Appendix F: Takeoff Flap Configuration Monitor Maintenance Messages - Honeywell MK V Line Maintenance Manual

16 APPENDIX F: TAKEOFF FLAP CONFIGURATION MONITOR MAINTENANCE
MESSAGES
TABLE F-1: TAKEOFF FLAP CONFIGURATION MONITOR MAINTENANCE MESSAGES
MAINT.
FUNCTION
Except where noted, all maintenance
message voices are Male
Self-Test Level 1 "Flaps Monitor Inhibited"
Self-Test Level 1 "Flaps Monitor INOP"
Self-Test Level 2 "Flaps Monitor Flap Angle Undefined"
Self-Test Level 3 "Flaps Monitor Enabled"
(Annunciated at
end of Selected
Options )
Self-Test Level 3 "RCD Part Number XXX-XXXX-XXX "
where X is the 10-digit installation-specific RCD
part number.
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.
CAGE CODE: 97896
EGPWS LINE MAINTENANCE MANUAL
MESSAGE
SCALE: NONE SIZE: A
All volume levels at same volume as
existing EGPWS Self-Test messages
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.
Takeoff Flap Configuration Monitor enabled but
the function is inoperative
Takeoff Flap Configuration Monitor function is
enabled but the aircraft does not provide a
source of Flap Position
RCD Enable Key is set and loaded RCD
activates Takeoff Flap Configuration Monitor
function.
Allows verification that the correct RCD is
loaded into the EGPWS.
DWG NO.: 060-4199-180
NOTES:
REV: G SHEET 66 of 68