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 AND PRE SBE 72-0027
Common Information
TASK 72-41-30-440-001-A00 HPC Front Case And Vane Assembly - Install The HPC Stage 3 Through 6 Rotor Path Rings, Assembly-001 - Pre SBE 72-0027
General
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 70-41-00-400-501, SPM TASK 70-41-01-400-501 and SPM TASK 70-41-02-400-501.
Special torque data and assembly tolerances are included in the procedure.
Lubricate all threads and touch faces of nuts and bolts with CoMat 10-077 APPROVED ENGINE OILS, unless other lubricants are referred to in the procedure.
To identify, lubricate and install seal rings, refer to 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 parts used to attach. Use the correct colour of the air drying enamel. Refer to the SPM TASK 70-63-02-380-501.
The number for each radial location must be identified in a clockwise direction. These start at the engine top position when you look from the rear of the engine, unless stated differently in the procedure.
Refer to Figure for a sectional view of the HP Compressor front case.
The Fits and Clearances, NEW PARTS DIMENSIONS and REJECT IF MORE THAN columns will be used by most operators. This permits the full use of the maximum wear allowance and a reduction in the number of parts which are rejected, is possible.
As long as REJECT IF MORE THAN columns do not include reject values, NEW PART DIMENSIONS do not have to be measured before assembly, as there are no reject-if criteria. Values are only valid for new parts, not for worn parts.
The column WORN PART DIMENSION (Non-select) is included for operators who want to have full interchangeability. If this column is used an increase in the number of parts which are rejected is possible.
After the part has been in service for some time the REJECT IF MORE THAN and WORN PART DIMENSIONS could be changed. The operator must tell IAE and if agreed the manual will be changed.
The abbreviation Intf shows an interference or tight fit. This causes REJECT IF MORE THAN to become REJECT IF LESS THAN.
The abbreviation clear shows a clearance fit.
This TASK gives the procedure to install the HP Compressor Stage 3 to 6 Rotor Path Rings pre SBE 72-0027. The subsequent TASKS give the procedure to assemble the HP Compressor front cases.
Install the HP Compressor Stage 5 and 6 Rotor Path Rings SBE 72-0027TASK 72-41-30-440-001-B00 (ASSEMBLY-001).
Measure and then machine the Stage 6 VSV and the Stage 3 to 6 Rotor Path Rings TASK 72-41-30-440-002-A00 (ASSEMBLY-002).
Install the VIGV TASK 72-41-30-440-003-A00 (ASSEMBLY-003).
Install the Stage 3 VSV TASK 72-41-30-440-004-A00 (ASSEMBLY-004).
Install the Stage 4 VSV TASK 72-41-30-440-005-A00 (ASSEMBLY-005).
Install the Stage 5 VSV TASK 72-41-30-440-006-A00 (ASSEMBLY-006).
Install the Stage 6 VSV TASK 72-41-30-440-007-A00 (ASSEMBLY-007).
Install the VIGV and the Stage 3 to 6 Connector Assemblies TASK 72-41-30-440-008-A00 (ASSEMBLY-008) .
Measure the HP Compressor Front Cases TASK 72-41-30-440-009-A00 (ASSEMBLY-009).
Disassemble the HP Compressor Front Cases TASK 72-41-30-440-010-A00 (ASSEMBLY-0010).
Check and Set VSV System with Optimised Build and Setting Clearances - SBE 72-0402TASK 72-41-30-440-011-A00 (ASSEMBLY-0011).
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Inspection table | LOCAL | Inspection table | ||
| IAE 1R18204 Location ring | 0AM53 | IAE 1R18204 | 2 | |
| IAE 1R18207 Support stand | 0AM53 | IAE 1R18207 | 1 | |
| IAE 1R18249 Lifting tool | 0AM53 | IAE 1R18249 | 2 | |
| IAE 1R18202 Support stand | 0AM53 | IAE 1R18202 | 1 | |
| IAE 1R18233 Foot support | 0AM53 | IAE 1R18233 | 1 | |
| IAE 1R18031 Checking fixture | 0AM53 | IAE 1R18031 | 1 | |
| IAE 1R18205 Lifting tool | 0AM53 | IAE 1R18205 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 07-038 AIR DRYING ENAMEL | k3504 | CoMat 07-038 | ||
| CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE | LOCAL | CoMat 04-005 | ||
| CoMat 10-070 ANTI-SEIZE COMPOUND | LOCAL | CoMat 10-070 | ||
| CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) | K6835 | CoMat 10-072 | ||
| CoMat 10-077 APPROVED ENGINE OILS | LOCAL | CoMat 10-077 |
Spares
NONESafety Requirements
NONEProcedure
Refer to Figure.
test.
Reference dimensions at location 1209. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 1. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1209
Stage 3 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-685)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 3 Rotor Path Ring Location Thickness
0.1151
0.1171
0.0019
HP Compressor Front Case Location Slot Width For The Stage 3 Rotor Path Ring
0.1190
0.0059
0.1210
Table 2. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1209
Stage 3 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-685)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 3 Rotor Path Ring Location Thickness
2.925
2.975
0.050
HP Compressor Front Case Location Slot Width For The Stage 3 Rotor Path Ring
3.025
0.150
3.075
SUBTASK 72-41-30-220-051 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1209
Refer to Figure.
test.
Reference dimensions at location 1210. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 3. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1210
Stage 3 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-685)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 3 Rotor Path Ring Width
2.3523
2.3562
0.0078
HP Compressor Front Case Slot Width For The Stage 3 Rotor Path Ring
2.3641
0.0157
2.3681
Table 4. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1210
Stage 3 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-685)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 3 Rotor Path Ring Width
59.75
59.85
0.20
HP Compressor Front Case Slot Width For The Stage 3 Rotor Path Ring
60.05
0.40
60.15
SUBTASK 72-41-30-220-052 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1210
Refer to Figure.
test.
Reference dimensions at location 1221. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 5. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1221
Stage 4 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-690)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 4 Rotor Path Ring Location Thickness
0.1151
0.1171
0.0019
HP Compressor Front Case Location Slot Width For The Stage 4 Rotor Path Ring
0.1190
0.0059
0.1210
Table 6. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1221
Stage 4 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-690)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 4 Rotor Path Ring Location Thickness
2.925
2.975
0.05
