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

3) Press the APR Key.
Or:
1) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary).
2) Ensure a LOC/ILS approach is loaded into the active flight plan.
3) Ensure the corresponding LOC frequency is tuned.
4) Press the APR Key.
Figure 7-20 Glideslope Mode Armed
Once LOC is the navigation source, the localizer and glideslope can be captured. Upon reaching the glideslope, the flight director transitions to Glideslope Mode and begins to capture and track the glideslope.
Figure 7-21 Glideslope ModeNAV2 (localizer) is Selected Navigation SourceCommand Bars Indicate Descenton Localizer/Glideslope PathGlideslope Mode ActiveApproach Mode ActiveActive ILS FrequencyTunedGlideslope Indicator
386 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Takeoff (TO) and Go Around (GA) Modes
Go Around and Takeoff modes are coupled pitch and roll modes and are annunciated as both the vertical and lateral modes when active. In these modes, the flight director commands a constant set pitch attitude and keeps the wings level. The GA Switch is used to select both modes. The mode entered by the flight director depends on whether the aircraft is on the ground.
Takeoff Mode provides an attitude reference during rotation and takeoff. This mode can be selected only while on the ground by pushing the GA Switch. The flight director Command Bars assume a wings-level, pitch-up attitude.
Pressing the GA Switch while in the air activates the flight director in a wings-level, pitch-up attitude, allowing the execution of a missed approach or a go around. Go Around Mode disengages the autopilot and arms Selected Altitude Capture Mode automatically. Subsequent autopilot engagement is allowed. Attempts to modify the aircraft attitude (i.e., with the NOSE UP/DN Wheel or CWS Button) result in reversion to Pitch and Roll Hold modes.
Autopilot Disconnect Annunciation Flashes Yellow 5 secGo Around Mode ActiveFigure 7-22 Go Around ModeCommand Bars Indicate Climb
Takeoff Mode ActiveFigure 7-23 Takeoff ModeCommand Bars Indicate Climb for Takeoff
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 387
Automatic utomatic utomatic Flight Control System ystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
7.4 Lateralateral Modes
The following table relates each GFC 700 lateral mode to its respective control and annunciation. Refer to the vertical modes section for information regarding Go Around and Takeoff modes.
Lateral Mode
Description
Control
Annunciation
Maximum Roll Command Limit
Roll Hold
Holds the current aircraft roll attitude or rolls the wings level, depending on the commanded bank angle
(default)
ROL
30°
Low Bank
Limits the maximum commanded roll angle
BANK Key
*
18°
Heading Select**
Captures and tracks the Selected Heading
HDG Key
HDG
30°
Navigation, GPS**
Captures and tracks the selected navigation source (GPS, VOR, LOC)
NAV Key
GPS
30°
Navigation, VOR Enroute Capture/Track**
VOR
25° Capture
10° Track
Navigation, LOC Capture/Track
(No Glideslope)
LOC
25° Capture
10° Track
Backcourse Arm/Capture/Track
Captures and tracks a localizer signal for backcourse approaches
BC Key
BC
25° Capture
10° Track
Approach, GPS
Captures and tracks the selected navigation source (GPS, VOR, LOC)
APR Key
GPS
30°
Approach, VOR Capture/Track
VAPP
25° Capture
10° Track
Approach, LOC Capture/Track
(Glideslope Mode automatically armed)
LOC
25° Capture
10° Track
Takeoff
Commands a constant pitch angle and wings level on the ground in preparation for takeoff
GA Switch
TO
Wings Level
Go Around
Disengages the autopilot and commands a constant pitch angle and wings level in the air
GA
Wings Level
* No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in green along the Roll Scale of the Attitude Indicator.
** The Heading, Navigation GPS and Navigation VOR mode maximum roll command limit will be limited to the Low Bank mode value if it is engaged.
The GFC 700 limits turn rate to 3 degrees per second (standard rate turn).
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Cessna Citation Mustang G1000 Integrated Flight Dec(137)