examples.
  2. Write down the calculated minimum and maximum diameters for each of the stator vane paths. The 6 to 7 and 7 to 8 stator vane path diameters are to be used in the INSPECTION/CHECK of the 3 to 8 compressor disk; refer to TASK 72-41-11-200-000 (INSPECTION/CHECK-000). The 8 to 9, 9 to 10, 10 to 11 and 11 to 12 stator vane path diameters are to be used in the INSPECTION/CHECK of the 9 to 12 compressor disk assembly; refer to TASK 72-41-12-200-000 (INSPECTION/CHECK-000).
1. Refer to Figure and Figure.
2. 1. Do the procedure given in Step.
3. 1. Install the transducer carrier in the correct position on the seal check beam.
    Carefully locate the transducer roller on the first seal fin at location 1401A and at the same time locate the transducer carriers two location plates in to the slot in the seal check beam.
    Move the transducer carrier in the location slot until the rear anvil touches the threaded stop on the seal check beam.
  2. Turn the HP compressor rotor smoothly in a clockwise direction.
  3. Write down the minimum and maximum values given on the transducer display. Also record the values as a negative or positive reading.
  4. Carefully move the front transducer block until the transducer roller is located on the seal fin at location 1401B.
  5. Do steps B.(2) and B.(3) again.
  6. Carefully move the front transducer block until the transducer roller is located on the seal fin at location 1401C.
  7. Do steps B.(2) and B.(3) again.
  8. Carefully move the front transducer block until the transducer roller is located on the seal fin at location 1401D.
  9. Do steps B.(2) and B.(3) again.
  10. Remove the transducer carrier from the seal check beam.
4. 1. Calculate the diameter of each of the seal fins as follows:
    Seal fin diameter = 2 (A + B)
    where A, = Tool setting radius
    B = Transducer reading
    The tool setting radius values (A) used in the calculations for the different rear rotating air seal fin diameter locations are as follows:
    A = 3.4528 in. (87.7 mm) for location 1401A.
    A = 3.5591 in. (90.4 mm) for location 1401B.
    A = 3.6654 in. (93.1 mm) for location 1401C.
    A = 3.7717 in. (95.8 mm) for location 1401D.
    Refer to Step for calculation examples.
  2. Write down the calculated minimum and maximum diameters for each of the seal fins. This data is to be used in the INSPECTION/CHECK of the rear rotating air seal. Refer to TASK 72-41-14-200-000 (INSPECTION/CHECK-000).
1. Refer to Figure, Figure, Figure and Figure.
2. Remove the seal check beam from the tip check fixture.
3. Remove the brake strap from the front pedestal.
4. Remove the front and rear location blocks from the front and rear pedestals.
5. Turn the quarter turn screw in the front and rear brackets, 90 degrees and move the brackets down on to the stop plates.
6. Remove the thruster plate adapter from the compressor shaft.
7. Install the IAE 1R18089 Lifting adapter 1 off and the IAE 1R18095 Universal slinging adapter 2 off. Refer to Step and Figure.
8. Attach a hoist to the compressor rotor and lift the rotor clear of the tip check fixture.
1. Refer to Figure.
2. 1. Move the compressor rotor and put it above the trolley. Make sure the trunnions on the universal slinging adapter (front) are above the trunnion supports.
  2. Lower the rotor until the trunnions engage in the trunnion supports.
3. Remove the hoist.
4. 1. Remove the eight bolts from the trolley rail locations.
  2. Install the rails on to the trolley and safety with the eight bolts.
1. Refer to Figure and Figure.
2. 1. Make sure that the bracket is at the identified position for the center of gravity of the beam sling only.
  2. Attach a hoist to the ring.
  3. Lift the beam sling and put it above the rotor assembly.
  4. Adjust the height of the beam sling until the shackles and screw pins can be attached to the universal sling adapter. Remove the screw pins.
  5. Install the screw pins through the shackles and universal sling adapters; tighten the screw pins.
  6. Set the beam sling to the identified position for the center of gravity of the beam sling and rotor assembly.
3. Carefully lift the HP compressor rotor assembly out of the trolley and install it on to an applicable stand which will permit the grinding machine tools to be installed.
4. 1. Set the beam sling to the identified position for the center of gravity of the beam sling only.
  2. Remove the screw pins from the shackles and disengage the shackles from the universal sling adapters.
  3. Install the screw pins in to the shackles and then lift the beam sling away from the rotor assembly. Put the beam sling on to an applicable surface and remove the hoist.
5. Remove the necessary tools from the HP compressor rotor assembly to permit the grinding machine adapters to be installed. Refer to Figure and Figure.
  NOTE
  The applicable grinding machine adapters are identified by machine type.
6. Install the applicable grinding machine adapters on to the HP compressor rotor assembly to prepare it for installation in to the grinding machine.
  NOTE
