DMC:V2500-A5-72-41-3000-02A-710A-B|Issue No:005|Issue Date:2019-05-01

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 72-41-30-440-003-B00 HPC Front Case And Vane Assembly - Install The Variable Inlet Guide Vanes, Assembly-003

General

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

All of the temporary marks made in this procedure must be removed after completion of this task.

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

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 SPM TASK 70-64-02-640-501.

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 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 Variable Inlet Guide Vanes (VIGV). The subsequent TASKs give the procedure to assemble HP Compressor front cases.

Install the HP Compressor Stage 4 and 5 Rotor Path Rings and Stage 6 Rotor Ring Segments TASK 72-41-30-440-001-C00 (ASSEMBLY-001).

Measure and then machine Stage 6 Stator Vanes and the Stage 4, 5 and 6 Rotor Path Rings TASK 72-41-30-440-002-B01 (ASSEMBLY-002).

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).

Check and Set VSV System with Optimised Build and Setting Clearances - SBE 72-0400TASK 72-41-30-440-011-B00 (ASSEMBLY-011).

NOTE

To identify the consumable materials refer to the PCI.

NOTE

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

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

Name	Manufacturer	Part Number / Identification	Quantity	Remark
IAE 1R18248 Rigging pin	0AM53	IAE 1R18248	2
IAE 1R18638 Rigging pin	0AM53	IAE 1R18638	2
IAE 1R18250 Split ring assembly	0AM53	IAE 1R18250	1
IAE 1R18260 Bushing assembly tool	0AM53	IAE 1R18260	1
IAE 1R18295 Bushing assembly tool	0AM53	IAE 1R18295	1
IAE 1R18423 Rigging pin	0AM53	IAE 1R18423	4
IAE 1R18892 Rigging pin	0AM53	IAE 1R18892	4
IAE 1R19633 Split ring assembly	0AM53	IAE 1R19633	1
IAE 1R18579 Pusher installation tool	0AM53	IAE 1R18579		(alternative to IAE 1R18260)
IAE 1R18576 Pusher installation tool	0AM53	IAE 1R18576		(alternative to IAE 1R18260)
IAE 1R18577 Bushing installation tool	0AM53	IAE 1R18577		(alternative to IAE 1R18260 and IAE 1R18295)
IAE 1R18573 Cylinder, hydraulic	0AM53	IAE 1R18573		(alternative to IAE 1R18260 and IAE 1R18295)
IAE 1R18582 Pusher installation tool	0AM53	IAE 1R18582		(alternative to IAE 1R18295)
IAE 1R19633 Split ring assembly	0AM53	IAE 1R19633

Consumables, Materials and Expendables

Name	Manufacturer	Part Number / Identification
CoMat 02-363 MARKING PEN	LOCAL	CoMat 02-363
CoMat 04-007 SILICONE GREASE	LOCAL	CoMat 04-007
CoMat 07-038 AIR DRYING ENAMEL	k3504	CoMat 07-038
CoMat 10-077 APPROVED ENGINE OILS	X333X	CoMat 10-077
CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R)	LOCAL	CoMat 10-108

Spares

NONE

Safety Requirements

NONE

Procedure

SUBTASK 72-41-30-220-157 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1201

Refer to Figure.

Reference dimensions at location 1201. If required use the data written as a note in TASK 72-41-32-200-000 and TASK 72-41-31-200-000.

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 1201
VIGV HPC Variable Stator Vanes (72-41-32, 01-500 And 01-600)
Spindle Location In The VIGV Bush HP COMPRESSOR SPLIT CASE (72-41-31, 01-244)
VIGV Spindle Diameter	0.5472
	0.5493	0.0027
VIGV Bush Bore	0.5520	0.0063
	0.5535

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 1201
VIGV HPC Variable Stator Vanes (72-41-32, 01-500 And 01-600)
Spindle Location In The VIGV Bush HP COMPRESSOR SPLIT CASE (72-41-31, 01-244)
VIGV Spindle Diameter	13.900
	13.952	0.070
VIGV Bush Bore	14.022	0.160
	14.060

SUBTASK 72-41-30-220-158 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1205

Refer to Figure.

Reference dimensions at location 1205. If required use the data written as a note in TASK 72-41-32-200-000 and TASK 72-41-33-200-000.

