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

inset in the lower left corner of the PFD. The
PFD inset map can contain much of the same
information as available in the full-size moving
map on the MFD.
AUXILIARY INFORMATION
WINDOW
In the lower-right corner of the PFD, an auxiliary
information window can be set to display
information from the system, including:
• Nearest airports, with basic information
as currently recorded in the navigation
database (NRST softkey)
• ADF and distance measuring equipment
(DME) tuning (ADF/DME softkey)
• Flight plan display and entry (FPL key)
• Garmin system messages (MSG softkey)
• PDF setup (MENU key)
• References (TMR/REF softkey)
• Flight plan procedures (PROC key)
• Direct-To (D➞ Key)
Also use this window to select a waypoint
from the database and/or to display information
about the waypoint.
REVERSIONARY MODE
To provide emergency backup of the MFD and
PFDs, and to provide flexibility in display
modes, the G1000 has a reversionary mode that
causes both the PFD and the MFD to display
the essential information for continued flight.
In the event of display failure, the display
modes are as follows:
• PFD1 failure—MFD enters reversionary
mode; PFD2 remains in normal mode.
• MFD failure—PFDI and PFD2 enter
reversionary mode.
• PFD2 failure—PFD1 and the MFD remain
in normal mode.
16-20 510OM-00
CITATION MUSTANG OPERATING MANUAL
4
4
2
2
VERTICAL 500
SPEED
POINTER
Figure 16-23. Vertical Speed Indicator
1800 M
0
O M I
ALTIMETER
OUTER MARKER MIDDLE MARKER INNER MARKER
Figure 16-22. Marker Beacon Indications
Reversionary mode can be manually selected for
the onside display and the MFD by pressing
the large red DISPLAY BACKUP button at the
bottom of either audio control panel. Pressing
the red DISPLAY BACKUP button a second
time returns both displays to normal mode.
In reversionary mode, the left edge of the display
includes a single-column of EICAS information
condensed from the normal two-column
EICAS display on the MFD. Additionally, a
CAS message window appears on the right
edge of the PFD and expands as necessary to
display any active CAS messages (up to 14 in
a window) (Figure 16-24). If more than 14
messages appear, they can be scrolled.
NAV/COM FREQUENCIES AND
NAVIGATION DATA WINDOWS
Across the top of the PFD are avionics settings
and data indications, including VHF NAV and
COM frequencies (active and standby), and
navigation status data.
PFD CONTROLS
Each PFD is controlled by knobs and pushbutton
keys on its bezel, and/or by pilot operation
of the AFCS or MFD/FMS controller.
The following general discussion of controls
is also applicable to the other controllers.
Controls
Garmin displays (PFD and MFD) and control
panels (audio panel, AFCS controller, and
FMS controller) have various types of knobs,
buttons and switches. Refer to Figure 16-25
for PFD controls locations and Table 16-5 for
a description on those controls.
Softkeys
Along the bottom of the PFD, the bezel contains
12 “softkeys” marked with upward-pointing
triangles. These keys do not have a single,
specific, permanent function. They have different
purposes at different times, as determined
by the G1000 software.
Some (or all) softkeys have labels appearing
immediately above them on the display. The
labels change depending upon pilot settings
and/or current conditions. Navigating the
lower level menus is done through the top
level softkey menu.
When the label for a specific feature is toggled
off, the text is white on a black background.
When the label is toggled on, the text is black
on a light gray background.
When the BACK softkey is available (on the
right end of the softkeys), this key can be pressed
to escape the current menu and return to the
previous menu display. For details on the menus
for PFD softkeys. refer to Figure 16-26.
TRANSPONDER DISPLAY AND
CONTROL
The PFD depicts current transponder status in
the black XPDR box on the bottom right side
510OM-00 16-21
CITATION MUSTANG OPERATING MANUAL
4
4
2
2
5700
0
5600
5500
5300
5200
54 20
20
00
XPDR1 5537 IDNT UTC 18:07:21
IDENT TMR/REF NRST MSG
GWX FAIL - GWX IS INOPERATIVE.
CNFG MODULE - PFD1 CONFIGURATION
MODULE IS INOPERATIVE.
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Cessna塞斯納公務機飛行手冊(107)