TASK 72-41-20-440-006-A01 HPC Rear Cases And Vanes Assembly - Machine The Stator Vane Tips And The Rotor Path Ring Liners (Silicone Rubber Mould Method), Assembly-006

DMC:V2500-A1-72-41-2000-00A-710B-B|Issue No:004.00|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

V2500-A1

Common Information

TASK 72-41-20-440-006-A01 HPC Rear Cases And Vanes Assembly - Machine The Stator Vane Tips And The Rotor Path Ring Liners (Silicone Rubber Mould Method), Assembly-006

General

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

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

For standard torque data and procedures refer to SPM TASK 70-41-00-400-501, SPM TASK 70-41-01-400-501 and SPM TASK 70-41-02-410-501.

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.

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

Refer to Figure for a sectional view of the HP compressor rear cases and vanes.

Make sure all the flange faces and tool faces that touch are very clean.

This TASK gives the procedures to machine the stator vane tips and the rotor path ring liners. For other parts of the HP compressor rear cases and vanes assembly, refer to TASK 72-41-20-440-000 (ASSEMBLY-000).

This procedure involves the use of a plastic mould which can be made locally, the procedure to make the mould is given in this TASK. The tooling can only be manufactured using new HP Compressor vanes.

Machining Requirements

The data that follows is a guideline. If any additional data is necessary contact IAE.

For the rotor path ring machining, a machine is necessary that can meet the conditions that follow:-

Permits a 31.00 in. (790.0 mm) diameter by 16.00 in. (401.5 mm) depth workpiece to be installed.

The workpiece must be turned in a counterclockwise direction, when viewed from the tailstock.

Permits a K Grade Carbide ITT turning tool with a 0.031in. (0.8 mm) radius tip to be installed.

The conditions that follow must be used when you machine the rotor path linings:-

A component surface speed of 70m/min. This is equivalent to a speed of 43 rpm.

The maximum depth of cut to be used is 0.006 in. (0.15 mm).

The feed rate is to be determined by 'general feel' for the workpiece.

For the stator vane tip grinding, a machine is necessary that can meet the conditions that follow:-

Permits a 31.00 in. (790.0 mm) diameter by 16.00 in. (401.5 mm) depth workpiece to be installed.

The workpiece must be turned in a clockwise direction, when viewed from the tailstock.

Permits a grinding set-up to be attached to the machine. It will be necessary for the grinding wheel to be turned.

The grinding wheel must be turned in a counterclockwise direction, when viewed from the tailstock.

Permits a swarf extraction unit to be installed.

The conditions that follow must be used when you are grinding the stator vane tips:-

A component surface speed of 34 m/min. This is equivalent to a speed of 23 rpm.

A grinding wheel surface speed of 1675 m/min. This is equivalent to a speed of approximately 4090 rpm at the recommended grinding wheel diameter.

A grinding wheel diameter of between 4.6 in. and 5.5 in. (118 mm and 140 mm).

Grind the repair area to the requirements of Figure to Figure. Refer to the SPM for consumables and definition where it is appropriate.

It is recommended that you use a plunge grinding method with an infeed rate of 0.0075 mm per revolution.

Use a 'spark-out' time of 10 revolutions or 25 seconds.

NOTE

To identify the consumable materials refer to the PCI.

