DMC:V2500-A5-72-41-3000-00A-710A-B|Issue No:004|Issue Date:2019-11-01

Export Control

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

Copyright

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

Applicability

V2500-A5

Common Information

TASK 72-41-30-440-001-C00 HPC Front Case And Vane Assembly - Install The HPC Stage 4 And 5 Rotor Path Rings And Stage 6 Rotor Ring Segments, Assembly-001

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 70-41-01-400-501 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 4 And 5 Rotor Path Rings and Stage 6 Rotor Ring Segments. The subsequent TASKs give the procedure to assemble the HP Compressor front cases.

Measure and then machine the Stage 6 Stator Vanes and the Stage 4 to 6 Rotor Path Rings TASK 72-41-30-440-002-B02 (ASSEMBLY-002).

Install the VIGV TASK 72-41-30-440-003-B00 (ASSEMBLY-003).

Install the Stage 3 VSV TASK 72-41-30-440-004-B00 (ASSEMBLY-004).

Install the Stage 4 VSV TASK 72-41-30-440-005-B00 (ASSEMBLY-005).

Install the Stage 5 VSV TASK 72-41-30-440-006-B00 (ASSEMBLY-006).

Install the Stage 6 Stator Vanes TASK 72-41-30-440-007-B00 (ASSEMBLY-007).

Install the VIGV and the Stage 3 to 5 Bridge Pieces TASK 72-41-30-440-008-B00 (ASSEMBLY-008).

Measure the HP Compressor Front Cases TASK 72-41-30-440-009-B00 (ASSEMBLY-009).

Disassemble the HP Compressor Front Cases TASK 72-41-30-440-010-B00 (ASSEMBLY-010).

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

Name	Manufacturer	Part Number / Identification	Quantity
Inspection table	LOCAL
IAE 1R18204 Location ring	0AM53	IAE 1R18204	2
IAE 1R18207 Support stand	0AM53	IAE 1R18207	1
IAE 1R18694 Drift handle	0AM53	IAE 1R18694	1
IAE 1R19284 Lifting fixture	0AM53	IAE 1R19284	2
IAE 1R19683 Drift front liner	0AM53	IAE 1R19683	1
IAE 1R19684 Drift rear liner	0AM53	IAE 1R19684	1
IAE 1R19694 Assembly tool	0AM53	IAE 1R19694

Consumables, Materials and Expendables

Name	Manufacturer	Part Number / Identification
CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE	LOCAL	CoMat 04-005
CoMat 07-038 AIR DRYING ENAMEL	k3504	CoMat 07-038
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	X333X	CoMat 10-077

Spares

Name	Manufacturer	Part Number / Identification	Quantity	Remark
Stage 6 front liner	LOCAL	Stage 6 front liner	4
Stage 6 rear liner	LOCAL	Stage 6 rear liner	4

Safety Requirements

NONE

Procedure

SUBTASK 72-41-30-220-148 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1221

Refer to Figure.

Reference dimensions at location 1221. 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 1221
Stage 4 Rotor Path Ring HP COMPRESSOR SPLIT CASE(72-41-31, 01-690)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (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 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 1221
Stage 4 Rotor Path Ring HP COMPRESSOR SPLIT CASE (72-41-31, 01-690)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (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 72-41-30-220-149 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1222

Refer to Figure.

Reference dimensions at location 1222. 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 1222
Stage 4 Rotor Path Ring HP COMPRESSOR SPLIT CASE (72-41-31, 01-690)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (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 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 1222
Stage 4 Rotor Path Ring HP COMPRESSOR SPLIT CASE (72-41-31, 01-690)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (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 72-41-30-220-150 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1233

Refer to Figure.

Reference dimensions at location 1233. 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 1233
Stage 5 Rotor Path Ring HP COMPRESSOR SPLIT CASE (72-41-31, 01-695)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (72-41-31, 01-400)
Stage 5 Rotor Path Ring Location Thickness	0.1151
	0.1171	0.002
HP Compressor Front Case Location Slot Width For The Stage 5 Rotor Path Ring	0.1191	0.006
	0.1211

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 1233
Stage 5 Rotor Path Ring HP COMPRESSOR SPLIT CASE (72-41-31, 01-695)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (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 72-41-30-220-151 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1234

Refer to Figure.