  The applicable tools are identified by machine type.
7. Install the applicable tools which are necessary to lift the HP compressor rotor assembly.
8. Carefully lift the HP compressor rotor assembly and install it in to the grinding machine.
9. Safety the headstock and tailstock adapters in position.
10. Remove the tools which were used to lift the HP compressor rotor assembly.
1. Measure the swash and run-out of the HP compressor rotor assembly on the applicable tool surfaces.
2. Make sure the swash and run-out are not more than 0.0012 in. (0.03 mm).
1. Refer to Figure, Figure and Figure.
2. If the HPC rotor is not scheduled to be disassembled and refurbished refer to Special Procedure TASK 72-00-00-200-801 (Special Procedure-001).
  NOTE
  The grinding machine must use a measuring device to measure the blade lengths.
3. Measure the blade lengths and write the results.
4. Use CoMat 02-121 TEMPORARY MARKER PENCIL/CRAYON or CoMat 02-122 TEMPORARY MARKER PENCIL/CRAYON to identify the blades that are too short.
1. Refer to Figure, Figure and Figure.
2. SBE 72-0295: HP compressor blades - introduction of a redesigned stage 4 blade assembly
3. If the HPC rotor is not scheduled to be disassembled and refurbished refer to Special Procedure TASK 72-00-00-200-801 (Special Procedure-001).
  NOTE
  The grinding machine must use a measuring device to measure the blade lengths.
4. Measure the blade lengths and write the results.
5. Use CoMat 02-121 TEMPORARY MARKER PENCIL/CRAYON or CoMat 02-122 TEMPORARY MARKER PENCIL/CRAYON to identify the blades that are too short.
1. Refer to Figure and Figure.
  NOTE
  The necessary tools are identified by machine type.
2. Install the tools which are necessary to lift the HP compressor rotor assembly out of the grinding machine.
3. Attach a hoist to the tools.
4. Remove the bolts which secure the HP compressor rotor assembly to the headstock and tailstock of the grinding machine.
5. Lift the HP compressor rotor assembly out of the grinding machine and put it on to an applicable stand.
6. Remove the hoist and tools which were installed on to the HP compressor rotor assembly for installation in to the grinding machine.
7. Put IAE 1R18708 Protection cover 1 off on to the end of the HP compressor shaft.
8. Install IAE 1R18089 Lifting adapter 1 off to the end of the HP compressor shaft. Tighten the lifting adapter.
9. 1. Lift pin E and put the adapter end of the tool in to the adapter. Turn the tool to engage the locations. Lower pin E.
  2. Install the lifting end of the tool in to the adapter end. Install the trunnion pin through both parts of the tool and tighten it.
  3. Tighten the locknut on to the lifting adapter.
10. 1. Examine the curvic teeth of the dummy stub shaft and the stage 3 disk for contamination and/or high metal. If there is contamination then the curvic teeth must be cleaned. If there is high metal, use a stone to make the surface smooth.
  2. Align the four location dowels in the dummy stub shaft with the holes in the stage 3 disk curvic coupling.
  3. Install the dummy stub shaft on to the curvic coupling and engage the 20 bolts in the dummy stub shaft in to the holes in the stage 3 disk. Lightly tighten the bolts.
  4. Torque all of the bolts. Do these three steps in the sequence shown. Refer to Figure.
    Torque all of the bolts to 18 lbfin (2.034 Nm).
    Torque all of the bolts to 35 lbfin (3.955 Nm).
    Torque all of the bolts to 70 * lbfin (7.900 Nm).
11. 1. Do steps H.(1) thru H.(3) again.
12. Install IAE 1R18081 Beam sling 1 off to the HP compressor rotor assembly. Refer to Step.
13. 1. Lift the compressor rotor assembly and put it above the trolley. Make sure that the trunnions on the universal sling adapters are above the trunnion supports.
  2. Carefully lower the compressor rotor assembly in to the trolley. Make sure that the trunnions on the universal sling adapters engage in the trunnion supports of the trolley.
14. 1. Engage the protection cover over the compressor rotating air seals. Make sure the protection cover is correctly installed on the seals.
  2. Attach the O-ring on to the O-ring location to safety the protection cover.
15. Remove the beam sling from the compressor rotor assembly. Refer to Step.
16. 1. Remove the eight bolts from the trolley rail locations.
  2. Install the rails on to the trolley and safety with the eight bolts.
1. 1. With IAE 1R18590 Socket end 1 off release the two nut and screw lock assemblies.
  2. With IAE 1R18097 Drift 1 off move the blades around the disk until a blade can be removed through the loading slot.
  3. Do step (2) again, to remove each blade and the two nut and screw lock assemblies, until all the blades have been removed.
2. 1. Do steps A.(1) thru A.(3) for each stage of blades.
    NOTE
    To drill out seized blade locknuts use the following tools: IAE 1R18911 Drill 1 off, IAE 18914 Setting gage 1 off (stage 6), IAE 18913 Setting gage 1 off (stage 7) and IAE 1R18912 Setting gage 1 off (stage 8).
3. 1. Remove the damping wires from the disks and do steps A. (1) thru A. (3) to remove the blades.
