Honeywell MK VIII, MK XXII manual Egpws Line Maintenance Manual, end of Selected Options

Models: MK VIII MK V MK XXII MK VII MK VI

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EGPWS LINE MAINTENANCE MANUAL

14 APPENDIX D: STABILIZED APPROACH MONITOR MAINTENANCE MESSAGES

TABLE D-1: STABILIZED APPROACH 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 “Approach Monitor Inhibited”

Self-Test Level 1 “Approach Monitor INOP

Self-Test Level 2 “Approach Monitor Approach Speed Undefined

Self-Test Level 3 “Approach 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.

Stabilized Approach Monitor enabled, but the advisories have been inhibited with the activation of an external input/switch

Stabilized Approach Monitor enabled but the function is inoperative

Stabilized Approach Monitor “Too Fast” function is enabled but the aircraft does not provide a source of Approach Speed

RCD Enable Key is set and loaded RCD activates Stabilized Approach Monitor function.

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 Stabilized Approach Monitor installed.

CAGE CODE: 97896

SCALE: NONE SIZE: A DWG NO.: 060-4199-180

REV: G

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Honeywell MK VIII, MK XXII manual Egpws Line Maintenance Manual, end of Selected Options