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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
TEMPORARY REVISION NO. 23-1
INSERT PAGE 45 OF 53 FACING PAGE 6-108.
Reason:
To add a new failure code, 0B, to Table 6-20 between failure codes 0A and 0D.
Failure code 0B is added as follows:
Table 6-20.
Failure
Code
0B
HDM
MCS-4200/7200
Airbus Level I (SDU No. 2) Failure Messages and ATA No.
SDU/SDU No. 2 – CFDS Normal and Interactive Modes
© Honeywell International Inc. Do not copy without express permission of Honeywell.
23-20-35
ATA Number
232832
Page 45 of 53
28 Sep 2009
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