4. 1. With an applicable tool remove the lockplates from the rear of the stage 3 disk and discard.
  2. With IAE 1R18079 Drift 1 off move the retaining plates around the disk to close up the spaces between them. This will give sufficient space to remove one blade, forwards, from the disk.
  3. Continue to move the retaining plates around in a counterclockwise direction (when viewed from the rear) until the next blade can be removed.
  4. Continue this procedure until sufficient blades have been removed to let you remove one of the retaining plates.
  5. Move the retaining plates, in turn, around the disk until they have all been removed.
  6. Remove the remaining blades in a counterclockwise direction from the stage 3 disk.
5. 1. With an applicable tool remove the lockplates from the front of the stage 4 disk and discard.
  2. With IAE 1R18080 Drift 1 off move the retaining plates around the disk to close up the space between them. This will give sufficient space to remove one blade, forwards, from the disk.
  3. Continue to move the retaining plates around the disk until sufficient blades have been removed to let you remove one of the retaining plates.
  4. Move the retaining plates, in turn, around the disk until they have all been removed.
  5. Remove the remaining blades from the stage 4 disk.
  6. Remove and discard the sealing strips HPC Rotor Blades (72-41-15, 01-520) from all the stage 4 blades.
6. 1. Do steps E.(1) thru E.(5) to remove the retaining plates and the blades from the stage 5 disk.
  2. Remove and discard the sealing strips HPC Rotor Blades (72-41-15, 01-820) from all the stage 5 blades.
1. SBE 72-0300: HP disks and blades - Introduction of revised stage 3 to 8 disk and revised stage 7 and 8 sealing wires.
2. 1. With IAE 1R18590 Socket end 1 off release the two nut and screw lock assemblies.
  2. With IAE 1R18097 Drift 1 off move the blades around the disk until a blade can be removed through the loading slot.
  3. Do step (2) again, to remove each blade and the two nut and screw lock assemblies, until all the blades have been removed.
3. 1. Do steps A.(1) thru A.(3) for each stage of blades.
    NOTE
    To drill out seized blade locknuts use the following tools: IAE 1R18911 Drill 1 off, IAE 18914 Setting gage 1 off (stage 6), IAE 18913 Setting gage 1 off (stage 7) and IAE 1R18912 Setting gage 1 off (stage 8).
4. 1. Remove the sealing wires from the disks and do steps A.(1) thru A.(3) to remove the blades.
5. 1. With an applicable tool remove the lockplates from the rear of the stage 3 disk and discard.
  2. With IAE 1R18079 Drift 1 off move the retaining plates around the disk to close up the spaces between them. This will give sufficient space to remove one blade, forwards, from the disk.
  3. Continue to move the retaining plates around in a counterclockwise direction (when viewed from the rear) until the next blade can be removed.
  4. Continue this procedure until sufficient blades have been removed to let you remove one of the retaining plates.
  5. Move the retaining plates, in turn, around the disk until they have all been removed.
  6. Remove the remaining blades in a counterclockwise direction from the stage 3 disk.
6. 1. With an applicable tool remove the lockplates from the front of the stage 4 disk and discard.
  2. With IAE 1R18080 Drift 1 off move the retaining plates around the disk to close up the space between them. This will give sufficient space to remove one blade, forwards, from the disk.
  3. Continue to move the retaining plates around the disk until sufficient blades have been removed to let you remove one of the retaining plates.
  4. Move the retaining plates, in turn, around the disk until they have all been removed.
  5. Remove the remaining blades from the stage 4 disk.
  6. Remove and discard the sealing strips HPC Rotor Blades (72-41-15, 01-520) from all the stage 4 blades.
7. 1. Do steps D.(1) thru D.(5) to remove the retaining plates and the blades from the stage 5 disk.
  2. Remove and discard the sealing strips HPC Rotor Blades (72-41-15, 01-820) from all the stage 5 blades.
1. SBE 72-0304: HP disks and blades - Introduction of a reworked stage 3 to 8 disk with revised L shaped sealing wires.
2. 1. With IAE 1R18590 Socket end 1 off release the two nut and screw lock assemblies.
  2. With IAE 1R18097 Drift 1 off move the blades around the disk until a blade can be removed through the loading slot.
  3. Do step (2) again, to remove each blade and the two nut and screw lock assemblies, until all the blades have been removed.
3. 1. Do steps A.(1) thru A.(3) for each stage of blades.
4. 1. Do steps A.(1) thru A.(3) to remove the blades and remove the sealing wires from the disks.
5. 1. With an applicable tool remove the lockplates from the rear of the stage 3 disk and discard.
  2. With IAE 1R18079 Drift 1 off move the retaining plates around the disk to close up the spaces between them. This will give sufficient space to remove one blade, forwards, from the disk.
