Honeywell MK XXII - Appendix F: Takeoff Flap Configuration Monitor Maintenance Messages

EGPWS LINE MAINTENANCE MANUAL
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16 APPENDIX F: TAKEOFF FLAP CONFIGURATION MONITOR MAINTENANCE
MESSAGES
TABLE F-1: TAKEOFF FLAP CONFIGURATION MONITOR MAINTENANCE MESSAGES
MAINT.
FUNCTION
MESSAGE
Except where noted, all maintenance
message voices are Male
NOTES:
All volume levels at same volume as
existing EGPWS Self-Test messages
Self-Test Level 1
“Flaps Monitor Inhibited”
Takeoff Flap Configuration Monitor enabled, but
the advisories have been inhibited with the
activation of an external input/switch. NOTE –
the EGPWS does not support a dedicated
Takeoff Flap Configuration Monitor inhibit, but
activation of a defined RAAS inhibit will also
inhibit Takeoff Flap Configuration Monitor.
Self-Test Level 1 “Flaps Monitor INOP” Takeoff Flap Configuration Monitor enabled but
the function is inoperative
Self-Test Level 2 “Flaps Monitor Flap Angle Undefined” Takeoff Flap Configuration Monitor function is
enabled but the aircraft does not provide a
source of Flap Position
Self-Test Level 3
(Annunciated at
end of Selected
Options )
“Flaps Monitor Enabled”
RCD Enable Key is set and loaded RCD
activates Takeoff Flap Configuration Monitor
function.
Self-Test Level 3 “RCD Part Number XXX-XXXX-XXX “
where X is the 10-digit installation-specific RCD
part number.
Allows verification that the correct RCD is
loaded into the EGPWS.
NOTE: Operators/Installers must refer to their Instructions for Continued Airworthiness (ICA) documentation to
identify the approved RCD configurations specific to their aircraft type/model having Takeoff Flap
Configuration Monitor installed.