NOTE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
IAE 19788 Clamping ring (Method B only)0AM53IAE 19788
IAE 19789 Clamping ring (Method B only)0AM53IAE 19789
IAE 19790 Clamping ring (Method B only)0AM53IAE 19790
IAE 19791 Clamping ring (Method B only)0AM53IAE 19791
IAE 19792 Clamping ring (Method B only)0AM53IAE 19792
IAE 1R18212 Support ring0AM53IAE 1R182121
IAE 1R18321 Turnover stand0AM53IAE 1R183211
IAE 1R18412 Turning fixture0AM53IAE 1R184121
IAE 1R18413 Turnover stand adaptor0AM53IAE 1R184131
IAE 1R18414 Boring bar0AM53IAE 1R184141
IAE 1R18415 Pallet0AM53IAE 1R184151
IAE 1R18416 Lifting tool0AM53IAE 1R184161
IAE 1R18417 Lifting Turnover trunnions0AM53IAE 1R184172
IAE 1R18418 Multiflex holder0AM53IAE 1R184181
IAE 1R18419 Probe holder0AM53IAE 1R184191
IAE 1R18420 Dressing attachment0AM53IAE 1R184201
IAE 1R18421 Diamond dresser0AM53IAE 1R184211
IAE 1R18422 Support probe bracket0AM53IAE 1R184221
IAE 1R18430 Turning holder0AM53IAE 1R184301
IAE 1R18431 Lifting beam0AM53IAE 1R184311
IAE 1R18503 Machine drawing0AM53IAE 1R185031
IAE 1R18661 Containment ring0AM53IAE 1R186611
IAE 1R18662 Containment ring0AM53IAE 1R186621
IAE 1R18663 Containment ring0AM53IAE 1R186631
IAE 1R18664 Containment ring0AM53IAE 1R186641
IAE 1R18665 Containment ring0AM53IAE 1R186651
IAE 1R18666 Containment ring0AM53IAE 1R186661
IAE 1R18667 Containment ring0AM53IAE 1R186671
IAE 1R18668 Containment ring0AM53IAE 1R186681
IAE 1R18669 Containment ring0AM53IAE 1R186691
IAE 1R18670 Containment ring0AM53IAE 1R186701
IAE 1R18738 Setting block0AM53IAE 1R187381
IAE 1R18739 Setting block0AM53IAE 1R187391
IAE 1R18740 Setting block0AM53IAE 1R187401
IAE 1R18741 Setting block0AM53IAE 1R187411
IAE 1R18760 Grinding head0AM53IAE 1R187601
IAE 3R18232 Lifting beam0AM53IAE 3R182321
Cleaning bathLOCALCleaning bath
GlovesLOCALGloves

Heat resistant

K Grade I.T.T. Turning ToolLOCALK Grade I.T.T. Turning Tool
OvenLOCALOven
VacuumLOCALVacuum

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
DELETEDLOCALDELETED
CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPERLOCALCoMat 02-002
CoMat 02-181 MODELLING CLAYLOCALCoMat 02-181
CoMat 07-038 AIR DRYING ENAMELk3504CoMat 07-038
CoMat 08-036 SILICONE RUBBER COMPOUNDLOCALCoMat 08-036
CoMat 10-077 APPROVED ENGINE OILSX333XCoMat 10-077
CoMat 12-031 FRENCH CHALKLOCALCoMat 12-031

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-41-20-440-113 Apply the Masking Tape to the HP Compressor Rear Cases and Vanes

      1. Apply the CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER to the subsequent areas.

      1. To seal the bleed slots in the stage 7 and 10 stator vanes.

      2. to seal the holes in the stage 8, 9 and 11 intrascope vanes.

      3. To seal the clearances at the stage 7 to 11 stator stop vanes.

      4. To seal the clearances between the stage 7 to 11 stator vanes and their rear liners.

    2. Apply the masking tape to the stage 7 to 12 rotor path ring linings. Make sure the linings are completely protected.

    2. SUBTASK 72-41-20-440-114 Install the Containment Rings on to the Stage 7 to 11 Stator Vanes

    1. Refer to Figure and Figure.

      2. Install IAE 1R18662 Containment ring 1 off, on to the stage 7 stator vanes.

        NOTE

        The outer face is the one that goes on to the stator vane tips.

      1. Attach a 0.118 in. to 0.276 in. (3.00 mm to 7.00 mm) strip of CoMat 02-181 MODELLING CLAY to the outer face of the containment ring.

      2. Apply a thin layer of CoMat 12-031 FRENCH CHALK to the faces of the modelling clay that will touch the stator vanes.

      3. Install the wax containment ring on to the stator vanes. Push the wax containment ring on to the stator vanes until the stator vane tips are in the modelling clay.

      3. Install IAE 1R18661 Containment ring 1 off, on to the stage 7 stator vanes.

      1. Put the wax containment ring on the trailing edge of the stator vanes.

      2. Use CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER to hold the wax containment rings in their correct position. Refer to Figure for the dimensions of the wax containment ring positions.