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 1205
VIGV HPC Variable Stator Vanes (72-41-32, 01-500 And 01-600)
Spindle Location In The Half Bush HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-190)
VIGV Spindle Diameter	0.2709
	0.2730	0.0026
Half Bush Bore	0.2756	0.0056
	0.2765

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 1205
VIGV HPC Variable Stator Vanes (72-41-32, 01-500 And 01-600)
Spindle Location In The Half Bush HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-190)
VIGV Spindle Diameter	6.881
	6.933	0.067
Half Bush Bore	7.000	0.141
	7.022

SUBTASK 72-41-30-220-159 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1206

Refer to Figure.

Reference dimensions at location 1206. If required use the data written as a note in TASK 72-41-32-200-000 and TASK 72-41-33-200-000.

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 1206
VIGV HPC Variable Stator Vanes (72-41-32, 01-500 And 01-600)
Inner Spindle Location In The Half Bush HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-190)
VIGV Inner Spindle Length	5.1440
	5.1520	0.015
Half Bush Outer Length	5.1670	0.0236
	5.1677

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 1206
VIGV HPC Variable Stator Vanes (72-41-32, 01-500 And 01-600)
Inner Spindle Location In The Half Bush HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-190)
VIGV Inner Spindle Length	130.660
	130.856	0.384
Half Bush Outer Length	131.240	0.600
	131.260

SUBTASK 72-41-30-220-160 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1208

Refer to Figure.

Reference dimensions at location 1208. If required use the data written as a note in TASK 72-41-32-200-000 and TASK 72-41-33-200-000.

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 1208
VIGV HPC Variable Stator Vanes (72-41-32, 01-500 And 01-600)
Inner Spindle Location In The Half Bush HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-190)
VIGV Iinner Spindle Length	5.8780
	5.8820	0.0117
Half Bush Outer Length	5.8612	0.0205
	5.8664

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 1208
VIGV HPC Variable Stator Vanes (72-41-32, 01-500 And 01-600)
Inner Spindle Location In The Half Bush HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-190)
VIGV inner spindle length	149.303
	149.399	0.297
Half Bush Outer Length	148.876	0.523
	149.006

SUBTASK 72-41-30-220-161 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1301

Refer to Figure.

Reference dimensions at location 1301. If required use the data written as a note in TASK 72-41-34-200-000.

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 1301
VIGV Lever HPC Variable Stator Vane Actuation System (72-41-34, 02-100 And 02-140)
Location In The Bush HPC Variable Stator Vane Actuation System (72-41-34, 02-460 And 02-560)
VIGV Lever Pin Diameter	0.2353
	0.2358	0.0004
Bush Inner Bore	0.2362	0.0016
	0.2369

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 1301
VIGV Lever HPC Variable Stator Vane Actuation System (72-41-34, 02-100 And 02-140)
Location In The Bush HPC Variable Stator Vane Actuation System (72-41-34, 02-460 And 02-560)
VIGV Lever Pin Diameter	5.978
	5.990	0.01
Bush Inner Bore	6.000	0.04
	6.018

SUBTASK 72-41-30-220-162 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1263

Refer to Figure.

Reference dimensions at location 1263. If required use the data written as a note in TASK 72-41-30-200-000 and TASK 72-41-31-200-000.

Table 11. Fits and Clearances (all dimensions in inches)
	NEW PART		WORN PART
	DIMENSIONS		DIMENSIONS
PART IDENT	Size	Clearance	Non-select	REJECT IF MORE THAN
LOCATION 1263
VIGV Bush HP COMPRESSOR SPLIT CASE (72-41-31, 01-244)
Location With The Sealing Washer ENGINE-HP COMPRESSOR FRONT CASES AND VANES (72-41-30, 01-100)
VIGV Bush Inner Flange Thickness	0.0546
	0.0576	0.003
Sealing Washer Thickness	0.0492	0.0084
	0.0516

Table 12. Fits and Clearances (all dimensions in millimetres)
	NEW PART		WORN PART
	DIMENSIONS		DIMENSIONS
PART IDENT	Size	Clearance	Non-select	REJECT IF MORE THAN
LOCATION 1263
VIGV Bush HP COMPRESSOR SPLIT CASE (72-41-31, 01-244)
Location With The Sealing Washer ENGINE-HP COMPRESSOR FRONT CASES AND VANES (72-41-30, 01-100)
VIGV Bush Inner Flange Thickness	1.387
	1.463	0.077
Sealing Washer Thickness	1.250	0.213
	1.310

SUBTASK 72-41-30-220-163 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1359

Refer to Figure.

