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Honeywell EGPWS MK V - Page 50

Honeywell EGPWS MK V
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Mark V and Mark VII EGPWS Pilot’s Guide
System Description 060-4241-000
44 Rev H, August 2011
Options
Continued
Altimeter Monitor issues annunciations if the altimeter
setting is improper.
Long Landing Monitor
issues annunciations if the
aircraft does not touchdown within an operator defined
distance from the runway threshold.
Low Airspeed Monitor (basic function
for Boeing
737NG aircraft only) issues annunciations when airspeed
decreases below 70% of the amber band on the PFD Speed
tape.
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.
RAAS/MON Inhibit/Enable Inhibits or Enables RAAS
and/or Stabilized Approach, Takeoff Flap Configuration,
and Long Landing monitor functions.
For additional options information contact Honeywell.

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