      4. Install IAE 1R18664 Containment ring 1 off, on to the stage 8 stator vanes.

      1. Do Step thru Step again.

      5. Install IAE 1R18663 Containment ring 1 off, on to the stage 8 stator vanes.

      1. Do Step and Step again.

      6. Install IAE 1R18666 Containment ring 1 off, on to the stage 9 stator vanes.

      1. Do Step thru Step again.

      7. Install IAE 1R18665 Containment ring 1 off, on to the stage 9 stator vanes.

      1. Put the wax containment ring on the leading edge of the stator vanes.

      2. Use CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER to hold the wax containment rings in their correct positions. Refer to Figure for the dimensions of the wax containment ring positions.

      8. Install IAE 1R18668 Containment ring 1 off, on to the stage 10 stator vanes.

      1. Do Step thru Step again.

      9. Install IAE 1R18667 Containment ring 1 off, on to the stage 10 stator vanes.

      1. Do Step and Step again.

      10. Install IAE 1R18670 Containment ring 1 off, on to the stage 11 stator vanes.

      1. Do Step thru Step again.

      11. Install IAE 1R18669 Containment ring 1 off, on to the stage 11 stator vanes.

      1. Do Step and Step again.

    3. SUBTASK 72-41-20-440-195 Manufacture the Tool to Restrain the Stator Vanes Stages 9 to 11

      NOTE

      The tooling can only be manufactured using new stator vanes.

      NOTE

      The procedure is not required if the tool has been made previously and is still in good condition.

    1. Mix a sufficient amount of CoMat 08-036 SILICONE RUBBER COMPOUND in accordance with the manufacturers data sheet. It is recommended that the mixture is put in a vacuum chamber to remove trapped air. Alternatively allow mixture to cure for 10 to 15 minutes at room temperature to allow the bubbles to rise to the surface for removal.

    2. Carefully apply the CoMat 08-036 SILICONE RUBBER COMPOUND to the stage 9 to 11 stator vane moulding cavities.

    3. Fill the vane cavities until the rubber reaches the top of the mould.

    4. Allow the mixture to cure for 18 to 24 hours at room temperature.

      NOTE

      The rubber mould should be stored at room temperature in clean dry conditions. Avoid contact with resins and other materials which may attack the mould.

    5. When the rubber has cured remove all the tooling from the vanes. Carefully make a cut through the cross section of the mould and remove the clamping ring from the stator vanes.

    6. Inspect the tool for integrity/damage prior to use.

      NOTE

      If a full set of rings is to be produced then each stage must be moulded individually from stages 7 to 11 in sequence for ease of removal once the rubber has cured.

      7. Use a black permanent marker pen to identify the tool with the following:

      4. Engine type (V2500-A1).

      5. Stage number (eg stage 9 vanes).

    4. SUBTASK 72-41-20-440-196 Install the Tooling to Hold the Stage 9 to 11 Stator Vanes

      1. Visually inspect the silicone rubber tooling for defects and loss of elasticity.

      1. If tooling has defects or loss of elasticity, reject and repeat Step.

      2. Install the silicone rubber tooling to the HP Compressor stage with fixed geometry stator vanes stages 9 to 11.

    5. SUBTASK 72-41-20-440-087 Turn the HP Compressor Rear Cases and Vanes

    1. Refer to Figure.

      2. Install the IAE 1R18212 Support ring 1 off on the front support cone.

      1. Put the support ring in position on the front support cone. Align the six bolts in the support ring with the six holes in the front support cone outer flange.

      2. Install the six bolts and washers, part of the support ring. Tighten the six bolts.

      1. Put one of the lifting turnover trunnions on to the location pin on the support ring.

      2. Install the two bolts and washers which attach the lifting turnover trunnion to the support ring.

      3. Tighten the two bolts.

      4. Install the remaining lifting turnover trunnion as given in Step to Step.

    4. Use a suitable hoist attached to IAE 1R18431 Lifting beam 1 off and set the lifting beam above the HP compressor rear case and vanes.

    5. Connect the two legs of the lifting beam to the two lifting turnover trunnions.

    6. Carefully lift the HP compressor rear cases and vanes.

    7. Turn the HP compressor rear cases and vanes through 180 degrees. The rear face (the cross key location ring) should point down. Lower the HP compressor rear cases and vanes on to a clean work bench.

    8. Remove the six bolts and the six washers which attach the HP compressor rear cases and vanes to the support ring.

    9. Use the hoist to remove the lifting beam the lifting turnover trunnions and the support ring from the HP compressor rear cases and vanes.