Reference dimensions at location 1359. If required use the data written as a note in TASK 72-41-34-200-000.

Table 13. Fits and Clearances (all dimensions in inches)
	NEW PART		WORN PART
	DIMENSIONS		DIMENSIONS
PART IDENT	Size	Clearance	Non-select	REJECT IF MORE THAN
LOCATION 1359
Upper VIGV Acutating Ring HPC Variable Stator Vane Actuation System (72-41-34, 02-440)
Location With The Spacer HPC Variable Stator Vane Actuation System (72-41-34, 02-786)
Upper VIGV Actuating	0.5512	Intf
Ring Spacer Hole Bore	0.5522	0.0009
Spacer Diameter	0.5517	clear
	0.5521	0.0005

Table 14. Fits and Clearances (all dimensions in millimetres)
	NEW PART		WORN PART
	DIMENSIONS		DIMENSIONS
PART IDENT	Size	Clearance	Non-select	REJECT IF MORE THAN
LOCATION 1359
Upper VIGV Actuating RingHPC Variable Stator Vane Actuation System (72-41-34, 02-440)
Location With The Spacer HPC Variable Stator Vane Actuation System (72-41-34, 02-786)
Upper VIGV Actuating	14.000	Intf
Ring Spacer Hole Bore	14.027	0.023
Spacer Diameter	14.012	clear
	14.023	0.015

SUBTASK 72-41-30-220-164 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1360

Refer to Figure.

Reference dimensions at location 1360. If required use the data written as a note in TASK 72-41-34-200-000.

Table 15. Fits and Clearances (all dimensions in inches)
	NEW PART		WORN PART
	DIMENSIONS		DIMENSIONS
PART IDENT	Size	Clearance	Non-select	REJECT IF MORE THAN
LOCATION 1360
VIGV Rig Pin Bracket HPC Variable Stator Vane Actuation System (72-41-34, 02-780)
Location With The Spacer HPC Variable Stator Vane Actuation System (72-41-34, 02-786)
VIGV Rig Pin Bracket Spacer Hole Bore	0.3150	Intf
	0.3158	0.0007
Spacer Diameter	0.3154	clear
	0.3157	0.0004

Table 16. Fits and Clearances (all dimensions in millimetres)
	NEW PART		WORN PART
	DIMENSIONS		DIMENSIONS
PART IDENT	Size	Clearance	Non-select	REJECT IF MORE THAN
LOCATION 1360
VIGV Rig Pin Bracket HPC Variable Stator Vane Actuation System (72-41-34, 02-780)
Location With The Spacer HPC Variable Stator Vane Actuation System (72-41-34, 02-786)
VIGV Rig Pin Bracket Spacer Hole Bore	8.000	Intf
	8.022	0.019
Spacer Diameter	8.010	clear
	8.019	0.012

