曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
Radar waypoints are used in the same manner as any other data
base waypoint. Either going direct-to the radar waypoint or modifying
the flight plan to include it eliminates any need to "decouple" from
the FMS or Nav mode of the flight guidance system by switching to
the Heading mode. All radar waypoints will be automatically erased
upon FMS initialization.
Radar waypoints are not part of the 200 pilot-defined locations.
They will appear on the FMS, as does any other waypoint. When
the FPL DTO page is displayed, the last radar waypoint defined is
always the first choice on the page.
Section VII
Sensors & Interfaces
2423sv602 7-55
Change 1
COLLINS EFIS INTERFACE
The following features are only available to the operator when the
FMS system is interfaced to a Collins C-14 EFIS, Pro Line 4 or
compatible.
NOTE: When the FMS is displayed or coupled to the Flight
Director/Autopilot System, monitor the EFIS heading bug
for proper values and reset as required.
Two-Way Interface with Heading Bug
This function allows the FMS to receive selected heading settings
that are driven from the heading select knob. These will appear in
the command heading window on the FMS. Conversely, when the
FMS is in Command Heading Mode, any entry on the FMS will be
received by the EFIS, and the heading bug will slew to that value. In
either case the Flight Guidance System (FGS) will fly to these
heading when NAV is engaged.
Go-Around Function
When the pilot presses the Go-Around button, the current Approach
will be canceled. If there are additional waypoints in the flight plan
between the end of approach and the destination, then the TO
waypoint becomes the first waypoint following the end of approach.
This is then referred to as the Missed Approach Procedure.
Section VII
Sensors & Interfaces
7-56 2423sv602
Change 1
The Creation and use of ILS Approaches
ILS approaches may be defined and linked into a flight plan using
the same procedures as VOR, RNV, VFR and TCN approaches.
When ARM APPR is selected on the FMS, the ILS receiver is
automatically tuned to the ILS frequency by the FMS, and the EFIS
arms for capture. If the pilot arms APPR on the Flight Guidance
System, the aircraft will transition from lateral and vertical FMS mode
to Approach mode using the localizer and glideslope signals from
the ILS receiver. If the pilot flies the approach with only NAV mode
selected on the FGS then only lateral transitions will be made from
FMS to Localizer.
Automatic Display of Second Course
If an approach is linked into the FMS flight plan, at 50 nautical miles
from the end of approach the ARM APPR option will become
available. When the approach is armed, the EFIS will automatically
display the inbound approach course as the second course on the
EHSI.
Enroute VNAV Pitch Commands
Enroute VNAV profiles may be flown while coupled to the Flight
Guidance System. The FMS computes a Vertical Pitch Command,
which is recognized when VNAV is selected on the FGS Mode
Select Panel.
TEMPORARY CHANGE
Page 1 of 1
19 June 2006
MANUALS AFFECTED: Operator’s Manual, Report No.
2423sv602, 2423sv603, 2423sv604, 2423sv702, 2423sv703,
2423sv704, 2423sv801/901 and 2423sv802/902.
FILING INSTRUCTIONS: Insert this Temporary Change
behind the UNILINK tab.
NOTE: Do not remove UniLink Instructions supplements until
applicable UniLink Operator’s Manuals are obtained.
REASON: New manuals to replace UniLink section. Refer to
Service Letter 2807.
INSTRUCTIONS:
The UniLink Section of this manual has been superseded by
separate UniLink Operator’s manuals. If your FMS is
interfaced to a Universal UniLink then refer to the applicable
manual as listed below;
UniLink UL-600 or UL-601, refer to report no. 23-20-02.01
UniLink UL-700 or UL-701, refer to report no. 23-20-04.01
These manuals are available online at www.uasc.com or they
may be ordered through our Marketing department at
(520) 295-2337 or (800) 321-5253. Requests can also be
made by emailing info@uasc.com.
Appendix A
2423sv602 A-i
Change 1
TABLE OF CONTENTS
INTRODUCTION ...................................................................... A-1
Description............................................................................. A-1
Global Data Center (GDC) .................................................... A-2
COMPONENTS ........................................................................ A-2
Data Management Unit (DMU).............................................. A-2
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者手册10(117)