HP Compressor Front Case Location Slot Width For The Stage 4 Rotor Path Ring
3.025
0.15
3.075
SUBTASK 72-41-30-220-053 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1221
Refer to Figure.
test.
Reference dimensions at location 1222. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 7. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1222
Stage 4 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-690)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 4 Rotor Path Ring Width
2.1830
2.1870
0.0039
HP Compressor Front Case Slot Width For The Stage 4 Rotor Path Ring
2.1909
0.0118
2.1948
Table 8. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1222
Stage 4 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-690)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 4 Rotor Path Ring Width
55.45
55.55
0.10
HP Compressor Front Case Slot Width For The Stage 4 Rotor Path Ring
55.65
0.30
55.75
SUBTASK 72-41-30-220-054 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1222
Refer to Figure.
test.
Reference dimensions at location 1233. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 9. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1233
Stage 5 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-695)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 5 Rotor Path Ring Location Thickness
0.1151
0.1171
0.0019
HP Compressor Front Case Location Slot Width For The Stage 5 Rotor Path Ring
0.1190
0.0059
0.1210
Table 10. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1233
Stage 5 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-695)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 5 Rotor Path Ring Location Thickness
2.925
2.975
0.050
HP Compressor Front Case Location Slot Width For The Stage 5 Rotor Path Ring
3.025
0.150
3.075
SUBTASK 72-41-30-220-055 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1233
Refer to Figure.
test.
Reference dimensions at location 1234. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 11. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1234
Stage 5 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-695)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 5 Rotor Path Ring Location Thickness
1.6437
1.6476
0.0039
HP Compressor Front Case Location Slot Width For The Stage 5 Rotor Path Ring
1.6515
0.0118
1.6555
Table 12. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1234
Stage 5 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-695)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 5 Rotor Path Ring Location Thickness
41.75
41.85
0.10
HP Compressor Front Case Location Slot Width For The Stage 5 Rotor Path Ring
41.95
0.30
42.05
SUBTASK 72-41-30-220-056 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1234
Refer to Figure.
test.
Reference dimensions at location 1245. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 13. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1245
Stage 6 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 6 Rotor Path Ring Location Thickness
0.1151
0.1171
0.0019
HP Compressor Front Case Location Slot Width For The Stage 6 Rotor Path Ring
0.1190
0.0059
0.1210
Table 14. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1245
Stage 6 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 6 Rotor Path Ring Location Thickness
2.925
2.975
0.050
HP Compressor Front Case Location Slot Width For The Stage 6 Rotor Path Ring
3.025
0.150
3.075
SUBTASK 72-41-30-220-057 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1245
Refer to Figure.
test.
Reference dimensions at location 1246. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 15. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1246
Stage 6 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 6 Rotor Path Ring Width
1.4074
1.4114
0.0039
HP Compressor Front Case Slot Width For The Stage 6 Rotor Path Ring
1.4153
0.0118
1.4192
Table 16. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1246
Stage 6 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 6 Rotor Path Ring Width
35.75
35.85
0.10
HP Compressor Front Case Slot Width For The Stage 6 Rotor Path Ring
35.95
0.30
36.05
SUBTASK 72-41-30-220-058 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1246
Refer to Figure.
test.
Reference dimensions at location 1247. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000).
Table 17. Fits and Clearances (all dimensions are in inches) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1247
Stage 6 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 6 Rotor Path Ring Rear Internal Diameter
0.0938
0.1098
0.0118
HP Compressor Front Case Location Leg Thickness For The Stage 6 Rotor Path Ring
0.0714
0.0383
0.0820
Table 18. Fits and Clearances (all dimensions are in millimeters) NEW PART
WORN PART
DIMENSIONS
DIMENSIONS
PART IDENT
Size
Clearance
Non-select
REJECT IF
MORE THAN
LOCATION 1247
Stage 6 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700)
Location In The HP Compressor Front Case ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-400)
Stage 6 Rotor Path Ring Rear Internal Diameter
2.385
2.790
0.30
HP Compressor Front Case Location Leg Thickness For The Stage 6 Rotor Path Ring
1.815
0.975
2.085
SUBTASK 72-41-30-220-059 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1247
Install IAE 1R18249 Lifting tool 2 off onto the HP Compressor upper and lower half front cases rear flanges.
SUBTASK 72-41-30-440-051 Install the HP Compressor Front Cases onto the Half Location Rings
Refer to Figure.
test.
Put the stage 3 borescope blank ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 1-100) into position in the lower half HP Compressor front case.
Apply CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) or CoMat 10-070 ANTI-SEIZE COMPOUND to the two bolts which attach the stage 3 borescope blank to the lower half of the HP Compressor front case.
Install the two bolts ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 1-102) which attach the stage 3 borescope blank to the lower half HP Compressor front case. Torque the bolts to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm).
Put the stage 5 borescope blank ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-140) into position in the lower half HP Compressor front case.
Apply CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) or CoMat 10-070 ANTI-SEIZE COMPOUND to the two screws which attach the stage 5 borescope blank to the lower half of the HP Compressor front case.
Install the two screws ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31,01-142) which attach the stage 5 borescope blank to the lower half HP Compressor front case. Torque the screws to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm).
