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

Autopilot Flight Director Mode Annunciations.
Autopilot HSI Select Arrow.
Low Bank Limit Arc.
Autopilot Flight Director Command Bar.
Vertical Deviation Scale/Pointer Annunciator (VTA).
Marker Beacons.
Airspeed Reference Bug/Readout.
Airspeed VNAV Speed Bug.
Airspeed VSpeed Bugs/Readout.
Radio Altitude Readout.
Decision Height Readout.
Minimum Descent Altitude Readout/Bug.
Selected Altitude Readout/Bug.
Altitude VNAV Target Readout/Bug.
All failure flags for the items listed above.
The following comparators: HDG, RAD, LOC, AZ, GS, GP, EICAS.
60
45
30
20
10
10
20
40
30
60
90
10
20
30
20
10
90
NOTE
The symbology will be restored when pitch is between 28 and −18 degrees (inclusive).
40
20 20
30
45
10 10
60
GF1110_028
10 10
20 20
30 30
FLIGHT INSTRUMENTS
REV 46, Jul 21, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−23
VERTICAL SPEED INDICATOR (VSI)
Vertical Speed Scale
Tick marks are placed at
the following: 0, + 1000,
+ 2000 and + 3000 FPM.
At vertical speeds in
excess of + 3600 FPM,
the pointer will park at
+ 3600 FPM.
Only one half of the
arrowhead and one half
of the target bug will be
in view.
0 1500
1
2
3
1
2
3
2
3
0 1000
1
2
3
1
2
3
1
0
1
0 4000
1
2
3
1
Vertical Speed Readout
The vertical speed readout has a
range of + 9999 FPM.
For vertical speeds less than
+ 1000 FPM information is
rounded to the nearest 100 FPM.
For vertical speeds more than
+ 1000 FPM information is rounded
to the nearest 100 FPM.
The digital readout and box is removed
for vertical speeds less than or equal to
+ 500 FPM, and enabled for vertical speeds
greater than or equal to + 600 FPM .
Vertical Speed Pointer
Vertical Speed Target Bug
Displayed when flight director VS
mode (cyan) or FMS VPTH mode
(magenta) is active.
When vertical speed target is
within range of + 1000 FPM it is
rounded to the nearest 100 FPM.
When vertical speed target
is greater than or equal to
+ 1000 FPM, information is
rounded to the nearest 100 FPM.
GF1110_029
−
−
−
−
−
−
−
−
−
−
−
−
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 46, Jul 21, 2005
CSP 700−6
Volume 2
11−10−24
PFD CONTROL PANEL
The PFD control panels (2) are located on the glareshield. Both the pilot’s and copilot’s
control
panels have identical but separate onside
functions. The PFD control panel is used for selection of
bearing pointers, VOR/LOC source, FMS source, setting of minimums and barometric settings and
compass display format.
V/L Button
Used to select VOR or LOC
as a primary NAV source.
BRG Button
Used to select bearing
sources, VOR 1, ADF 1,
FMS 1 (FMS 3 if installed).
BRG Button
Used to select bearing
sources, VOR 2, ADF 2,
FMS 2.
FMS Button
Used to select FMS1, FMS 2 or
FMS 3, (If installed) source or,
FMS1, FMS 2 or LTRK (if installed).
HSI Button
Used to select full or
partial compass display.
MINIMUMS Knob
RAD
Height (DH) value on PFD.
BARO
Descent Altitude (MDA) value
on PFD.
BARO SET Knob
PUSH STD
29.92 (in)/hg or 1013 HPa.
IN
HPa
Indicates Chapter in which information on item may be found.
GF1110_030
− Sets the Decision
− Sets the Minimum
− When pushed, it will either display
− Sets the altimeter for inches of mercury.
− Sets the altimeter for hectopascals.
17
17
17
17
RAD BARO
MINIMUMS NAV SCR BARO SET
PUSH STD
IN HPa
FLIGHT INSTRUMENTS
REV 46, Jul 21, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−25
PFD CONTROL PANEL (CONT'D)
MINIMUMS Knob
MINIMUMS Outer Knob
RAD
Height (DH) value on PFD.
BARO
Descent Altitude (MDA) value
on PFD.
MINIMUMS Inner Knob
Slow rotation of inner knob
allows for precise setting of data
(1 "click" of knob = 10 feet).
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰(zhàn)者手冊6(153)