1. Refer to Figure.
2. SBE 72-0385 or SBE 72-0416: Introduction of revised actuating rings with increased dowel locations.
3. 1. Put the two centralizing actuating housings in to position in the upper VIGV actuating ring.
  2. Install the four bolts HPC Variable Stator Vane Actuation System (72-41-34, 02-682) and washers HPC Variable Stator Vane Actuation System (72-41-34, 02-684) to attach the two centralizing actuating housings to the upper VIGV actuating ring.
  3. Tighten the bolts.
4. 1. Do Step to Step to install the two centralizing actuating housings in to the lower VIGV actuating ring.
5. 1. Put the two spacers HPC Variable Stator Vane Actuation System (72-41-34, 02-786) through the two boltholes at the location identified C.
  2. Locate the rig pin location bracket on to the spacers.
  3. Install the two bolts HPC Variable Stator Vane Actuation System (72-41-34, 02-784) and nuts HPC Variable Stator Vane Actuation System (72-41-34, 02-782) to attach the bracket to the upper VIGV actuating ring. Make sure the bolt heads are correctly located against the bracket.
  4. Torque the two nuts to 36 lbfin to 45 lbfin (4.00 Nm to 5.00 Nm).
1. SBE 70-0984: Information - Engine - HP Compressor Variable Stator Split Cases - VSV bushes of new material.
2. Refer to Figure.
  NOTE
  Old and new parts (SBE 70-0984 standard) are not interchangeable. All new parts (SBE 70-0984 standard) must be installed as a set.
3. 1. Use IAE 1R18295 Bushing assembly tool 1 off to install the bushes. Refer to detail A on Figure.
  2. Remove the ring, handle, spacer and nylon washer B from the tool pin.
  3. Install the pin with the nylon washer A in to the VIGV bush location at the No. 1 position. Make sure the nylon washer is correctly located on the HP Compressor front case outer surface.
  4. Locate the bush that is to be installed on the pin on the inside of the HP Compressor front case.
  5. Install the nylon washer B, spacer, ring and handle on to the pin. Turn the handle until the nylon washer B abuts the bush that is to be installed.
  6. Make sure the bush assembly tool is correctly located and is at 90 degrees to the location bore.
  7. Hold the dowel, then continue to turn the handle to install the bush. Do not let the dowel turn.
  8. When the bush is installed remove the bush assembly tool.
  9. Do Step to Step to install the remaining 39 inner bushes.
4. 1. Use IAE 1R18260 Bushing assembly tool 1 off to install the bushes. Refer to detail B on Figure.
  2. Remove the ring, handle, spacer and nylon washer B from the tool pin.
  3. Locate the bush that is to be installed on to the nylon washer A.
  4. Install the pin, nylon washer A and the bush in to the VIGV location at the No. 1 position. Make sure the bush is correctly located.
  5. Install the nylon washer B, spacer, handle and ring removed in Step.
  6. Turn the handle until the nylon washer B touches the inner bush.
  7. Make sure the bush assembly tool is correctly located and is at 90 degrees to the location bore.
  8. Hold the dowel, then continue to turn the handle to install the bush. Do not let the dowel turn.
  9. When the bush is installed remove the bush assembly tool.
  10. Do Step to Step to install the remaining 39 outer bushes.
1. SBE 70-0984: Information - Engine - HP Compressor Variable Stator Split Cases - VSV bushes of new material.
2. Refer to Figure.
  NOTE
  Old and new parts (SBE 70-0984 standard) are not interchangeable. All new parts (SBE 70-0984 standard) must be installed as a set.
3. 1. Use the correct installation tool.
    For the VIGV long vane bushes HPC Variable Stator Vanes (72-41-32, 01-500) use IAE 1R18579 Pusher installation tool 1 off. Refer to detail A on Figure.
    For the VIGV short vane bushes HPC Variable Stator Vanes (72-41-32, 01-600) use IAE 1R18576 Pusher installation tool 1 off. Refer to detail B on Figure.
  2. Install the pusher in the VIGV bush location at the No. 1 position. Make sure the pusher is correctly located on the HP Compressor front case outer surface.
  3. Put the bush on the pusher on the inside of the HP Compressor front case.
  4. Install the IAE 1R18577 Bushing installation tool 1 off, on the pusher.
  5. Install the IAE 1R18573 Cylinder, hydraulic 1 off, on the pusher until the cylinder comes against the bush installation.
  6. CAUTION
    YOU MUST MAKE SURE THE ASSEMBLY TOOL IS CORRECTLY LOCATED AT 90 DEGREES TO THE LOCATION BORE TO PREVENT DAMAGE TO THE HP COMPRESSOR FRONT CASE.
    Apply hydraulic pressure to the cylinder until the bush is pushed into the Compressor Case.
  7. Release the hydraulic pressure and remove the assembly tool.
  8. Do Step to Step again to install the remaining 39 inner bushes.
4. 1. Use the IAE 1R18582 Pusher installation tool 1 off to install the bushes for the VIGV long and short vanes. Refer to detail B on Figure.