    10. Disassemble the tools and put them on a suitable work surface.

    6. SUBTASK 72-41-20-440-197 Manufacture the Tool to Restrain the Stator Vanes Stages 7 to 8

      NOTE

      The tooling can only be manufactured using new stator vanes.

      NOTE

      The procedure is not required if the tool has been made previously and is still in good condition.

    1. Mix a sufficient amount of CoMat 08-036 SILICONE RUBBER COMPOUND in accordance with the manufacturer's data sheet. It is recommended that the mixture is put in a vacuum chamber to remove trapped air. Alternatively allow mixture to cure for 10 to 15 minutes at room temperature to allow the bubbles to rise to the surface for removal.

    2. Carefully apply the CoMat 08-036 SILICONE RUBBER COMPOUND to the stage 6 to 8 stator vane moulding cavities.

    3. Fill the vane cavities until the rubber reaches the top of the mould.

    4. Allow the mixture to cure for 18 to 24 hours at room temperature.

      NOTE

      The rubber mould should be stored at room temperature in clean dry conditions. Avoid contact with resins and other materials which may attack the mould.

    5. When the rubber has cured remove all the tooling from the vanes. Carefully make a cut through the cross section of the mould and remove the clamping ring from the stator vanes.

    6. Inspect the tool for integrity/damage prior to use.

      NOTE

      If a full set of rings is to be produced then each stage must be moulded individually from stages 7 to 11 in sequence for ease of removal once the rubber has cured.

      7. Use a black permanent marker pen to identify the tool with the following:

      3. Engine type (V2500-A1).

      4. Stage number (eg stage 7 vanes).

    7. SUBTASK 72-41-20-440-198 Install the Tooling to Restrain the HP Compressor Stage 7 to 11 Stator Vanes

      1. Visually inspect the silicone rubber tooling for defects and loss of elasticity.

      1. If tooling has defects or loss of elasticity, reject and repeat Step.

      2. Install the silicone rubber tooling to the HP Compressor stage with fixed geometry stator vanes stages 7 to 9.

    3. If this TASK has not already been completed, install the silicone rubber tooling to the HP Compressor stages with fixed geometry stator vanes stages 7 to 11.

    8. SUBTASK 72-41-20-440-121 Prepare the Tools to Turn the HP compressor Rear Cases and Vanes from the Vertical to the Horizontal

    1. Refer to Figure.

      1. Attach a suitable sling and hoist to the turnover stand adapter.

      2. Lift the turnover stand adapter and put it in position in the turnover stand.

      3. Attach the turnover stand adapter to the turnover stand with the six tool bolts. Use the three 0.375 in. (9.5 mm) 24 UNF x 0.75 in. (19.05 mm) long bolts at the position 2. Use the three 0.375 in. (9.5 mm) 24 UNF x 0.50 in. (12.7 in.) long bolts at the position 1.

      4. Tighten the six tool bolts to safety the turnover stand adapter.

      3. Install IAE 1R18412 Turning fixture 1 off, on to the turnover stand adapter.

      1. Attach a suitable sling and hoist to the turning fixture.

      2. Lift the turning fixture and put it in position over the turnover stand adapter.

      3. Lower the turning fixture on to the turnover stand adapter. At the same time align the dowel on the turnover stand adapter with the dowel hole in the turning fixture.

      4. Attach the turning fixture to the turnover stand adapter with the four tool bolts. Use the four 0.75 in. (19.05 mm) 10UNC x 3.0 in. (76.2 mm) long bolts.

      5. Tighten the bolts to safety the turning fixture.

    9. SUBTASK 72-41-20-440-088 Install the HP Compressor Rear Cases and Vanes in the Turning Fixture

    1. Refer to Figure and Figure.

      2. Install the IAE 1R18416 Lifting tool 1 off on to the front support cone ENGINE-HP COMPRESSOR RING CASES (72-41-21, 03-300).

      1. Use a suitable hoist and lift the lifting tools on to the HP compressor rear cases and vanes.

      2. Align the four holes in the lifting tool with four holes in the front support cone ENGINE-HP COMPRESSOR RING CASES (72-41-21, 03-300) outer flange. Use the bolt holes that are on each side of a location dowel hole.

      3. Install the four bolts and washers, part of the lifting tool, through the front support cone outer flange. These attach the lifting tool to the front support cone.

