TASK 71-00-02-000-008-B00 (A5-PPBU) - Remove The Thermal Anti-Ice (TAI) Duct, Removal-008

DMC:V2500-A5-71-00-0200-07B-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

Common Information

TASK 71-00-02-000-008-B00 (A5-PPBU) - Remove The Thermal Anti-Ice (TAI) Duct, Removal-008

General

Fig/item numbers in parentheses in the procedure agree with those used in the EIPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the EIPC.

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.

Discard all rubber seal rings, split cotter pins and gaskets removed in this procedure.

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

All the tubes, hoses and ducts removed in this procedure must have their maintenance completed, as given in the Component Maintenance Manual (CMM-THD-V2500-1IA) or the Aeroquip Maintenance Manual (29-11-49) as specified.

Seal all openings when the tubes and components are disconnected to prevent contamination from unwanted material.

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 10-058 PENETRATING OIL0AM53CoMat 10-058

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 71-00-02-020-020 Remove the Thermal Anti-Ice (TAI) Duct

    2. Refer to Figure and Figure.

      1. Safety the TAI duct.

      2. Attach temporary ties to the rear of the duct Anti-Ice Ducts (30-21-49, 01-070), to hold it in safety.

      1. Remove the duct Anti-Ice Ducts (30-21-49, 01-070).

      2. Remove the bolt, the flanged bush, the washer and the nut which attach the female link bearing to the duct.

      3. NOTE

        The procedure for the remaining TAI ducts (7th stage offtake) is given in TASK 72-00-40-020-004, SUBTASK 72-00-40-020-087.

        Remove the temporary ties. Remove the duct and the attached coupling.

  1. Figure: Remove the Thermal Anti-Ice (TAI) Duct

    Sheet 1

    Legend
    Remove the Thermal Anti-Ice (TAI) Duct

    Sheet 1

    Close

    Figure: Remove the Thermal Anti-Ice (TAI) Duct

    Sheet 2

    Legend
    Remove the Thermal Anti-Ice (TAI) Duct

    Sheet 2

    Close

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: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