  2. Put the bush on the pusher and install the pusher in the VIGV bush location at the No. 1 position. Make sure the bush is correctly located.
  3. Install the IAE 1R18577 Bushing installation tool on the pusher.
  4. Install the IAE 1R18573 Cylinder, hydraulic on the pusher until the cylinder comes against the bush installation.
  5. CAUTION
    YOU MUST MAKE SURE THE ASSEMBLY TOOL IS CORRECTLY LOCATED AT 90 DEGREES TO THE LOCATION BORE TO PREVENT DAMAGE TO THE COMPRESSOR CASE.
    Apply hydraulic pressure to the cylinder until the bush is pushed into the HP Compressor Case.
  6. Release the hydraulic pressure and remove the assembly tool.
  7. Do Step to Step again to install the remaining 39 outer bushes.
1. Refer to Figure, Figure, Figure, Figure and Figure.
2. Pre SBE 72-0400: It is not necessary to lubricate the VIGV locations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) during this SUBTASK.
3. SBE 72-0400: Lubricate the VIGV locations during these assembly operations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) as specified in TASK 72-41-30-440-011-B00, SUBTASK 72-41-30-440-211.
4. Install the 40 sealing washers ENGINE-HP COMPRESSOR FRONT CASES AND VANES (72-41-30, 01-100) on the inner bushes. Make sure the sealing washers are correctly located around the inner bush.
5. 1. Temporary mark vane sequence number on each vane before it is installed.
    NOTE
    Do not vibropeen.
    Use CoMat 02-363 MARKING PEN.
    Refer to SPM TASK 70-09-01-400-501.
  2. NOTE
    Install the two guide vanes HPC Variable Stator Vanes (72-41-32, 01-600) at the positions 10 and 11.
    Install the 18 guide vanes HPC Variable Stator Vanes (72-41-32, 01-500) and the two guide vanes HPC Variable Stator Vanes (72-41-32, 01-600) in to the bushes.
6. Install the guide vanes in the lower half HP Compressor front case.
  Install the 20 guide vanes HPC Variable Stator Vanes (72-41-32, 01-500) as given in Step and Step.
  NOTE
  There are no short spindled guide vanes installed in the lower half HP Compressor front case.
7. 1. Put two spacers HPC Variable Stator Vane Actuation System (72-41-34, 02-060) on the spindle of each guide vane.
  2. Install the 40 guide vane actuating levers on the spindles of the Guide Vanes and in to their locations in the actuating ring.
    The two actuating levers HPC Variable Stator Vane Actuation System (72-41-34, 02-140) go at the positions 10 and 11.
    The eight actuating levers HPC Variable Stator Vane Actuation System (72-41-34, 02-120) go at the positions 1, 2, 19, 20, 21, 22, 39 and 40.
    The 30 actuating levers HPC Variable Stator Vane Actuation System (72-41-34, 02-100) go at the positions 3 to 9, 12 to 18 and 23 to 38.
    NOTE
    The guide vane actuating levers must be parallel with the casing center line when you torque the nuts. This is the null position.
  3. Pre SBE 72-0486: Install the 40 slave nuts to attach the actuating levers to the Guide Vanes. Torque the nuts to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm). The nuts that are used must have no run down torque.
    NOTE
    The guide vane actuating levers must be parallel with the casing center line when you torque the nuts. This is the null position.
  4. SBE 72-0486: Install the 40 bolts to attach the actuating levers to the Guide Vanes. Torque the bolts to 100 lbfin (11.5 Nm) plus the run down torque.
  5. At each guide vane apply a load at the inner pivot point, to push the guide vane radially out.
  6. Measure and write down a record of the end float, dimension A. Measure between the actuating lever and the specified spacers.
    NOTE
    Temporarily mark the actuating levers with their position numbers. These must be the same as the numbers on the Guide Vanes location.
  7. Pre SBE 72-0486: Remove the 40 slave nuts and actuating levers from the Guide Vanes.
    NOTE
    Temporarily mark the actuating levers with their position numbers. These must be the same as the numbers on the Guide Vanes location.
  8. SBE 72-0486: Remove the 40 bolts and actuating levers from the Guide Vanes.
  9. Pre SBE 72-0486: Install the 40 slave nuts on to the guide vane spindles. Tighten the slave nuts sufficiently to keep the spacers on the guide vane spindles.
  10. SBE 72-0486: Install the 40 bolts on to the guide vane spindles. Tighten the bolts sufficiently to keep the spacers on the guide vane spindles.
1. Refer to Figure, Figure, Figure, Figure and Figure.
2. Pre SBE 72-0400:
  It is not necessary to lubricate the VIGV locations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) during this SUBTASK.
3. SBE 72-0400:
  Lubricate the VIGV locations during these assembly operations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) as specified in TASK 72-41-30-440-011-B00, SUBTASK 72-41-30-440-211.