      4. Tighten the four bolts.

      3. Install the HP compressor rear cases and vanes in to the tools assembled in Step.

      1. Remove the 10 nuts and the 10 washers which attach the 10 clamps to the turning fixture. Remove the 10 clamps.

      2. Release the 24 nuts which attach the 12 location blocks to the turning fixture. Slide the 12 location blocks radially out.

      3. Use a suitable hoist attached to the lifting tool and lift the HP compressor rear cases and vanes above the turning fixture.

      4. Carefully lower the HP compressor rear cases and vanes in to the turning fixture. Engage the 10 dowels in the turning fixture with the 10 dowel locating holes in the front support cone outer flange. There is a dowel location hole on each of the legs of the lifting tool. These must be located on two of the dowels on the turning fixture.

      5. Align the cross key ring and seal assembly with the 12 locating blocks on the turning fixture.

      6. Install the 10 clamps removed in step (1). Tighten the 10 nuts in sequence.

      7. Slide the location blocks radially in tighten the 24 nuts in the correct sequence. The location blocks must not change the position of the HP compressor rear cases and vanes. The HP compressor rear cases and vanes must be held by a minimum of six location blocks. The location blocks must be set at equal positions around the flange.

      8. Remove the four bolts and washers which attach the lifting tool to the front support cone.

      9. Remove the lifting tool.

    4. Turn the HP compressor rear cases and vanes with the turning fixture from the vertical position to the horizontal position.

    10. SUBTASK 72-41-20-440-117 Install the HP compressor Rear Cases and Vanes in the Pallet

    1. Refer to Figure.

      2. Install the IAE 3R18232 Lifting beam 1 off on to the IAE 1R18412 Turning fixture 1 off.

      1. remove the four bolts from the front face of the lifting beam.

      2. Use a suitable hoist and lift the lifting beam on to the turning fixture. Align the lifting beam front face with the location on the turning fixture.

      3. Install the four bolts removed in Step.

      4. Tighten the four bolts.

      3. Lift the HP compressor rear cases and vanes.

      1. Adjust the hoist used in Step until it just holds the weight of the turning fixture and the HP compressor rear cases and vanes.

      2. Remove the four bolts and washers which attach the turning fixture to the turnover stand adapter.

      3. Use the hoist and remove the turning fixture with the HP compressor rear cases and vanes from the turnover stand adapter.

    4. Carefully lower the assembly in to the IAE 1R18415 Pallet 1 off.

    5. Transport the assembly to the machine area to have the stator vanes and rotor path rings machined.

    11. SUBTASK 72-41-20-324-051 Machine the Stage 7 to 11 Stator Vanes

    1. Refer to Figure, Figure and Figure.

    2. Attach the IAE 1R18760 Grinding head 1 off to the machine. Use a suitable adapter plate.

      3. Set up the universal machining centre.

      1. Attach the IAE 1R18420 Dressing attachment 1 off to the grind attachment on the machine and secure with the four set screws.

      2. Set the dressing angle. Use IAE 1R18738 Setting block 1 off, IAE 1R18739 Setting block 1 off or IAE 1R18741 Setting block 1 off. Refer to the IAE 1R18503 Machine drawing 1 off for the correct setting block.

      3. Attach the IAE 1R18421 Diamond dresser 1 off to the dressing attachment and secure with the set screw.

      4. Attach the IAE 1R18422 Support probe bracket 1 off to the grind attachment. Position the support probe bracket behind the dressing attachment and secure with the four set screws.

      5. Attach the IAE 1R18418 Multiflex holder 1 off at the locating slot on the support probe bracket and secure with the three set screws.

    4. To measure the stages 7 to 11 stator vanes attach the IAE 1R18419 Probe holder 1 off at the multiflex holder interface and secure with the allen screw.

    5. Install the HP compressor rear cases and vanes in to the machine.

    6. Use the conditions given in machine requirements to machine the stage 7 to 11 stator vanes. Write down a record of the dimensions which the stator vanes are machined to.

