Honeywell MK VI Benutzerhandbuch

EGPWS LINE MAINTENANCE MANUAL 

CAGE CODE: 97896 

SCALE: NONE     SIZE: A 

DWG NO.:  060-4199-180 

REV:   G 

SHEET  66 of 68 

 

 

Except where noted, all maintenance 
message voices are Male 

All volume levels at same volume as 

existing EGPWS Self-Test messages  

Self-Test Level 1 

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 ) 

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.