  3. Continue to move the retaining plates around in a counterclockwise direction (when viewed from the rear) until the next blade can be removed.
  4. Continue this procedure until sufficient blades have been removed to let you remove one of the retaining plates.
  5. Move the retaining plates, in turn, around the disk until they have all been removed.
  6. Remove the remaining blades in a counterclockwise direction from the stage 3 disk.
6. 1. With an applicable tool remove the lockplates from the front of the stage 4 disk and discard.
  2. With IAE 1R18080 Drift 1 off move the retaining plates around the disk to close up the space between them. This will give sufficient space to remove one blade, forwards, from the disk.
  3. Continue to move the retaining plates around the disk until sufficient blades have been removed to let you remove one of the retaining plates.
  4. Move the retaining plates, in turn, around the disk until they have all been removed.
  5. Remove the remaining blades from the stage 4 disk.
  6. Remove and discard the sealing strips HPC Rotor Blades (72-41-15, 01-520) from all the stage 4 blades.
7. 1. Do steps E.(1) thru E.(5) to remove the retaining plates and the blades from the stage 5 disk.
  2. Remove and discard the sealing strips HPC Rotor Blades (72-41-15, 01-820) from all the stage 5 blades.
1. Refer to Figure, Figure, Figure and Figure.
2. Install the IAE 1R18091 Support stand 1 off on to the IAE 1R18090 Safety support stand 1 off. Refer to Figure.
3. Lift the compressor disks and shaft assembly from the trolley and install it on to the safety support stand.
4. Remove the universal slinging adapter from the dummy stub shaft.
5. Lift the compressor disks and shaft assembly off the safety support stand and put it above the IAE 1R18020 Build stand 1 off. Refer to Figure.
6. CAUTION
  YOU MUST NOT LET THE COMPRESSOR DISKS AND SHAFT ASSEMBLY HIT THE BUILD STAND.
  Slowly lower the compressor disks and shaft assembly in to the build stand. Make sure the dummy stub shaft engages in the location in the bottom of the build stand.
7. Remove the eight screws from the top of the build stand.
  NOTE
  The edge of the support ring that touches the compressor disks and shaft assembly is at an angle. Thus, one face of the support ring is shorter than the other face. The short face must go to the top.
8. Put one half of IAE 1R18021 Support ring 1 off on to the top of the build stand; align the four holes in the support ring with the four holes in the build stand. Install four of the screws through the support ring in to the build stand. Tighten the screws.
9. Install the other half of the support ring. Refer to Step and Step.
10. Remove the lifting adapter and universal slinging adapter from the end of the compressor shaft. Refer to Figure and Figure.
11. 1. If Data Plate contains part numbers 4W6517, 4W6518, 4W6519, 4W6520, 4W6617, 4W6620, or 4W6621; perform Step and Step for Post SB 72-0687 disassembly.
  2. For all other HPC Module part numbers, perform Step and Step for Pre SB 72-0687 disassembly.
1. Refer to Figure.
2. Remove the protection cover from the rotating air seal.
3. Remove the nuts that attach the rotating air seal to the compressor shaft.
4. 1. Install the thrust plate in to the end of the compressor shaft.
  2. Assemble the extractor and locate the two puller halves on the rotating air seal. Slide the retaining ring down on to the puller halves.
  3. Install the Hydraulic jack 1 off in to the extractor and with IAE 1F10026 Hydraulic hand pump 1 off slowly remove the rotating air seal. Put the rotating air seal on to an applicable surface.
  4. Remove the thrust plate from the compressor shaft.
1. Refer to Figure, Figure and Figure.
2. Remove the protection cover from the rotating air seal.
3. 1. Install the ten Retention Blocks between the bolt head and the stages 9-12 drum bore. Top side of Retention Blocks will press against the bolt head and the bottom side of the Retention Blocks will press against the stages 9-12 Drum Bore.
    NOTE
    There are nine full-size IAE 1P18865-1 Retention Blocks and one half-size IAE 1P18865-2 Retention Block. The half-size block is black in color and is to be the last block installed.
4. 1. Install the thrust plate into the end of the compressor shaft.
  2. Assemble the extractor and locate the two puller halves on the rotating air seal. Slide the retaining ring down on to the puller halves.
  3. Install the Hydraulic jack 1 off into the extractor and with IAE 1F10026 Hydraulic hand pump 1 off slowly remove the rotating air seal. Put the rotating air seal onto an applicable surface.
  4. Remove the thrust plate from the compressor shaft.
1. Refer to Figure and Figure.
2. Install the IAE 1R18441 Lifting adapter 1 off on to the end of the compressor shaft. Refer to Figure.
3. Assemble the IAE 1R19008 Puller 1 off with the two split rings located on the front face of the shaft forward flange. Make sure the tufnol pads are correctly located on the rear face of the stage 12 disk. Refer to Figure.
4. With a hoist support the compressor shaft.
5. CAUTION