    7. Use a Vacuum adjacent to the grinding wheel to remove the dust during the grinding process.

    8. Remove the burrs from the stator vane tips and all unwanted material.

    9. Measure the stator vane tip surface profile.

    10. Remove the HP compressor rear cases and vanes and the turning fixture from the machine.

    12. SUBTASK 72-41-20-324-052 Machine the Stage 7 to 12 Rotor Path Rings (Pre SBE 72-0463 and SBE 72-0463)

    1. SBE 72-0463: Engine - HP compressor - Increase in tip clearance to stage 6 and stage 7 rotor paths.

    2. Refer to Figure, Figure, Figure and Figure.

    3. Remove the CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER from the stage 7 to 12 rotor path rings.

    4. Install the HP compressor rear cases and vanes in the machine.

      5. Set up the universal machining centre.

      1. Attach the IAE 1R18414 Boring bar 1 off to the machine tool post and secure with the three set screws.

      2. Attach the IAE 1R18418 Multiflex holder 1 off at the locating slot on the boring bar and secure with the three grub screws.

      3. Attach the IAE 1R18430 Turning holder 1 off to the multiflex holder interface and secure with the allen screw.

    6. To measure the rotor path rings remove the IAE 1R18430 Turning holder and install the IAE 1R18419 Probe holder 1 off to the multiflex holder interface and secure with the allen screw.

    7. Set and measure the swash and runout of the stage 7 and 12 rotor path rings. This should be a maximum of 0.003 in. (0.08 mm). Write down a record of the values.

    8. Use the conditions given in machining requirements to machine the stage 7 to 12 rotor path rings. Write a record of the dimensions which the rotor path rings are machined to.

      NOTE

      Only remove the minimum quantity of abradable lining to show the metal of the rotor path rings at the front and rear of the liner.

    9. Remove the unwanted material and the machine cusps after you have machined the rotor path rings.

    10. Remove the HP compressor rear cases and vanes from the machine.

    11. Put the HP compressor rear cases and vanes in to IAE 1R18415 Pallet 1 off.

    13. SUBTASK 72-41-20-440-089 Prepare the HP Compressor Rear Cases and Vanes to be Cleaned

    1. Use a suitable hoist and lift the HP compressor rear cases and vanes from the pallet. Refer to Figure.

    2. Align the turning fixture with the turnover stand adapter in the turnover stand.

    3. Install the four bolts and the four washers to attach the turning fixture to the turnover stand adapter. Tighten the four bolts.

    4. Remove the bolts which attach the lifting beam to the turning fixture. Remove the hoist and the lifting beam.

    5. Turn the assembly in the turnover stand from the horizontal position to the vertical position.

    6. Install the IAE 1R18416 Lifting tool 1 off as given in Step.

    7. Attach a suitable hoist to the lifting tool. Hold the weight of the assembly on the hoist.

      8. Remove the HP compressor rear cases and vanes from the turning fixture.

      1. Loosen the 12 nuts which secure the 12 location blocks on the turning fixture.

      2. Slide the location blocks radially out.

      3. Remove the 10 nuts and washers which attach the 10 clamps to the turning fixture.

      4. Remove the 10 clamps.

      5. Use the hoist installed in step G and lift the HP compressor rear cases and vanes on to a clean work surface.

      6. Remove the hoist and the lifting tool from the HP compressor rear cases and vanes.

    14. SUBTASK 72-41-20-110-053 Clean the HP Compressor Rear Case and Vanes

    1. Remove all masking from the stator vanes and cases and vanes.

    2. Remove the silicone rubber tooling from the HP Compressor vanes.

    3. Use a Vacuum to remove any loose swarf or dust which may have accumulated during the grinding process.

    4. Aqueous degrease the HP compressor cases and vanes by TASK 70-11-03-300-503.

    15. SUBTASK 72-41-20-440-090 Install the HP Compressor Rear Cases and Vanes on to the Support Rings

    1. Refer to Figure.

      2. Install the IAE 1R18212 Support ring 1 off on to the front support cone.

      1. Put the two halves of the support ring in position on the front support cone. Align the six bolt holes in the support ring with six holes in the front support cone outer flange.