Reference dimensions at location 1234. 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 1234
Stage 5 Rotor Path Ring HP COMPRESSOR SPLIT CASE (72-41-31, 01-695)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (72-41-31, 01-400)
Stage 5 Rotor Path Ring Location Thickness	1.6437
	1.6476	0.004
HP Compressor Front Case Location Slot Width For The Stage 5 Rotor Path Ring	1.6516	0.0118
	1.6555

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 1234
Stage 5 Rotor Path Ring HP COMPRESSOR SPLIT CASE (72-41-31, 01-695)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (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 72-41-30-220-152 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1245

Refer to Figure.

Reference dimensions at location 1245. 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 1245
Stage 6 Rotor Ring Segments HP COMPRESSOR SPLIT CASE (72-41-31, 01-705)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (72-41-31, 01-400)
Stage 6 Rotor Ring Segments Location Thickness	0.1101
	0.1121	0.007
HP Compressor Front Case Location Slot Width For The Stage 6 Rotor Ring Segments	0.1191	0.011
	0.1211

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 1245
Stage 6 Rotor Ring Segments HP COMPRESSOR SPLIT CASE (72-41-31, 01-705)
Location In The HP Compressor Front Case HP COMPRESSOR SPLIT CASE (72-41-31, 01-400)
Stage 6 Rotor Ring Segments Location Thickness	2.798
	2.848	0.177
HP Compressor Front Case Location Slot Width For The Stage 6 Rotor Ring Segments	3.025	0.277
	3.075

SUBTASK 72-41-30-220-153 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1246

Refer to Figure.

Reference dimensions at location 1246. 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 1246
Stage 6 Front Liner HP COMPRESSOR SPLIT CASE (72-41-31, 01-710)
Location In The Stage 6 Rotor Ring Segment HP COMPRESSOR SPLIT CASE (72-41-31, 01-705)
Stage 6 Rotor Ring Segment Slot Width	0.1153
	0.1173	0.0000
Stage 6 Front Liner Width	0.1122	0.0051
	0.1153

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 1246
Stage 6 Front Liner HP COMPRESSOR SPLIT CASE (72-41-31, 01-710)
Location In The Stage 6 Rotor Ring Segment HP COMPRESSOR SPLIT CASE (72-41-31, 01-705)
Stage 6 Rotor Ring Segment Slot Width	2.930
	2.980	0.000
Stage 6 Front Liner Width	2.850	0.130
	2.930

SUBTASK 72-41-30-220-154 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1247

Refer to Figure.

Reference dimensions at location 1247. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000) and TASK 72-41-22-200-000 (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 1247
Stage 6 stator vanes HP COMPRESSOR SPLIT CASE (72-41-22, 01-400)
Location In The Stage 6 Front Liner HP COMPRESSOR SPLIT CASE (72-41-31, 01-710)
Stage 6 Front Liner Slot Width	0.0807
	0.0878	0.0020
Stage 6 Stator Vanes Platform Width	0.0756	0.0122
	0.0787

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 1247
Stage 6 Stator Vanes HP COMPRESSOR SPLIT CASE (72-41-22, 01-400)
Location In The Stage 6 Front Liner HP COMPRESSOR SPLIT CASE (72-41-31, 01-710)
Stage 6 Front Liner Slot Width	2.050
	2.230	0.050
Stage 6 Stator Vanes Platform Width	1.920	0.310
	2.000

SUBTASK 72-41-30-220-155 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1248

Refer to Figure.

Reference dimensions at location 1248. 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 1248
Stage 6 Rear Liner HP COMPRESSOR SPLIT CASE (72-41-31, 01-715)
Location In The Stage 6 Rotor Ring Segment (72-41-31, 01-705)
Stage 6 Rotor Ring Segment Slot Width	0.1350
	0.1370	0.0000
Stage 6 Rear Liner Width	0.1319	0.0051
	0.1350

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 1248
Stage 6 Rear Liner HP COMPRESSOR SPLIT CASE (72-41-31, 01-715)
Location In The Stage 6 Rotor Ring Segment HP COMPRESSOR SPLIT CASE (72-41-31, 01-705)
Stage 6 Rotor Ring Segment Slot Width	3.430
	3.480	0.000
Stage 6 Rear Liner Width	3.350	0.130
	3.430

SUBTASK 72-41-30-220-156 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1249

Refer to Figure.