4. 1. Put the upper guide vane actuating ring in to position on the upper half HP Compressor front case.
    NOTE
    Set the upper guide vane actuating ring adjacent to the guide vanes at the positions 3 to 18.
  2. Install two of IAE 1R18423 Rigging pin 4 off or IAE 1R18892 Rigging pin 4 off. Install one of IAE 1R18248 Rigging pin 2 off or IAE 1R18638 Rigging pin 2 off to attach the actuating ring to the HP compressor front case at the positions X.
  3. Pre SBE 72-0486:
    Remove the 16 slave nuts from the guide vanes at the positions 3 to 18.
  4. SBE 72-0486:
    Remove the 16 bolts from the guide vanes at the positions 3 to 18.
  5. Remove the two spacers from the spindle of each guide vane.
  6. Install two spacers HPC Variable Stator Vane Actuation System (72-41-34, 02-060) to HPC Variable Stator Vane Actuation System (72-41-34, 02-078) on to the spindle of each guide vane at the positions 3 to 18. The thickness of the spacers that are installed are equal to:
    the removed spacer thickness + the end float - 0.003 in. to 0.005 in. (0.08 mm to 0.13 mm).
    Write down a record of the thickness of the spacers that are installed.
  7. Install the actuating levers HPC Variable Stator Vane Actuation System (72-41-34, 02-100) and HPC Variable Stator Vane Actuation System (72-41-34, 02-140). Make sure the correct actuating lever goes on the correct guide vane at the positions 3 to 18.
  8. Pre SBE 72-0486:
    Install the 16 nuts HPC Variable Stator Vane Actuation System (72-41-34, 02-103) and HPC Variable Stator Vane Actuation System (72-41-34, 02-143) on to the guide vanes at the positions 3 to 18.
  9. SBE 72-0486:
    Install the 16 bolts HPC Variable Stator Vane Actuation System (72-41-34, 02-102) and HPC Variable Stator Vane Actuation System (72-41-34, 02-140) on to the guide vanes at the positions 3 to 18.
  10. Remove the three rigging pins and set the guide vane levers at the null position.
  11. Pre SBE 72-0486:
    Torque the nuts to 85 lbfin to 105 lbfin (10.00 Nm to 12.00 Nm) plus the run down torque.
  12. SBE 72-0486:
    Torque the bolts to 100 lbfin (11.5 Nm) plus the run down torque.
  13. Measure the guide vane end float at the positions 3 to 18. Make sure it is 0.003 in. to 0.005 in. (0.08 mm to 0.13 mm).
5. 1. Install the lower guide vane actuating ring on to the lower half HP Compressor front case at the guide vane positions 23 to 38. Use the procedure given in Step to Step.
  2. To attach the actuating ring to the lower half HP compressor front case use the other two of IAE 1R18423 Rigging pin 4 off or IAE 1R18892 Rigging pin 4 off. Install one of IAE 1R18248 Rigging pin 2 off or IAE 1R18638 Rigging pin 2 off.
1. Refer to Figure.
2. SBE 72-0400: HP Compressor variable vanes - Inlet Guide Vane and Stages 3 to 5 with optimised build and setting instructions.
  SBE 72-0410: HP Compressor variable inner shrouds - Introduction of revised one piece bushes
3. Pre SBE 72-0400 : It is not necessary to lubricate the VIGV locations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) during this SUBTASK.
4. SBE 72-0400 : Lubricate the VIGV locations during these assembly operations with CoMat 10-108 HIGH PERFORMANCE PENETRATING LUBRICANT WITH TEFLON (R) as specified in TASK 72-41-30-440-011-B00, SUBTASK 72-41-30-440-211.
5. 1. Pre SBE 72-0410: Apply a thin layer of CoMat 04-007 SILICONE GREASE to the 20 half bushes HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-190) outer surface.
  2. SBE 72-0410: Apply a thin layer of CoMat 04-007 SILICONE GREASE to the 20 bushes HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-190) outer surface.
    NOTE
    The rear upper half of the Guide Vane half shroud has four location dowels.
  3. Pre SBE 72-0410: Install the 20 half bushes in to the rear upper half of the guide vane half shroud HPC Variable Stator Vane Shrouds And Related Part (72-41-33, 01-200).
    NOTE
    The rear upper half of the guide vane half shroud has four location dowels.
  4. SBE 72-0410: Install the 20 bushes onto the Stator Vanes.
  5. Pre SBE 72-0410: Install the guide vanes half shroud and half bushes on to the rear of the guide vanes at the inner pivot point.
  6. SBE 72-0410: Install the guide vanes half shroud on to the rear of the guide vanes at the inner pivot point.
  7. Pre SBE 72-0410: Install one half of IAE 1R18250 Split ring assembly split ring assembly on to the front of the guide vanes at the inner pivot point.
  8. SBE 72-0410: Install one half of IAE 1R19633 Split ring assembly split ring assembly on to the front of the guide vanes at the inner pivot point.
  9. Install the three bolts and nuts, part of the split ring assembly, to attach the split ring assembly to the guide vane half shroud.
  10. Tighten the nuts.
6. 1. Install the rear lower half of the guide vane half shroud and split ring assembly as given in Step to Step.