  THE SET SCREWS MUST BE TIGHTENED IN SEQUENCE AND NOT MORE THAN ONE TURN AT A TIME.
  Turn each of the six set screws in small increments until the shaft is released from the stage 12 disk. Lift the shaft clear of the stage 12 disk and put it on an applicable surface.
6. Release the double retaining washers and remove the square head bolts. Discard the double retaining washers.
1. Refer to Figure, Figure and Figure.
2. Install the IAE 1R18441 Lifting adapter 1 off on to the end of the compressor shaft. Refer to Figure.
3. Install the IAE 1R19008 Puller 1 off with the two split rings located on the front face of the shaft forward flange. Make sure the tufnol pads are correctly located on the rear face of the stage 12 disk. Refer to Figure.
4. With a hoist support the compressor shaft.
5. CAUTION
  THE SET SCREWS MUST BE TIGHTENED IN SEQUENCE AND NOT MORE THAN ONE TURN AT A TIME.
  Turn each of the six set screws in small increments until the shaft is released from the stage 12 disk. Lift the shaft clear of the stage 12 disk and put it on an applicable surface.
6. 1. Attach the twenty-eight working nuts to the fourteen bolts until hand tight.
7. CAUTION
  AVOID DROPPING ANYTHING DOWN THE DISK CENTER TO PREVENT DAMAGE TO THE DISK BORE.
  Locate and remove the retention blocks, working nuts, bolts and washers.
  NOTE
  There are nine full-sized IAE 1P18865-1 Retention Blocks and one half-sized IAE 1P18865-2 Retention Block. The half-size retention block is black in color and is to be the first block removed.
1. Refer to Figure, Figure and Figure.
2. 1. Move the handles together to compress the spring and retract the flanges.
  2. Put the blanking tool in to the bore of the stages 3 to 12 compressor disks assembly. Make sure the flanges are aligned with the space between the stage 7 and 6 compressor disks.
  3. Release the handles and put the blanking tool on to the stage 6 compressor disk.
3. 1. Carefully lower the protection sleeve in to the bore of the stages 3 to 12 compressor disk assembly. Let the rear flange of the protection sleeve touch the rear face of the stage 12 compressor disk.
4. 1. Find the location dowel hole on the stage 12 compressor disk rear flange.
  2. Put the indexing ring (with the numbers to the top) on to the stage 12 compressor disk rear flange. Engage the dowel in the indexing ring in to the location dowel hole. Make sure the stage 12 compressor disk rear flange outer diameter is fully engaged in the indexing ring.
5. 1. Remove the location pin from the bush in the carrier.
  2. Pull the knob (on the end of the installation arm) to move the installation arm out of the carrier.
  3. Install the retaining pin through the hole in the carrier and the installation arm.
  4. Move the carrier until it touches the carrier stop.
6. 1. Lift the geared indexing spanner and put it on to the indexing ring. Make sure the geared head goes in to the protection sleeve.
7. 1. Remove the retaining pin from the carrier and installation arm.
  2. Move the installation arm in to the bore of the stages 3 to 12 compressor disks assembly.
  3. Move the carrier away from the carrier stop until the bush is aligned with the holes in the indexing ring.
  4. Adjust the position of the geared indexing spanner until the bush is aligned with the No.1 hole in the indexing ring.
  5. Install the location pin through the bush and the No. 1 hole.
  6. Install a Snap-on TMX60 extension in to the geared head extension. Push the extension to move the geared head towards the special head bolts.
  7. Install a Snap-on TM70B wrench on to the extension.
  8. Push the knob (on the end of the installation arm) to compress the spring. At the same time, push the wrench to make the geared head align with the special head bolts. Remove pressure from the knob.
  9. Operate the wrench to remove the splined nut from the special head bolt.
8. 1. Push the knob (on the end of the installation arm) to compress the spring. At the same time, pull the wrench to move the geared head clear of the special head bolt.
  2. Remove the wrench from the extension.
  3. Pull the extension to make the geared head extension fully retract.
  4. Remove the extension from the geared head extension.
  5. Remove the location pin from the bush in the carrier.
  6. Move the carrier until it touches the carrier stop.
  7. Pull the knob (on the end of the installation arm) to move the installation arm out of the carrier.
  8. Install the retaining pin through the hole in the carrier and the installation arm. Remove the splined nut and anti-score washer from the geared head extension.
9. 1. Do steps D. thru H. again and again until all of the spline nuts and anti-score washers have been removed.
  2. Remove all the tooling.
  3. Discard all the splined nuts, anti-score washers, special head bolts and anti-fret plates. Do not use this hardware again.
1. Refer to Figure and Figure.
2. 1. Move the handles together to compress the spring and retract the flanges.
