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

EGPWS LINE MAINTENANCE MANUAL

15 APPENDIX E: ALTIMETER MONITOR MAINTENANCE MESSAGES

TABLE E-1: ALTIMETER 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 “Altimeter Monitor INOP”

Self-Test Level 2 “Altimeter Monitor GPS Signal Undefined”

Self-Test Level 2 “Altimeter Monitor Static Air Temperature Undefined”

Self-Test Level 3 “Altimeter 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.

Altimeter Monitor enabled but the function is inoperative

Altimeter Monitor function is enabled but the aircraft does not provide a source of GPS

Altimeter Monitor function is enabled but the aircraft does not provide a source of SAT

RCD Enable Key is set and loaded RCD activates Altimeter 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 Altimeter Monitor installed.

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