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• Audio Declutter Disable – Disables the Audio Declutter
function so that audio alerts are constant.
• Audio Alerting Voice Select – Selects the type(s) of voice
that are used for audio alerts.
• Lamp Format – One of two lamp formats are available.
• Lamp Format 1 provides only Mode 5 “Glideslope” alerts
to the caution (amber) lamp output and all other alerts
(except Windshear and Mode 6 callouts) to the warning
(red) lamp output.
• Lamp Format 2 provides all “Pull Up” warning alerts to
the warning (red) lamp output and all caution alerts to
the caution (amber) lamp output (FAA requirement for
new installations).
NOTE: Windshear annunciations are provided by separate outputs
and indications and are not affected by lamp format. Mode
6 advisories do not effect any annunciation and are not affected
by lamp format.
• Peaks Enable – Adds additional density patterns and
level thresholds to the Standard Display Mode, allowing
display of highest and lowest terrain/obstacle to increase
situational awarness.
Options
continued
060-4241-000 • Rev. E - December 2003
MK V & MK VII EGPWS Pilot Guide 43
Additional input discretes are used to control or define EGPWS
operations:
• EGPWS Self-Test – Cockpit switch initiates EGPWS Self-
Test on the ground. Typically part of EGPWS warning (red)
lamp.
• Glideslope Cancel – Cockpit switch cancels Mode 5
Glideslope alerting. Typically part of EGPWS caution (amber)
lamp.
• Glideslope Inhibit – Inhibits Mode 5 Glideslope alerting.
Normally used for backcourse approaches.
• Altitude Callout Enable – Enables Mode 6 Callouts.
• Mode 6 Low Volume – Reduces Mode 6 volume (an additional)
6 dB. This is typically hardwired or connected to an
external switch.
• TAD and TCF Inhibit – Cockpit switch to disable all TAD
and TCF functions. (FAA requirement)
• Audio Inhibit – disables all EGPWS audio outputs.
• Steep Approach Enable – Enables Steep Approach
(Mode 1 Excessive Descent Rate) alerts biasing.
• Steep Approach Select – Selects (activates) Steep Approach
(Mode 1 Excessive Descent Rate) alerts biasing to
reduce nuisance alerts.
• Flap Over-Ride – Cockpit switch to select landing flaps
when not in the landing flap configuration.
• Gear Over-Ride – Cockpit switch to select gear down
when not in the gear down configuration.
• PLI Select/Deselect – Used for displaying or deselecting
the display of EGPWS derived Pitch Limit Indicator (PLI)
signals when a Windshear warning occurs.
For additional options information contact Honeywell.
Options
continued
060-4241-000 • Rev. E - December 2003
44 MK V & MK VII EGPWS Pilot Guide
SECTION 3
Operational Procedures
System Constraints ........................................................................... 45
System Activation ............................................................................. 46
EGPWS Self Test ................................................................................. 47
Normal Procedures .......................................................................... 50
Caution Alerts .............................................................................. 51
Warning Alerts ............................................................................. 51
Glideslope Alerts .......................................................................... 51
Advisory Callouts .......................................................................... 52
Windshear Caution ....................................................................... 52
Windshear Warning ...................................................................... 52
Abnormal Procedures ........................................................................ 53
Emergency Procedures ...................................................................... 54
060-4241-000 • Rev. E - December 2003
MK V & MK VII EGPWS Pilot Guide 45
System
Constraints
System constraints for the EGPWS are:
• If terrain data is unavailable for a particular area, then
Terrain and Obstacle alerting and display is not available for
that area and the affected display area is colored MAGENTA.
(normally only displayed at or near North and South
Poles dependent upon airplane flight path and location).
• The display of terrain and obstacle information is intended
to serve as a situational awareness tool. It does not provide
　
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