  2. Put the blanking tool in to the bore of the stages 3 to 12 compressor disks assembly. Make sure the flanges are aligned with the space between the stage 7 and 6 compressor disks.
  3. Release the handles and put the blanking tool on to the stage 6 compressor disk.
3. 1. Carefully lower the protection sleeve in to the bore of the stages 3 to 12 compressor disk assembly. Let the rear flange of the protection sleeve touch the rear face of the stage 12 compressor disk.
4. 1. Find the location dowel hole on the stage 12 compressor disk rear flange.
  2. Put the indexing ring (with the numbers to the top) on to the stage 12 compressor disk rear flange. Engage the dowel in the indexing ring in to the location dowel hole. Make sure the stage 12 compressor disk rear flange outer diameter is fully engaged in the indexing ring.
5. 1. Make sure the nut (part of the IAE 1R18201 Torque spanner) is loose.
  2. Install a Snap-on TES10 socket on to the arm.
  3. Install the arm, socket end first, through the bore of the stages 3 to 12 compressor disk. Put the arm through the space between the stage 8 and 9 compressor disk.
6. 1. Put the rod through the bore of the stages 3 to 12 compressor disks. Engage the location pin in to the indexing ring at the No. 1 position.
7. 1. Engage the end of the rod on to the end of the arm.
  2. Install the screw, through the rod, in to the arm. Hand tighten the screw.
    NOTE
    Make sure the locator touches the top plate before the nut is tightened.
  3. Tighten the nut to engage the socket on to the first splined nut.
  4. Attach a torque wrench to the torque wrench location.
  5. Operate the torque wrench to remove the splined nut from the special head bolt.
8. 1. Loosen the nut on the rod.
    NOTE
    Step H.(2) will release the socket from the splined nut.
  2. Push the top plate until the stop touches the indexing ring.
  3. Pull the top plate until the location pin is clear of the bush in the indexing ring. Make sure the rod does not move.
  4. Move the torque spanner to the No. 2 position.
    NOTE
    Make sure the locator touches the top plate before the nut is tightened.
  5. Tighten the nut to engage the socket on to the second splined nut.
9. Do step G.(4) and G.(5) again.
10. 1. Do steps H. thru I. again and again until all of the spline nuts and anti-score washers have been removed.
  2. Remove all the tooling.
  3. Discard all the splined nuts, anti-score washers, special head bolts and anti-fret plates. Do not use this hardware again.
1. Refer to Figure, Figure and Figure.
2. Install the IAE 1R18691 Lifting fixture 1 off on to the stage 12 disk. Refer to Figure.
3. 1. Assemble the lower split ring and install it on the stage 8 disk.
  2. Assemble the top split ring assembly and install it on the stage 9 disk. Make sure the six set screws touch the lower split ring assembly.
4. With a hoist support the stage 9 to 12 disks.
5. CAUTION
  THE SET SCREWS MUST BE TIGHTENED IN SEQUENCE AND NOT MORE THAN ONE TURN AT A TIME.
  Turn each of the set screws in small increments until the stage 9 to 12 disks is released from the stage 3 to 8 disks.
6. Lift the stage 9 to 12 disks clear of the stage 3 to 8 disks.
7. Install the IAE 1R18025 Turnover stand adapter 1 off on to the IAE 1R18322 Turnover stand 1 off. Refer to Figure.
8. Install the stage 9 to 12 disks in the turnover stand.
1. Refer to Figure.
2. Operate the turnover stand to turn the stage 9 to 12 disks until the lifter is at the bottom.
3. 1. Loosen the eight clamp nuts sufficient to let the four clamps be moved to the center of the removal puller.
  2. Lift the clamp nuts and move the clamps to the center of the removal puller.
  3. Make sure that the six extraction bolts are fully retracted.
  4. CAUTION
    YOU MUST MAKE SURE THERE IS A CLEARANCE BETWEEN THE SPECIAL HEADED BOLTS AND THE HOLES IN THE REMOVAL PULLER.
    Use the handles to lift the removal puller and install it on to the stage 9 disk. Engage the special headed bolts through the holes in the extractor.
  5. Make sure that all of the pressure ring touches the stage 9 disk.
  6. Lift the clamp nuts and move the clamps to the outer edge of the removal puller. Make sure the clamps are engaged correctly on the vortex reducer ring. Tighten the eight clamp nuts.
  7. CAUTION
    THE EXTRACTION BOLTS MUST BE TIGHTENED IN SEQUENCE AND NOT MORE THAN ONE TURN AT A TIME.
    Tighten the six extraction bolts in small increments until the vortex reducer ring is released from the stage 9 disk.
  8. Use the handles to lift the removal puller and vortex reducer ring assembly off the stage 9 disk. Put the assembly on an applicable surface and remove the removal puller.
1. Refer to Figure, Figure and Figure.
2. Install the IAE 1R18065 Lifter 1 off on to the stage 8 disk. Refer to Figure.
3. Remove the bolts that attach the dummy stub shaft to the stage 3 to 8 disks. Refer to Figure.
4. Attach a hoist and lift the stage 3 to 8 disks clear of the build stand and the dummy stub shaft and install it in the IAE 1R18092 Support tool 1 off. Refer to Figure.
5. Remove the IAE 1R18673 Dummy stub shaft and install the curvic protector.