      2. Install the six bolts and washers, part of the support ring. Tighten the six bolts.

    3. Install the IAE 1R18417 Lifting Turnover trunnions 2 off as given in Step.

    4. Attach the IAE 1R18431 Lifting beam 1 off on a suitable hoist to the lifting turnover trunnions.

    5. Lift the HP compressor rear cases and vanes.

    6. Turn the HP compressor rear cases and vanes through 180 degrees. The support rings must point down.

    7. Lower the HP compressor rear cases and vanes with the support ring on to a clean work surface.

    8. Remove the lifting beam and the lifting turnover trunnions from the HP compressor rear cases and vanes.

    16. Figure: View Through the HP Compressor Rear Cases and Vanes

    View Through the HP Compressor Rear Cases and Vanes

    Figure: Install the Wax Containment Rings

    Install the Wax Containment Rings

    Figure: Apply the Encapsulating Material on To the Stator Vanes

    Apply the Encapsulating Material on To the Stator Vanes

    Figure: Install the Lifting Turnover Trunnions

    Install the Lifting Turnover Trunnions

    Figure: Preapre the Tools to Turn the HP Compressor Rear Cases and Vanes

    Preapre the Tools to Turn the HP Compressor Rear Cases and Vanes

    Figure: Install the HP Compressor Rear Cases and Vanes in to the Turning Fixture

    Install the HP Compressor Rear Cases and Vanes in to the Turning Fixture

    Figure: Install the HP Compressor Rear Cases and Vanes in to the Turning Fixture

    Install the HP Compressor Rear Cases and Vanes in to the Turning Fixture

    Figure: Move the HP Compressor Rear Cases and Vanes From the Turnover Stand to the Pallet

    Move the HP Compressor Rear Cases and Vanes From the Turnover Stand to the Pallet

    Figure: Machine the Stator Vane Tips

    Machine the Stator Vane Tips

    Figure: Machine the Stator Vane Tips

    Machine the Stator Vane Tips

    Figure: Machine the Stator Vane Tips

    Machine the Stator Vane Tips

    Figure: Machine the Rotor Path Ring Liners

    Machine the Rotor Path Ring Liners

    Figure: Pre SBE 72-0463: Machine the Rotor Path Ring Liners

    Pre SBE 72-0463: Machine the Rotor Path Ring Liners

    Figure: Machine the Rotor Path Ring Liners

    Machine the Rotor Path Ring Liners

    Figure: SBE 72-0463: Machine the Rotor Path Ring Liners

    SBE 72-0463: Machine the Rotor Path Ring Liners

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised step. (19VG309)

Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:X333X
Enterprise Name:REFER TO V2500 SB ENG-79-0108
Link not Found
Manufacturer Code:LOCAL
Supply Number:CoMat 02-002
Type:sp01
Supply Short Name:CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER
Supply Name:CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER
Specification Groups:
Doc NumberType
JCR-198SCOTCH 202 PREMIUM GRADE (A-A-883 TYPE I)
OMAT: 237SCOTCH 202 PREMIUM GRADE (A-A-883 TYPE I)
Suppliers:
ManufacturerRemarks
LOCAL
94960
K0993
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 02-181
Type:sp01
Supply Short Name:CoMat 02-181 MODELLING CLAY
Supply Name:CoMat 02-181 MODELLING CLAY
Specification Groups:
Doc NumberType
OMAT: 249PLASTICINE A-A-51006
Suppliers:
ManufacturerRemarks
LOCAL
K6835
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:71984
Supply Number:CoMat 08-036
Type:sp01
Supply Short Name:CoMat 08-036 SILICONE RUBBER COMPOUND
Supply Name:CoMat 08-036 SILICONE RUBBER COMPOUND
Specification Groups:
Doc NumberType
SILASTIC RUBBER J RTV
Suppliers:
ManufacturerRemarks
71984
K6835
KG699
B1571
V277V
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
Supply Number:CoMat 12-031
Type:sp01
Supply Short Name:CoMat 12-031 FRENCH CHALK
Supply Name:CoMat 12-031 FRENCH CHALK
Specification Groups:
Doc NumberType
DEF STAN 68-209 FRENCH CHALK
Suppliers:
ManufacturerRemarks
LOCAL
K6835
Manufacturer Code:LOCAL
Supply Number:DELETED
Type:sp01
Supply Short Name:DELETED
Supply Name:DELETED
Specification Groups:
Doc NumberType
DELETED
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:LOCAL
Tool Number:Cleaning bath
Tool Name:Cleaning bath
Manufacturer Code:LOCAL
Tool Number:Gloves
Tool Name:Gloves
Manufacturer Code:0AM53
Tool Number:IAE 19788
Tool Name:IAE 19788 Clamping ring (Method B only)
Manufacturer Code:0AM53
Tool Number:IAE 19789
Tool Name:IAE 19789 Clamping ring (Method B only)
Manufacturer Code:0AM53
Tool Number:IAE 19790
Tool Name:IAE 19790 Clamping ring (Method B only)
Manufacturer Code:0AM53
Tool Number:IAE 19791
Tool Name:IAE 19791 Clamping ring (Method B only)
Manufacturer Code:0AM53
Tool Number:IAE 19792
Tool Name:IAE 19792 Clamping ring (Method B only)
Manufacturer Code:0AM53
Tool Number:IAE 1R18212
Tool Name:IAE 1R18212 Support ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18321
Tool Name:IAE 1R18321 Turnover stand
Manufacturer Code:0AM53
Tool Number:IAE 1R18412
Tool Name:IAE 1R18412 Turning fixture
Manufacturer Code:0AM53
Tool Number:IAE 1R18413
Tool Name:IAE 1R18413 Turnover stand adaptor
Manufacturer Code:0AM53
Tool Number:IAE 1R18414
Tool Name:IAE 1R18414 Boring bar
Manufacturer Code:0AM53
Tool Number:IAE 1R18415
Tool Name:IAE 1R18415 Pallet
Manufacturer Code:0AM53
Tool Number:IAE 1R18416
Tool Name:IAE 1R18416 Lifting tool
Manufacturer Code:0AM53
Tool Number:IAE 1R18417
Tool Name:IAE 1R18417 Lifting Turnover trunnions
Manufacturer Code:0AM53
Tool Number:IAE 1R18418
Tool Name:IAE 1R18418 Multiflex holder
Manufacturer Code:0AM53
Tool Number:IAE 1R18419
Tool Name:IAE 1R18419 Probe holder
Manufacturer Code:0AM53
Tool Number:IAE 1R18420
Tool Name:IAE 1R18420 Dressing attachment
Manufacturer Code:0AM53
Tool Number:IAE 1R18421
Tool Name:IAE 1R18421 Diamond dresser
Manufacturer Code:0AM53
Tool Number:IAE 1R18422
Tool Name:IAE 1R18422 Support probe bracket
Manufacturer Code:0AM53
Tool Number:IAE 1R18430
Tool Name:IAE 1R18430 Turning holder
Manufacturer Code:0AM53
Tool Number:IAE 1R18431
Tool Name:IAE 1R18431 Lifting beam
Manufacturer Code:0AM53
Tool Number:IAE 1R18503
Tool Name:IAE 1R18503 Machine drawing
Manufacturer Code:0AM53
Tool Number:IAE 1R18661
Tool Name:IAE 1R18661 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18662
Tool Name:IAE 1R18662 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18663
Tool Name:IAE 1R18663 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18664
Tool Name:IAE 1R18664 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18665
Tool Name:IAE 1R18665 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18666
Tool Name:IAE 1R18666 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18667
Tool Name:IAE 1R18667 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18668
Tool Name:IAE 1R18668 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18669
Tool Name:IAE 1R18669 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18670
Tool Name:IAE 1R18670 Containment ring
Manufacturer Code:0AM53
Tool Number:IAE 1R18738
Tool Name:IAE 1R18738 Setting block
Manufacturer Code:0AM53
Tool Number:IAE 1R18739
Tool Name:IAE 1R18739 Setting block
Manufacturer Code:0AM53
Tool Number:IAE 1R18740
Tool Name:IAE 1R18740 Setting block
Manufacturer Code:0AM53
Tool Number:IAE 1R18741
Tool Name:IAE 1R18741 Setting block
Manufacturer Code:0AM53
Tool Number:IAE 1R18760
Tool Name:IAE 1R18760 Grinding head
Manufacturer Code:0AM53
Tool Number:IAE 3R18232
Tool Name:IAE 3R18232 Lifting beam
Manufacturer Code:LOCAL
Tool Number:K Grade I.T.T. Turning Tool
Tool Name:K Grade I.T.T. Turning Tool
Manufacturer Code:LOCAL
Tool Number:Oven
Tool Name:Oven
Manufacturer Code:LOCAL
Tool Number:Vacuum
Tool Name:Vacuum