SUBTASK 72-41-30-440-052 Install the Stage 3 and 5 Borescope Blanks
Refer to Figure.
Apply a thin layer of CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE onto the face of the bracket ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-115) that will touch the blank. Locate the bracket on the blank.
Apply CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) or CoMat 10-070 ANTI-SEIZE COMPOUND to the two bolts which attach the bracket and the blank to the upper half of the HP Compressor front case.
Install the two bolts ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-122) which attach the bracket and the blank to the upper half HP Compressor front case. Torque the bolts to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm).
test.
Install a support tool blank ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-120) into the upper half HP Compressor front case.
Locate the bracket ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-118) on the blank at the 120 degree position.
Apply CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) or CoMat 10-070 ANTI-SEIZE COMPOUND to the four bolts which attach the bracket and the blanks to the lower half of the HP Compressor front case.
Install the four bolts ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-122) to attach the bracket and the blanks to the lower half HP Compressor front case. Torque the bolts to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm).
Install the two support tool blanks into the lower half HP Compressor front case.
SUBTASK 72-41-30-440-053 Install the Support Tool Blanks
The HP compressor stage 3 rotor path ring that is installed must be a related set.
The segments must be installed, into the HP compressor front case, from the split line flange opposite to the anti-rotation pin.
Examine the identification marks engraved on the two Stage 3 Rotor Path Ring Segments. If one of the segments is marked with the symbol 'A' in triangle, the marked segment must be installed so that the stop face is not in contact with the anti-rotation pin. If the pair of the ring segments are engraved with the symbol, one must be rejected.
Install a sealing strip ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-677) into the slot in the segment at the centre of the upper half HP Compressor front case.
test.
Install the two segments of the stage 3 rotor path ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-685) into the upper half HP Compressor front case.
SUBTASK 72-41-30-440-054 Install the HP Compressor Stage 3 Rotor Path Ring
NOTE
The HP Compressor Stage 4 Rotor Path Ring that is installed must be a related set.
The segments must be installed, into the HP Compressor front case, from the flange opposite to the anti-rotation pin.
Examine the identification marks engraved on the two Stage 4 Rotor Path Ring Segments. If one of the segments is marked with the symbol 'A' in triangle, the marked segment must be installed so that the stop face is not in contact with the anti-rotation pin. If the pair of the ring segments are engraved with the symbol, one must be rejected.
Install a sealing strip ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-678) into the slot in the segment at the center of the upper half HP Compressor front case.
test.
Install the segments of the Stage 4 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-690) into the upper half HP Compressor front case.
SUBTASK 72-41-30-440-055 Install the HP Compressor Stage 4 Rotor Path Ring
NOTE
The HP Compressor Stage 5 Rotor Path Ring that is installed must be a related set.
The segment must be installed, into the HP Compressor front case, from the flange opposite to the anti-rotation pin.
Examine the identification marks engraved on the two Stage 5 Rotor Path Ring Segments. If one of the segments is marked with the symbol 'A' in triangle, the marked segment must be installed so that the stop face is not in contact with the anti-rotation pin. If the pair of the ring segments are engraved with the symbol, one must be rejected.
Install a sealing strip ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-679) into the slot in the segment at the centre of the upper half HP Compressor front case.
test.
Install the segments of the Stage 5 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-695) into the upper half HP Compressor front case.
SUBTASK 72-41-30-440-056 Install the HP Compressor Stage 5 Rotor Path Ring
NOTE
The HP Compressor Stage 6 Rotor Path that is installed must be a related set.
The segments must be installed into the front HP Compressor case, from the flange opposite to the anti-rotation pin.
Examine the identification marks engraved on the two stage 6 rotor path ring segments. If one of the segments is marked with the symbol 'A' in triangle, the marked segment must be installed so that the stop face is not in contact with the anti-rotation pin. If the pair of the ring segments are engraved with the symbol, one must be rejected.
Install a sealing strip ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-680) into the slot in the segment at the center of the upper half HP Compressor front case.
test.
Install the segments of the stage 6 rotor path ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700) into the upper half HP Compressor front case.
SUBTASK 72-41-30-440-057 Install the HP Compressor Stage 6 Rotor Path Ring
NOTE
Refer to: Figure
test.
Install IAE 1R18249 Lifting tool 2 off onto the rear flange of the HP Compressor half cases as given in Step.
Install two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-677) into the slots in the segments at the split line flange, of the Stage 3 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-690).
Install two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-678) into the slots in the segments at the split line flange, of the Stage 4 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-690).
Install two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-679) into the slots in the segments, at the split line flange, of the Stage 5 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-695).
Install two sealing strips ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-680) into the slots in the segments at the split line flange, of the Stage 6 Rotor Path Ring ENGINE-HP COMPRESSOR SPLIT CASES (72-41-31, 01-700).
Install the sealing strips.
Align the HP Compressor front cases split line flanges. Make sure the sealing strips installed in Step. are correctly engaged in the opposite rotor path ring segment.

