曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Marker
Beacon
Lateral
Deviation (CDI)
Vertical
Deviation Scale
and Pointer
DME/FMS
Distance
Heading
Source
HGS® Pilot Guide for the Bombardier CRJ 700 Model 4200
4-34 November 2002 9701-1153 Rev A
Excessive Localizer Deviation: Excessive Localizer Deviation shows as a
right or left-pointing triangle to the side of the Flight Path symbol to give
the direction of correction for the aircraft. The symbol flashes continuously
until localizer deviation is within limits.
Excessive Glideslope Deviation: shows as a downward or upward-pointing
triangle above or below the Flight Path symbol to give direction of
correction for the aircraft. The symbol flashes continuously until the
glideslope deviation is within limits.
FMS Waypoint Identifier: The FMS Waypoint Identifier identifies the
next FMS waypoint on the flight plan. This symbol shows in the lower left
corner of the display when flight-path data is set. If an FMS LNAV alert
occurs, the symbol flashes continuously.
FMS Messages: The FMS Messages are shown on one to two lines to give
data about FMS conditions. Eight characters can show on each line. This
symbol shows under the FMS Waypoint Identifier and flashes continuously.
FMS Reference Altitude: FMS Reference Altitude is shown above the
Altitude Scale when the FMS flight plan is in use. The altitude is followed
by “VN” and is the next waypoint crossing altitude.
FMS Vertical Speed: FMS Vertical Speed followed by “VN” give the
vertical speed that should be maintained to reach the FMS Waypoint
Reference Altitude. It is displayed in the lower right corner of the display.
Flight Director Transfer Message: “FD2” below the HGS and FCS modes
in the upper left corner of the Combiner display is shown when the left-side
pilot’s Flight Director source is #2.
HGS® Pilot Guide for the Bombardier CRJ 700 Model 4200
9701-1153 Rev A November 2002 4-35
Figure 4-16:
PRI Mode Navigation Symbols
FMS Reference
Altitude
FMS Waypoint
Identifier
FMS
Messages
FMS
Vertical Speed
Excessive
Glideslope
Deviation
Excessive
Localizer
Deviation
Flight Director
Transfer
Message
HGS® Pilot Guide for the Bombardier CRJ 700 Model 4200
4-36 November 2002 9701-1153 Rev A
Bearing Source: Bearing Source #1 shows to the left of the HSI and
Bearing Source #2 shows to the right of the HSI. Table 4-8 identifies the
bearing source symbol and function.
Table 4-8: Primary Mode Bearing Source Annunciations
Symbol Function
“ADF1” #1 ADF Receiver tuned and shows on left-side PFD
“ADF2” #2 ADF Receiver tuned and shows on left-side PFD
“FMS” Single FMS installation: FMS is navigation source and shows
on left-side PFD
“FMS1” Dual FMS installation: #1 FMS is navigation source and shows
on left-side PFD
“FMS2” Dual FMS installation: #2 FMS is navigation source and shows
on left-side PFD
“VOR1” #1 NAV Receiver tuned to VOR and shows on left-side PFD
“VOR2” #2 NAV Receiver tuned to VOR and shows on left-side PFD
Each set of characters is followed on the right by a Bearing Source symbol.
Bearing Pointers: these symbols are pointers that move on the outside of
the HSI. As the symbols move, they identify the selected bearing source as
it relates to the aircraft heading.
HGS® Pilot Guide for the Bombardier CRJ 700 Model 4200
9701-1153 Rev A November 2002 4-37
Figure 4-17:
PRI Mode Navigation Symbols
Bearing
Pointer #1
Bearing Source
#2
Bearing Source
#1
Bearing
Pointer #2
HGS® Pilot Guide for the Bombardier CRJ 700 Model 4200
4-38 November 2002 9701-1153 Rev A
Primary Mode Flight Path Symbol Group
See Figure 4-18 thru Figure 4-20. Table 4-9 gives the Primary Mode Flight
Path Symbol Group that moves together.
Table 4-9: Primary Mode Flight Path Symbol Group
PRI
Symbol
Ground
Flight
TO
Flight Path Symbol ● ●
Flight Path Acceleration ● ● ●
Speed Error Tape ●
FCS-Derived Guidance Cue ●
Flight Path Slip/Skid Indicator ●
Flare Cue ●
Flight Path Symbol (FPS): The Flight Path Symbol is unique information
not normally available on conventional head-down displays. The FPS
shows the actual flight path vector of the aircraft. The gull wings of the FPS
are angled downward at 30° to the horizon so that in a 30° level turn, the
30° angle overlays the Zero-Degree Pitch Line.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰(zhàn)者手冊8(15)