View through the HP compressor front cases

Locations for the fits and clearances

Install the centralizing actuating housings

Sheet 1

Sheet 2

Position for the variable inlet guide vanes

Sheet 1

Sheet 2

Sheet 1

Sheet 2

The positions for the rigging pins

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:	LOCAL
Enterprise Name:	LOCALLY SUPPLIED

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

Manufacturer Code:	0AM53
Tool Number:	IAE 1R18248
Tool Name:	IAE 1R18248 Rigging pin

TASK 72-41-30-440-003-B00 HPC Front Case And Vane Assembly - Install The Variable Inlet Guide Vanes, Assembly-003

Export Control

Copyright

Applicability

Common Information

TASK 72-41-30-440-003-B00 HPC Front Case And Vane Assembly - Install The Variable Inlet Guide Vanes, Assembly-003

General

NOTE

NOTE

Preliminary Requirements

Pre-Conditions

Support Equipment

Consumables, Materials and Expendables

Spares

Safety Requirements

Procedure

SUBTASK 72-41-30-220-157 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1201

SUBTASK 72-41-30-220-158 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1205

SUBTASK 72-41-30-220-159 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1206

SUBTASK 72-41-30-220-160 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1208

SUBTASK 72-41-30-220-161 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1301

SUBTASK 72-41-30-220-162 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1263

SUBTASK 72-41-30-220-163 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1359

SUBTASK 72-41-30-220-164 Reference Fits and Clearances of the HP Compressor Front Cases and Vanes at Location 1360

SUBTASK 72-41-30-440-137 Assemble the VIGV Actuating Rings (Pre SBE 72-0385 or SBE 72-0416 and SBE 72-0385 or SBE 72-0416)

SUBTASK 72-41-30-440-138-001 Install the VIGV Spindle Bushes using IAE 1R18260 and IAE 1R18295 Bush Assembly Tools (Pre SBE 70-0984 and SBE 70-0984)

NOTE

SUBTASK 72-41-30-440-138-002 Install the VIGV Spindle Bushes using IAE 1R18579, IAE 1R18576, IAE 1R18577, IAE 1R18573 and IAE 1R18582 Bush Assembly Tools (Pre SBE 70-0984 and SBE 70-0984)

NOTE

CAUTION

CAUTION

SUBTASK 72-41-30-440-139 Install the VIGV in the HP Compressor Front Case (Pre SBE 72-0486, SBE 72-0486, Pre SBE 72-0400, SBE 72-0400, Pre SBE 72-0385 or SBE 72-0416 and SBE 72-0385 or SBE 72-0416)

NOTE

NOTE

NOTE

NOTE

NOTE

NOTE

NOTE

SUBTASK 72-41-30-440-140 Install the VIGV Upper and Lower Actuating Rings (Pre SBE 72-0486, SBE 72-0486, Pre SBE 72-0400, SBE 72-0400, Pre SBE 72-0385 or SBE 72-0416 and SBE 72-0385 or SBE 72-0416)

NOTE

NOTE

SUBTASK 72-41-30-440-141 Install the VIGV Shroud (Pre SBE 72-0400, SBE 72-0400, Pre SBE 72-0410 and SBE 72-0410)

NOTE

NOTE

NOTE

Figure: View through the HP compressor front cases

View through the HP compressor front cases

Figure: Locations for the fits and clearances

Locations for the fits and clearances

Figure: Install the centralizing actuating housings

Install the centralizing actuating housings

Figure: Tools to install the spindle location bushes

Sheet 1

Figure: Tools to install the spindle location bushes

Sheet 2

Figure: Position for the variable inlet guide vanes

Position for the variable inlet guide vanes

Figure: Pre SBE 72-0486: Install the Variable Inlet Guide Vanes

Sheet 1

Figure: SBE 72-0486: Install the Variable Inlet Guide Vanes

Sheet 2

Figure: Pre SBE 72-0486: Measure the Guide Vane End Float

Sheet 1

Figure: SBE 72-0486: Measure the Guide Vane End Float

Sheet 2

Figure: The positions for the rigging pins

The positions for the rigging pins

Requirements After Job Completion

Follow-On Conditions