CAUTION
YOU MUST NOT LET THE BOLTS TURN WHEN YOU INSTALL THEM. THE BOLTS ARE A CLOSE TOLERANCE FIT.Install the two bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-112) and nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-101) at the positions 31 and 13. Install the 30 bolts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-108), spacers ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-104) and nuts ENGINE-SECURING FEATURES-HP COMPRESSOR CASES (72-41-00, 01-102) at the remaining positions. Lightly tighten the nuts.

CAUTION
YOU MUST NOT LET THE BOLTS TURN WHEN YOU TORQUE THE NUTS. THE BOLTS ARE A CLOSE TOLERANCE FIT.Torque the nuts to 180 lbfin to 220 lbfin (20.00 Nm to 25.00 Nm). Refer to Figure for the sequence to torque the nuts.
SUBTASK 72-41-30-440-058 Install the HP Compressor Split Line Flange Bolts
Refer to Figure.
test.
Put IAE 1R18202 Support stand 1 off onto the IAE 1R18233 Foot support 1 off. Install the attachment pin to attach the support stand to the foot assembly.
Attach a suitable hoist to IAE 1R18031 Checking fixture 1 off lifting eyes.
SUBTASK 72-41-30-440-059 Assemble the Checking Fixture, the Support Stand and the Foot Assembly