Install the protection cover on the rotating air seal

Install the beam sling on to the HP compressor rotor assembly

Remove/install the universal sling adapters

Install the HP compressor rotor assembly on to the safety support stand

Install the HP compressor rotor in to the tip check fixture

Set the transducer carriers to zero

Measure the seal and stator path diameters

Install the HP compressor rotor assembly in to the trolley

HP compressor rotor tip radius

Pre SBE 72-0295 : HP compressor rotor tip radius

Post SBE 72-0295 - HP Compressor Rotor Tip Radius

Stage 3 disk curvic coupling bolts torque sequence

Install the HP compressor rotor assembly in to the build stand

Remove the rotating air seal

Install the lifter on the compressor shaft

Remove the HP compressor shaft

Remove the splined nuts and the anti-score washers

Install the lifter on the stage 12 disk

Remove the stage 9 to 12 disks from the stage 3 to 8 disks

Install the stage 9 to 12 disks in the turnover stand

Remove the vortex reducer ring from the stage 9 to 12 disks

Install the lifter on to the stage 8 disk

Remove the dummy stub shaft

Install the stage 3 to 8 disks in the support tool

Remove Rotating Air Seal (Post SB 72-0687)

(Post SB 72-0687) Configuration Immobilizer Tool (IAE 1P18865) and Retention Blocks (IAE 1P18865-1 and IAE 1P18865-2)

Requirements After Job Completion

Follow-On Conditions

NONE

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:	IE304
Enterprise Name:	DELETED
BU Name:	DELETED,SEE CAGE CODE 0V6W9

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:	LOCAL
Tool Number:	Digital read out equipment
Tool Name:	Digital read out equipment

TASK 72-41-10-040-001-B00 HPC Rotor Assembly - Disassemble The Rotor Assembly, Disassembly-001