Reference dimensions at location 1249. If required use the data written as a note in TASK 72-41-31-200-000 (INSPECTION-000) and TASK 72-41-22-200-000 (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 1249
Stage 6 Stator Vanes HP COMPRESSOR SPLIT CASE (72-41-22, 01-400)
Location In The Stage 6 Rear Liner HP COMPRESSOR SPLIT CASE (72-41-31, 01-715)
Stage 6 Rear Liner Slot Width	0.1004
	0.1075	0.0020
Stage 6 Stator Vanes Platform Width	0.0953	0.0122
	0.0984

Table 18. 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 1249
Stage 6 Stator Vanes HP COMPRESSOR SPLIT CASE (72-41-22, 01-400)
Location In The Stage 6 Rear Liner HP COMPRESSOR SPLIT CASE (72-41-31, 01-715)
Stage 6 Rear Liner Slot Width	2.550
	2.730	0.050
Stage 6 Stator Vanes Platform Width	2.420	0.310
	2.500

1. Refer to Figure and Figure.
2. Put IAE 1R18204 Location ring half location rings 2 off on to IAE 1R18207 Support stand stand 1 off.
3. 1. Use a suitable hoist and lift a lifter in to position on each HP Compressor half front case rear flange.
  2. Engage the two location pins on the lifter in the boltholes in the split line flanges.
  3. Adjust the six screws and engage them in six boltholes in the rear flange of each HP Compressor half front case.
4. Use a suitable hoist and lift the HP Compressor front half cases on to the half location rings. Align the eight bolt holes in the two half location rings with eight boltholes in the HP Compressor front cases front flanges.
5. Install the eight bolts and washers to attach the HP Compressor front half cases to the half location rings. Tighten the bolts.
6. Remove the two lifters from the HP Compressor front cases rear flanges.
1. Refer to Figure and Figure.
2. SBE 72-0345: Introduction of revised Stage 4 and 5 Rotor path seal ring segments.
3. 1. 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 'A', one must be rejected.
  2. Pre SBE 72-0345: Install one segment of the stage 4 rotor path ring into the upper half HP Compressor front case. Move the segment until the slot in the segment is against the anti-rotation pin.
  3. SBE 72-0345: Install one segment of the Stage 4 Rotor path ring into the upper half HP Compressor front case. Move the segment until the slot in the segment is against the anti-rotation pin.
  4. Install a sealing strip HP COMPRESSOR SPLIT CASE (72-41-31, 01-678) into the slot in the segment at the center of the upper half HP Compressor front case.
  5. Pre SBE 72-0345: Install a second segment of the Stage 4 Rotor path ring into the upper half HP Compressor front case. Engage the sealing strip in the slot in the segment. Make sure the two segments are in line with or below the split line flanges.
  6. SBE 72-0345: Install a second segment of the Stage 4 Rotor path ring into the upper half HP Compressor front case. Engage the sealing strip in the slot in the segment. Make sure the two segments are in line with or below the split line flanges.
  7. Set the clearance between the two segments to the dimensions shown at position A.
4. 1. Install the two segments of the stage 4 rotor path ring and the sealing strip into the lower half HP Compressor front case as given in Step to Step.
1. Refer to Figure.
2. 1. Put the blank in to position in the upper half HP Compressor front case.
  2. Apply a thin layer of CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE on to the face of the bracket HP COMPRESSOR SPLIT CASE (72-41-31, 01-115) that will touch the blank. Locate the bracket on the blank.
  3. Install the two bolts HP COMPRESSOR SPLIT CASE (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).
3. 1. Put the two blanks in to position in the lower half HP Compressor front case.
  2. Locate the bracket HP COMPRESSOR SPLIT CASE (72-41-31, 01-118) on the blank at the 120 degree position.
  3. Install the four bolts HP COMPRESSOR SPLIT CASE (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).
4. 1. Install the blanking plates into position on the upper half and lower half HP Compressor front case.
  2. Install the four bolts HP COMPRESSOR SPLIT CASE (72-41-31, 01-352) to attach the blanking plates to the upper half and lower half HP Compressor front case. Torque the bolts to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm).
1. Refer to Figure and Figure.
2. SBE 72-0345: Introduction of revised Stage 4 And 5 Rotor Path seal ring segments.
3. 1. 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 'A', one must be rejected.
  2. Pre SBE 72-345: Install one segment of the Stage 5 Rotor Path ring into the upper half HP Compressor front case. Move the segment until the slot in the segment is against the anti-rotation pin.
  3. SBE 72-345: Install one segment of the Stage 5 Rotor Path ring into the upper half HP Compressor front case. Move the segment until the slot in the segment is against the anti-rotation pin.
  4. Install a sealing strip HP COMPRESSOR SPLIT CASE (72-41-31, 01-679) into the slot in the segment at the centre of the upper half HP Compressor front case.
