TASK 72-32-00-430-009-A00 LPC/Intermediate Case Module - Install The LPC Stage 2.5 Vanes, Assembly-009

DMC:V2500-A1-72-32-0000-09A-710A-B|Issue No:002.00|Issue Date:2013-11-01

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-A1

Common Information

TASK 72-32-00-430-009-A00 LPC/Intermediate Case Module - Install The LPC Stage 2.5 Vanes, Assembly-009

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 the SPM TASK 70-41-00-400-501 and TASK 70-41-02-400-501.

Special torque data is identified with the symbol * after the torque value.

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.

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.

The No. 1 strut, which is the top position strut of the fan frame assembly, is identified by the five pressure tubes on the No. 1 strut leading edge.

This TASK gives the procedure to install the LP compressor stage 2.5 vanes.

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 1J13104 Vertical sling0AM53IAE 1J131041

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-124 ISOPROPYL ALCOHOLLOCALCoMat 01-124
CoMat 04-004 JOINTING COMPOUND, LIGHT GRADELOCALCoMat 04-004
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-00-430-126 Turn the Fan Frame Assembly Vertical with the Front End Up

    1. Refer to Figure.

    2. Make sure that the fan frame assembly is installed horizontally on the turnover stand. Refer to TASK 72-32-00-430-008 (ASSEMBLY-008, CONFIG-001).

    3. Release the lock pin from the holes in the handle and the support C of the turnover stand.

    4. Turn the handle to set the fan frame assembly vertical with the front end up.

    5. NOTE

      Make sure that the hole in the support C and one of the eight holes in the handles are aligned. If necessary, turn the handle to make the two holes aligned.

      Install the lock pin into position to lock the handle.

    2. SUBTASK 72-32-00-430-127 Apply Jointing Compound to the Mating Face on the Fan Frame Assembly

    1. Refer to Figure.

    2. Use a clean cloth made moist with CoMat 01-124 ISOPROPYL ALCOHOL to clean the area B on the fan frame assembly.

    3. NOTE

      Do not get the jointing compound to the threaded holes in the clinch nuts in the fan frame assembly.
      Install the LP compressor stage 2.5 vanes onto the mating face before the jointing compound becomes dry.

      Apply CoMat 04-004 JOINTING COMPOUND, LIGHT GRADE to the area B with a stiff brush.

    3. SUBTASK 72-32-00-430-128 Install the LP Compressor Stage 2.5 Vanes (Stage 2.5 Vanes) to the Fan Frame Assembly

    1. Refer to Figure.

    2. Attach a hoist to IAE 1J13104 Vertical sling 1 off.

      3. Install the vertical sling to the stage 2.5 vanes ENGINE-STAGE 2.5 LP COMPRESSOR VANES (72-32-76, 01-400).

      1. Install the three eye bolts (part of the vertical sling) into the three of the 49 clinch nuts of the stage 2.5 vanes. The three eye bolts must be installed at 120 degrees apart from each other.

      2. Connect the vertical sling to the three eye bolts with the three shackles (part of the vertical sling).

    4. Lift and move the stage 2.5 vanes adjacent to the fan frame assembly.

    5. Align the 18 bolt holes in the stage 2.5 vanes with the 18 threaded holes in the fan frame assembly.

    6. Attach the stage 2.5 vanes to the fan frame assembly and safety with 18 bolts (01-675) and washers (01-680).

      7. Remove the vertical sling from the stage 2.5 vanes.

      1. Remove the three shackles which connect the vertical sling to the eye bolts on the stage 2.5 vanes.

      2. Remove the three eye bolts from the clinch nuts of the stage 2.5 vanes.

    8. Remove the hoist from the vertical sling.

    9. Torque the 18 bolts (01-675) to between 85 and 105 lbfin (10.00 and 12.00 Nm).

      10. Attach the stage 2.5 vanes to the ring support of the bleed valve and actuating mechanism.

      1. Attach the stage 2.5 vanes to the ring support with the 25 bushes (01-670) and bolts (01-660).

      2. NOTE

        This torque value is special.

        Torque the bolts to 57 to 63* lbfin (6.48 to 7.08* Nm).

    4. Figure: Install the lock pin into position to lock the handle of the turnover stand

    Install the lock pin into position to lock the handle of the turnover stand

    Figure: Apply jointing compound to the mating faces on the fan frame assembly

    Apply jointing compound to the mating faces on the fan frame assembly

    Figure: Install the LP compressor stage 2.5 vanes

    Install the LP compressor stage 2.5 vanes

    Figure: Install the LP compressor stage 2.5 vanes

    Install the LP compressor stage 2.5 vanes

    Figure: Install the rear fairing onto the LP compressor bleed duct

    Install the rear fairing onto the LP compressor bleed duct

    Figure: Fill the recesses in the rear fairing with cold curing silicone compound

    Fill the recesses in the rear fairing with cold curing silicone compound

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:LOCAL
Supply Number:CoMat 01-124
Type:sp01
Supply Short Name:CoMat 01-124 ISOPROPYL ALCOHOL
Supply Name:CoMat 01-124 ISOPROPYL ALCOHOL
Specification Groups:
Doc NumberType
OMAT:1/40GPR TECHNICAL GRADE
PMC 9094GPR TECHNICAL GRADE
JCR-011GPR TECHNICAL GRADE
Suppliers:
ManufacturerRemarks
LOCAL
U1185
24853
K6835
Manufacturer Code:LOCAL
Supply Number:CoMat 04-004
Type:sp01
Supply Short Name:CoMat 04-004 JOINTING COMPOUND, LIGHT GRADE
Supply Name:CoMat 04-004 JOINTING COMPOUND, LIGHT GRADE
Specification Groups:
Doc NumberType
OMAT: 4/46 (REF RR)HYLOMAR AEROGRADE (PL32), LIGHT GRADE
JCR-025 (JAEC REF)HYLOMAR AEROGRADE (PL32), LIGHT GRADE
MSRR 9055 (RR REF)HYLOMAR AEROGRADE (PL32), LIGHT GRADE
Suppliers:
ManufacturerRemarks
LOCAL
460Y4
CJ731
K3237
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:0AM53
Tool Number:IAE 1J13104
Tool Name:IAE 1J13104 Vertical sling