TASK 72-00-40-050-004 HP System Module Components - Remove The Igniter Plug, Removal-014

DMC:V2500-A0-72-00-4050-03A-520A-B|Issue No:002.00|Issue Date:2021-08-01

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

All

Common Information

TASK 72-00-40-050-004 HP System Module Components - Remove The Igniter Plug, Removal-014

General

This TASK gives the procedure to remove the igniter plug.

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.

The igniter plug removed in the procedure must have their maintenance completed, as given in the NGK Spark Plug Co. Component Maintenance Manual (74-21-41).

Seal all openings when the 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 OILX222XCoMat 10-058

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-00-40-040-052 Disconnect the Ignition Leads (74-21-43, 01-100) and (74-21-43, 02-100)

    1. Refer to Figure.

    2. CAUTION

      DO NOT BEND THE ELECTRICAL CABLE CONDUIT TOO MUCH WHEN YOU DISCONNECT THE ELECTRICAL CONNECTOR. THE CONDUIT CAN BE DAMAGED AND CAN CAUSE ELECTRICAL CIRCUIT DEFECTS.

      Loosen the clamps IGNITION-IGNITION LEADS (74-21-43, 01-055) and clamps IGNITION-IGNITION LEADS (74-21-43, 01-060) or clamps Ignition Leads (74-21-43, 02-055) and clamps Ignition Leads (74-21-43, 02-060) and move them away from the cooling shrouds IGNITION-IGNITION LEADS (74-21-43, 01-070) and IGNITION-IGNITION LEADS (74-21-43, 01-075) or cooling shrouds Ignition Leads (74-21-43, 02-070) and Ignition Leads (74-21-43, 02-075).

    3. Remove the cooling shroud IGNITION-IGNITION LEADS (74-21-43, 01-070) and cooling shroud IGNITION-IGNITION LEADS (74-21-43, 01-075) or cooling shroud Ignition Leads (74-21-43, 02-070) and Ignition Leads (74-21-43, 02-075).

    4. Disconnect the ignition lead IGNITION-IGNITION LEADS (74-21-43, 01-100) and Ignition Leads (74-21-43, 02-100).

    2. SUBTASK 72-00-40-050-053 Remove the Igniter Plug (74-21-41, 01-100) and (74-21-41, 02-100)

    1. Refer to Figure.

    2. Remove the Igniter Plug (74-21-41, 01-100) and Igniter Plug (74-21-41, 02-100).

    3. SUBTASK 72-00-40-620-051 Seal all Openings

    1. Install covers to all exposed opening.

    4. Figure: Remove The Igniter Plug

    Remove The Igniter Plug

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Revised procedural steps and figure. (21VC075)

Manufacturer Code:X222X
Enterprise Name:N/A – REFER TO APPLICABLE COMAT SUFFIX
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