CAUTION
MAKE SURE ALL THE TOOL FACES AND HP COMPRESSOR FRONT CASE FACES THAT TOUCH ARE CLEAN AND ARE NOT DEFECTIVE.test.
Install IAE 1R18205 Lifting tool 1 off onto the HP Compressor front case rear flange.
SUBTASK 72-41-30-440-060 Install the HP Compressor Front Case on to the Checking Fixture
Figure: View through the HP Compressor front case
View through the HP Compressor front case

Figure: Locations for the fits and clearances
Locations for the fits and clearances

Figure: Install the lifter
Install the lifter

Figure: Install the HP Compressor front cases on to the half location rings
Install the HP Compressor front cases on to the half location rings

Figure: Install the borescope blanks and the support tool blanks
sheet 1

Figure: Install the borescope blanks and the support tool blanks
sheet 2

Figure: Install the stage 3 rotor path ring
Install the stage 3 rotor path ring

Figure: Stages 3 to 6 rotor path ring anti-rotation pins
Stages 3 to 6 rotor path ring anti-rotation pins

Figure: Install the stage 4 rotor path ring
Install the stage 4 rotor path ring

Figure: Install the stage 5 rotor path ring
Install the stage 5 rotor path ring

Figure: Install the stage 6 rotor path ring
Install the stage 6 rotor path ring

Figure: Install the split line flange bolts
Install the split line flange bolts

Figure: Assemble the checking fixture
Assemble the checking fixture

Figure: Install the HP compressor front case on the checking fixture
sheet 1

Figure: Install the HP compressor front case on the checking fixture
sheet 2