  5. Pre SBE 72-345: Install a second segment of the Stage 5 Rotor Path ring into the upper half HP Compressor front case. Engage the sealing strip in the slot in the segment. Make sure the two segments are in line with, or below the split line flanges.
  6. SBE 72-345: Install a second segment of the Stage 5 Rotor Path ring into the upper half HP Compressor front case. Engage the sealing strip in the slot in the segment. Make sure the two segments are in line with, or below the split line flanges.
  7. Set the clearance between the two segments to the dimensions shown at position A.
4. 1. Install the two segments of the stage 5 rotor path ring and the sealing strip in to the lower half HP compressor front case, as given in Step to Step.
1. Refer to Figure and Figure.
2. 1. Use screw C (2 off) to install IAE 1R19683 Drift front liner (1 off) on to IAE 1R18694 Drift handle (1 off). Tighten the two screws.
3. 1. Put the Stage 6 Rotor ring segments front face down on a clean work surface.
  2. Use the IAE 1R19684 Drift rear liner and the IAE 1R19694 Assembly tool to install the stage 6 front liners. Make sure that the liner touches the Stage 6 Rotor ring segment at face A.
4. 1. Put the Stage 6 Rotor ring segments face down on a clean work surface.
  2. Use the liner drift and the drift handle to install the stage 6 rear liners. Make sure that the liner touches the stage 6 rotor ring segment at face B.
1. Refer to Figure, Figure, Figure and Figure.
2. 1. Install one segment of the Stage 6 Rotor ring in to the upper half HP Compressor front case. Move the segment until the slot in the segment is against the anti-rotation stop HP COMPRESSOR SPLIT CASE (72-41-31, 01-720).
  2. Install a sealing strip HP COMPRESSOR SPLIT CASE (72-41-31, 01-680) in to the slot in the segment at the center of the upper half HP Compressor front case.
  3. Install one stage 6 stop vane HPC Stator Vanes (72-41-22, 01-350) into the rotor ring segment at the center position so that the stop on the stop vane touches the segment. The stop vanes have been identified with their position numbers. You must install the correct stop vane. Refer to Figure.
  4. Install a second segment of the stage 6 rotor ring in to the upper half HP Compressor front case. Engage the sealing strip in the slot in the segment. Engage the stop vane installed in Step in the liners in the segment. Make sure the two segments are in line with or below the split line flanges.
  5. Set the clearance between the two segments to the dimensions shown at position A.
3. 1. Install the two segments of the Stage 6 Rotor ring, a stop vane and the sealing strip in to the lower half HP Compressor front case, as given in Step to Step.
4. Remove the eight bolts and washers which attach the HP Compressor front cases to the two location half rings.
1. Refer to Figure.
2. Put the stage 3 stator borescope blank HP COMPRESSOR SPLIT CASE (72-41-31, 01-100) into position in the lower half HP compressor front case.
3. Apply CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) or CoMat 10-070 ANTI-SEIZE COMPOUND to the two bolts HP COMPRESSOR SPLIT CASE (72-41-31, 01-102) which hold the stage 3 borescope blank to the lower half of the HP compressor front case.
4. Install the two bolts HP COMPRESSOR SPLIT CASE (72-41-31, 01-102) which attach the stage 3 stator 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).
5. Put the stage 3 rotor borescope blank HP COMPRESSOR SPLIT CASE (72-41-31, 01-105) into position in the lower half HP compressor front case.
6. Apply CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) or CoMat 10-070 ANTI-SEIZE COMPOUND to the two bolts HP COMPRESSOR SPLIT CASE (72-41-31, 01-107) which attach the stage 3 borescope blank to the lower half of the HP compressor front case.
7. Install the two bolts HP COMPRESSOR SPLIT CASE (72-41-31, 01-107) which attach the stage 3 rotor 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).
1. Refer to Figure.
2. Put the stage 6 borescope blank HP COMPRESSOR SPLIT CASE (72-41-31, 01-140) into position in the lower half HP compressor front case.
3. Pre SBE 72-0265, SBE 72-0317 and SBE 72-0337: Apply CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) or CoMat 10-070 ANTI-SEIZE COMPOUND to the two screws HP COMPRESSOR SPLIT CASE (72-41-31, 01-142) which attach the stage 6 borescope blank to the lower half of the HP compressor front case.
4. SBE 72-0265: Apply CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE) or CoMat 10-070 ANTI-SEIZE COMPOUND to the screw HP COMPRESSOR SPLIT CASE (72-41-31, 01-142) which attach the stage 6 borescope blank to the lower half of the HP compressor front case.
5. SBE 72-0265: Install the screw HP COMPRESSOR SPLIT CASE (72-41-31, 01-142) which attach the stage 6 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).
6. SBE 72-0317 and SBE 72-0337: Install the two screws HP COMPRESSOR SPLIT CASE (72-41-31, 01-142) which attach the stage 6 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).