Export Control

Copyright

Applicability

Common Information

TASK 72-41-10-040-001-B00 HPC Rotor Assembly - Disassemble The Rotor Assembly, Disassembly-001

General

NOTE

NOTE

Preliminary Requirements

Pre-Conditions

Support Equipment

Consumables, Materials and Expendables

Spares

Safety Requirements

Procedure

SUBTASK 72-41-10-040-078 Prepare the Tip Check Fixture for Installation of the HP Compressor Rotor Assembly

SUBTASK 72-41-10-040-084 Install the HP Compressor Rotor Assembly in to the Tip Check Fixture

NOTE

CAUTION

CAUTION

SUBTASK 72-41-10-040-085 Set the Axial Position of the HP Compressor Rotor Assembly

SUBTASK 72-41-10-040-086 Do a Check on the Compressor Rotor for Concentricity and Swash

SUBTASK 72-41-10-040-087 Set the Transducer Carriers to the Zero Position

SUBTASK 72-41-10-040-088 Measure and Calculate the Stage 3 to 4 Seal Fin Diameters at Location 1001

SUBTASK 72-41-10-040-115 Measure and Calculate the Stage 4 to 5 Seal Fin Diameters at Locations 1002 and 1003

SUBTASK 72-41-10-040-116 Measure and Calculate the Stage 5 to 6 Seal Fin Diameters at Location 1004

SUBTASK 72-41-10-040-117 Measure and Calculate the Stator Vane Path Diameters

SUBTASK 72-41-10-040-118 Measure and Calculate the HP Compressor Rear Rotating Seal Fin Diameters

SUBTASK 72-41-10-040-119 Remove the HP Compressor Rotor Assembly from the Tip Check Fixture

SUBTASK 72-41-10-040-089 Install the HP Compressor Rotor Assembly in the Trolley

CAUTION

SUBTASK 72-41-10-040-090 Remove the HP Compressor Rotor Assembly from the Trolley and Install it in to the Grinding Machine

NOTE

NOTE

SUBTASK 72-41-10-040-091 Measure the Swash and Run-out of the HP Compressor Rotor Assembly

SUBTASK 72-41-10-040-092-A00 Measure the Length of the HP Compressor Blades,andand (Pre SBE 72-0295)

NOTE

SUBTASK 72-41-10-040-092-B00 Measure the Length of the HP Compressor Blades (SBE 72-0295)

NOTE

SUBTASK 72-41-10-040-093 Remove the HP Compressor Rotor Assembly from the Grinding Machine and Install it in to the Trolley

NOTE

SUBTASK 72-41-10-040-094-A00 Remove the Blades from the HP Compressor Rotor Assembly (Pre SBE 72-0300 and Pre SBE 72-0304)

NOTE

NOTE

SUBTASK 72-41-10-040-094-B00 Remove the Blades from the HP Compressor Rotor Assembly (SBE 72-0300)

CAUTION

NOTE

NOTE

SUBTASK 72-41-10-040-094-C00 Remove the Blades from the HP Compressor Rotor Assembly (SBE 72-0304)

CAUTION

NOTE

CAUTION

SUBTASK 72-41-10-040-095 Install the HP Compressor Disks and Shaft Assembly in to the Build Stand

CAUTION

NOTE

SUBTASK 72-41-10-040-096 Remove the Rotating Air Seal (Pre SB 72-0687)

SUBTASK 72-41-10-040-132 Remove Rotating Air seal (Post SB 72-0687)

NOTE

SUBTASK 72-41-10-040-097 Remove the HP Compressor Shaft (Pre SB 72-0687)

CAUTION

SUBTASK 72-41-10-040-133 Remove the HP Compressor Shaft (Post SB 72-0687)

CAUTION

CAUTION

CAUTION

NOTE

SUBTASK 72-41-10-040-098-001 Remove the Splined Nuts and Anti-score Washers (Geared Indexing Spanner Method)

CAUTION

SUBTASK 72-41-10-040-098-002 Remove the Splined Nuts and Anti-score Washers (Torque Spanner Method)

CAUTION

NOTE

NOTE

NOTE

NOTE

NOTE

SUBTASK 72-41-10-040-099 Remove the Stage 9 to 12 Disks and Vortex Reducer Ring from the Stage 3 to 8 Disks

CAUTION

SUBTASK 72-41-10-040-100 Remove the Vortex Reducer Ring from the Stage 9 to 12 Disks

CAUTION

CAUTION