Temporary Revision
DCM005
TEMPORARY REVISION
TR No: TR18-CMM-001
ISSUE DATE: 23-Oct-18
Revision to Aircraft Modular Power Supply CMM 24-30-03
1
INTRODUCTION
The purpose of this Temporary Revision is to provide an Alternate Acceptance
Test Procedure.
2
EFFECTIVE DATE: 23-Oct-18
3
INSERTION INSTRUCTIONS:

Insert the TR immediately after Page 111, Testing and Fault Isolation section of the
Aircraft Modular Power Supply CMM 24-30-03

The Revision Details provided in Section 8 below are additional to the manual.

After insertion of the TR, ensure that all applicable details are recorded in the
Record of Temporary Revisions in Chapter 0 of the manual.

The manual holder is responsible for ensuring that all subordinate staff are advised
of the changes.
4
ISSUED BY:
Sharon Bye, Maintenance Program Approval Employee
5
APPLICABLE TO:
All holders of the Aircraft Modular Power Supply CMM 24-30-03
6
DISTRIBUTION:
All holders of the Aircraft Modular Power Supply CMM 24-30-03
7
CANCELLATION
The applicability of this TR will be reviewed at the next revision of the Aircraft
Modular Power Supply CMM 24-30-03
DCM005 – v3.0
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Temporary Revision
DCM005
8
REVISION DETAILS
The following text now forms part of the manual:
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