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slightly beyond
• Runway database that covers all runways at least 3,500 feet in length
The database is updated when significant changes occur. The database updates
are on a PCMCIA card available from Honeywell. The number of the latest
database version is listed on the Honeywell website http://www.egpws.com/ or by
calling the EGPWS hotline at (800) 813-2099.
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EGPWS System Diagram
Figure 8
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O-RIDES / TEST Panels
on Center Pedestal
Figure 9
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Excessive Descent Rate Envelope - Mode 1
Figure 10
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Excessive Terrain Closure Envelope - Mode 2A
Figure 11
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Excessive Terrain Closure Envelope - Mode 2B
Figure 12
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Altitude Loss After Takeoff Envelope - Mode 3
Figure 13
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Unsafe Terrain Clearance
Envelope - Mode 4A and
Mode 4B
Figure 14
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Unsafe Terrain Clearance
Envelope - Mode 4C and
Excessive Glide Slope
Deviation - Mode 5
Figure 15
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Excessive Bank Angle Envelope - Mode 6
Figure 16
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Windshear Alerting
Envelope - Mode 7
Figure 17
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Terrain Clearance Floor Envelope
Figure 18
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Forward Looking Terrain Alerting Areas
Figure 19
Terrain Awareness Display Altitudes
Figure 20
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Terrain Awareness Display
Figure 21
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2A-34-60: Traffic / Aircraft Alert and Collision Avoidance System (TCAS /
ACAS)
1. General Description:
The Honeywell Traffic / Aircraft Alert and Collision Avoidance System (TCAS-2000
/ ACAS) is production installed on GIV Serial Number (SN) 1390 and subsequent.
Airplanes SN 1390 to 1433 were originally programmed with TCAS software
version 6.04 and SN 1434 and subsequent with ACAS software version 7.0.
Software version 7.0 is required for operation within European airspace. It is
expected that all TCAS equipped airplanes will be equipped with version 7.0. This
system description presumes the installation of software version 7.0.
TCAS/ACAS provides the flight crew with notifications of the presence of other
transponder equipped traffic in the vicinity that may present a collision hazard.
TCAS/ACAS can track up to fifty (50) airplanes simultaneously. The system
provides aural alerts to the presence of traffic, visual plots on cockpit displays of
the relative location of other airplanes, and aural and visual cues for evasive
maneuvers if collision is imminent. If both converging airplanes are equipped with
TCAS/ACAS and Mode S transponders, the systems mutually coordinate evasive
maneuvers to ensure diverging flight paths.
The system functions as a low-powered airborne equivalent of the ground-based
ATC system, interrogating and receiving replies from the transponders of other
airplanes. Transponder replies are used to plot the position of traffic, and for traffic
with Mode C and Mode S transponders, the altitude of the target is also
determined.
TCAS / ACAS consists of the following subsystems / components as shown in the
simplified block diagram in Figure 22:
• Two antennas, one on the top and one on the bottom of the airplane, each
　
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