曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

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.
OPERATING MANUAL
2A-34-00 PRODUCTION AIRCRAFT SYSTEMS
Page 36
October 11/01
Revision 5
EGPWS System Diagram
Figure 8
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-34-00
Page 37
October 11/01
Revision 5
OPERATING MANUAL
THIS PAGE IS INTENTIONALLY LEFT BLANK.
2A-34-00 PRODUCTION AIRCRAFT SYSTEMS
Page 38
October 11/01
O-RIDES / TEST Panels
on Center Pedestal
Figure 9
OPERATING MANUAL
2A-34-00
Page 39 / 40
October 11/01
Excessive Descent Rate Envelope - Mode 1
Figure 10
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-34-00
Page 41
October 11/01
Revision 5
Excessive Terrain Closure Envelope - Mode 2A
Figure 11
OPERATING MANUAL
2A-34-00 PRODUCTION AIRCRAFT SYSTEMS
Page 42
October 11/01
Revision 5
Excessive Terrain Closure Envelope - Mode 2B
Figure 12
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-34-00
Page 43
October 11/01
Revision 5
Altitude Loss After Takeoff Envelope - Mode 3
Figure 13
OPERATING MANUAL
2A-34-00 PRODUCTION AIRCRAFT SYSTEMS
Page 44
October 11/01
Revision 5
Unsafe Terrain Clearance
Envelope - Mode 4A and
Mode 4B
Figure 14
OPERATING MANUAL
2A-34-00
Page 45 / 46
October 11/01
Unsafe Terrain Clearance
Envelope - Mode 4C and
Excessive Glide Slope
Deviation - Mode 5
Figure 15
OPERATING MANUAL
2A-34-00
Page 47 / 48
October 11/01
Excessive Bank Angle Envelope - Mode 6
Figure 16
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-34-00
Page 49
October 11/01
Revision 5
OPERATING MANUAL
THIS PAGE IS INTENTIONALLY LEFT BLANK.
2A-34-00 PRODUCTION AIRCRAFT SYSTEMS
Page 50
October 11/01
Windshear Alerting
Envelope - Mode 7
Figure 17
OPERATING MANUAL
2A-34-00
Page 51 / 52
October 11/01
Terrain Clearance Floor Envelope
Figure 18
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-34-00
Page 53
October 11/01
Revision 5
Forward Looking Terrain Alerting Areas
Figure 19
Terrain Awareness Display Altitudes
Figure 20
OPERATING MANUAL
2A-34-00 PRODUCTION AIRCRAFT SYSTEMS
Page 54
October 11/01
Revision 5
Terrain Awareness Display
Figure 21
OPERATING MANUAL
PRODUCTION AIRCRAFT SYSTEMS 2A-34-00
Page 55
October 11/01
Revision 5
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
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：灣流4操作手冊 Gulfstream IV Operating Manual 2(121)