View through the HP Compressor front case

Locations for the fits and clearances

Install the lifter

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

sheet 1

sheet 2

Stages 4 to 6 rotor path ring anti-rotation pins

Install the stage 4 rotor path ring

Install the stage 5 rotor path ring

Sheet 1

Sheet 2

sheet 1

sheet 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:	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:	X333X
Enterprise Name:	REFER TO V2500 SB ENG-79-0108

Manufacturer Code:	0AM53
Tool Number:	IAE 1R18204
Tool Name:	IAE 1R18204 Location ring

TASK 72-41-30-440-001-C00 HPC Front Case And Vane Assembly - Install The HPC Stage 4 And 5 Rotor Path Rings And Stage 6 Rotor Ring Segments, Assembly-001

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Common Information

TASK 72-41-30-440-001-C00 HPC Front Case And Vane Assembly - Install The HPC Stage 4 And 5 Rotor Path Rings And Stage 6 Rotor Ring Segments, Assembly-001

General

NOTE

Preliminary Requirements

Pre-Conditions

Support Equipment

Consumables, Materials and Expendables

Spares

Safety Requirements

Procedure

SUBTASK 72-41-30-220-148 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1221

SUBTASK 72-41-30-220-149 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1222

SUBTASK 72-41-30-220-150 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1233

SUBTASK 72-41-30-220-151 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1234

SUBTASK 72-41-30-220-152 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1245

SUBTASK 72-41-30-220-153 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1246

SUBTASK 72-41-30-220-154 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1247

SUBTASK 72-41-30-220-155 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1248

SUBTASK 72-41-30-220-156 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1249

SUBTASK 72-41-30-440-127 Install the HP Compressor Front Cases on to the Half Location Rings

SUBTASK 72-41-30-440-130 Install the HP Compressor Stage 4 Rotor Path Ring (Pre SBE 72-0345 and SBE 72-0345)

NOTE

SUBTASK 72-41-30-440-129 Install the Support Tool Blanks and the Blanking Plates

SUBTASK 72-41-30-440-131 Install the HP Compressor Stage 5 Rotor Path Ring (Pre SBE 72-0345 and SBE 72-0345)

NOTE

SUBTASK 72-41-30-440-213 Install the Liners in the Stage 6 Rotor Ring Segments

SUBTASK 72-41-30-440-133 Install the HP Compressor Stage 6 Rotor Ring Segments

NOTE

SUBTASK 72-41-30-440-128 Install the Stage 3 Borescope Blanks

SUBTASK 72-41-30-440-291 Install the Stage 6 Borescope Blanks (Pre SBE 72-0265, SBE 72-0265, Pre SBE 72-0317 and SBE 72-0337 and SBE 72-0317 and SBE 72-0337)

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: Stages 4 to 6 rotor path ring anti-rotation pins

Stages 4 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 Front Liners into the Stage 6 Rotor Ring Segments

Sheet 1

Figure: Install the Rear Liners into the Stage 6 Rotor Ring Segments

Sheet 2

Figure: Install the stage 6 rotor ring segments

sheet 1

Figure: Install the stage 6 rotor ring segments

sheet 2

Requirements After Job Completion

Follow-On Conditions