TASK 72-00-40-050-001-C00 HP System Module Components - Remove The Variable Stator Vane (VSV) Actuator, Removal-010 - SBE 72-0564 (SelectOne Production Standard), Removal-010

DMC:V2500-A5-72-00-4050-00C-520A-B|Issue No:001.00|Issue Date:2014-05-01

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 and Post SBE 72-0564

Common Information

TASK 72-00-40-050-001-C00 HP System Module Components - Remove The Variable Stator Vane (VSV) Actuator, Removal-010 - SBE 72-0564 (SelectOne Production Standard), Removal-010

General

This task gives the procedure for removal of the Variable Stator Vane (VSV) Actuator only for engines, which have SBE 72-0564 (SelectOne Production Standard) incorporated.

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.

Apply the approved CoMat 10-058 PENETRATING OIL before the removal of threaded parts. Let the parts soak before removal.

Remove and discard the lockwire before the tube or connector is disconnected.

When electrical connections are disconnected, special plastic caps must be installed.

Seal all openings to prevent contamination from unwanted materials.

Discard all rubber seal rings removed in this procedure.

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 1R18254 Rigging pin0AM53IAE 1R182541

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 06-086 TIES18992CoMat 06-086
CoMat 10-058 PENETRATING OIL0AM53CoMat 10-058

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-40-050-061 Disconnect the Electrical Connectors from the VSV Actuator

    1. Refer to Figure and Figure.

    2. Disassemble and remove the bolts, the clips, the nuts and the washers which attach the electrical connectors together at the bracket. Remove and discard the lockwire at the bracket, refer to the view at A.

    3. Disconnect the electrical connectors 4022KS-A, 4022KS-B, 4022KS-C and temporarily tie them clear of the actuator with CoMat 06-086 TIES.

    2. SUBTASK 72-00-40-050-062 Remove the VSV Actuator

      NOTE

      Some fuel leakage could occur during this procedure. It is recommended that an applicable container be available.

    1. Refer to Figure, Figure, Figure and Figure.

    2. Disconnect the two fuel servo tubes (44 and 46) from the VSV actuator and remove the two packings.

    3. Disconnect the fuel drain tube (47) from the VSV actuator.

    4. Remove the bolts, washers and clipnuts from the clip positions 5745 and 5746.

      5. Remove the VSV actuator.

      1. Move the VSV actuating mechanism to the high speed position.

      2. Install IAE 1R18254 Rigging pin 1 off through the bearing housing and locate in the crankshaft recess.

      3. Remove the nut HPC Variable Stator Vane Actuator (75-32-42, 01-082), the washer HPC Variable Stator Vane Actuator (75-32-42, 01-083) and the bolt HPC Variable Stator Vane Actuator (75-32-42, 01-084) to disconnect the control rod.

      4. Hold the VSV actuator, remove the four bolts and the two washers that attach the actuator to the HP compressor case and remove the actuator. Remove the bracket HPC Variable Stator Vane Actuator (75-32-41, 01-070).

      5. NOTE

        The VSV actuator must have its maintenance completed, as given in the D.S.I.C. Component Maintenance Manual (75-32-41).

        Remove the bolt that attaches the bracket HPC Variable Stator Vane Actuator (75-32-41, 01-080) to the actuator and remove the bracket.

    3. Figure: Disconnect the Electrical Harness Connectors

    Disconnect the Electrical Harness Connectors

    Figure: Disconnect the Electrical Harness Connectors

    Disconnect the Electrical Harness Connectors

    Figure: Remove the VSV Actuator

    Remove the VSV Actuator

    Figure: Remove the VSV Actuator

    Remove the VSV Actuator

    Figure: Remove the VSV Actuator

    Remove the VSV Actuator

    Figure: Remove the VSV Actuator

    Remove the VSV Actuator

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:18992
Enterprise Name:HANSCOM INC
BU Name:HANSCOM INC
Street:331 MARKET STREET
P.O. Box:364
City:WARREN
State:RI
Zip Code:02885
Country:USA
Phone Number:1-401-247-1999, 1-800-725-6788
Fax Number:1-401-247-4575
Internet:www.hanscominc.com
Manufacturer Code:18992
Supply Number:CoMat 06-086
Type:sp01
Supply Short Name:CoMat 06-086 TIES
Supply Name:CoMat 06-086 TIES
Specification Groups:
Doc NumberType
PMC 4272SPECIAL WIRE TIES
Suppliers:
ManufacturerRemarks
18992
Manufacturer Code:X222X
Supply Number:CoMat 10-058
Type:sp01
Supply Short Name:CoMat 10-058 PENETRATING OIL
Supply Name:CoMat 10-058 PENETRATING OIL
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:0AM53
Tool Number:IAE 1R18254
Tool Name:IAE 1R18254 Rigging pin