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
220
200
180
160
VOR 1
10.0 NM
190 GS
ADF1
ADF2
0.0 VS
21
30
2 000
100
900
800
00
000
1
ELV 200
CRS 240
DME Distance Readout
Navigation Source
Indicator
Indicates navigation source
as set at NAV SOURCE knob
on display control panel.
The selected navigation
source is displayed using
the characters:
VOR 1 or VOR 2,
LOC 1 or LOC 2.
(1 is on--side; 2 is off--side)
An FMS navigation source is
not annunciated.
REV 56, Jan 31/03
Vol. 1 12--70--54
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual MASTER
CSP A--013
Primary Mode --- Navigation/Position Indications
Figure 12---70---24 Sheet 2
Glideslope Failure Flag GS
AP 10
SYNC
PRI
LOC 1
GS
VOR 1
21
1700
M .545
240
220
200
180
160
LOC 1
10.0 NM
190 GS
ADF1
ADF2
0.0 VS
21
30
2 000
100
900
800
00
000
1
Vertical deviation pointer which
retains its full diamond shape
when travelling within the scale.
The pointer changes to a
half--diamond shape when
the vertical deviation
exceeds 2 dots.
At altitudes below 600 feet
AGL, the pointer will flash, for
as long as the excessive
glideslope deviation exists.
Glideslope Index
+2 dots
+1 dot
--1 dot
--2 dots
CRS 240
Glideslope Scale
0 dot
Indicates the airplane’s vertical
deviation relative to the ILS
glideslope beam. Displayed in
the following conditions:
Navigatioin source is LOC;
Armed or captured vertical
AFCS mode is GS;
Altitude is above 50 feet AGL.
A glideslope failure is indicated by the above failure flag
and all glideslope information is removed from the display.
A miscompare between the glideslope deviation sources
is indicated by the same failure flag but glideslope data is
retained. The flag flashes for 5 seconds when the
miscompare is first detected and thereafter remains
displayed until the condition is corrected.
+2 dots
Vol. 1 12--70--55
REV 56, Jan 31/03
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual
CSP A--013
MASTER
Primary Mode --- Navigation/Position Indications
Figure 12---70---24 Sheet 3
AP 10
SYNC
PRI
LOC 1
GS
A
VOR 1
21
1800
M .545
240
220
200
180
160
--0.7 VS
21
30
2 000
100
900
800
00
000
1
Glideslope Reference Line
--3.00 --3.00
--3.00 --3.00
Glideslope Line
Glideslope Readout
LOC 1
10.0 NM
190 GS
ADF1
ADF2
Provides a visual reference of the desired glide path to be
flown, as entered through the HGS control panel (HCP).
The glideslope reference line also represents 0 glideslope
deviation when it overlays the glideslope line.
Display criteria are:
Always displayed during approach and landing, at any
mode, except Rollout;
In flight, other than during the approach and landing
modes, the reference line is displayed for five seconds
whenever the selected glideslope value is changed
through the HCP.
Provides an accurate indication of the
airplane’s glideslope deviation.
Glideslope deviation is 0 when the
glideslope line is aligned with the
glideslope reference line.
Display criteria are:
Displayed during approach and landing
(AI, AII, AIII and F/D modes);
Removed from the display 70 feet AGL.
Digital indication of the selected
reference glideslope value.
Displayed in conjunction with
the glideslope reference line.
CRS 240
Lateral Deviation Line
(In Flight)
Provides an accurate
indication of the airplane’s
lateral deviation from the
selected course.
Airplane is on track when
the lateral deviation line is
aligned with the selected
course mark (on the
horizon line).
Displayed during HGS
approach and F/D
modes.
REV 56, Jan 31/03
Vol. 1 12--70--56
FLIGHT INSTRUMENTS
Head--Up Guidance System
Flight Crew Operating Manual MASTER
CSP A--013
Primary Mode --- Navigation/Position Indications
Figure 12---70---24 Sheet 4
33 N
1700
10.0 NM
190 GS
0.0 VS
21
30
800
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Bombardier_CRJ_00-Flight_Instruments(37)
