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

• Current Track Indicator
• Wind Data (calculated based on GPS information)
• Distances in the Bearing Information windows
• GPS bearing pointers
These items should be verified when operating in Dead Reckoning Mode.
190-00494-02 Rev. B Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 79
Flight Instruments
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS EICAS AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE AFCS ADDITIONAL
FEATURES APPENDICES INDEX
Unusualnusual Attitudes
When the aircraft enters an unusual pitch attitude, red extreme pitch warning chevrons pointing toward the horizon are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon line.
Figure 2-47 Pitch Attitude WarningsNose LowNose High
If pitch exceeds +30˚/-20˚ or bank exceeds 65˚, some information displayed on the PFD is removed. The Altimeter and Airspeed, Attitude, Vertical Speed, and Horizontal Situation indicators remain on the display and the Bearing Information, Alerts, and Annunciation windows can be displayed during such situations. The following information is removed from the PFD (and corresponding softkeys are disabled) when the aircraft experiences unusual attitudes:
• Traffic Annunciations• AFCS Annunciations• Flight director Command Bars• Inset Map• Temperatures• DME Information Window• Wind data• Selected Heading Box• Selected Course Box• Transponder Status Box• System Time• PFD Setup Menu• Windows displayed in the lower right corner of the PFD:– Timer/References– Nearest Airports– Flight Plan– Messages– Procedures– ADF/DME Tuning• Minimum Descent Altitude/Decision Height readout• Vertical Deviation, Glideslope, and Glidepath Indicators• Altimeter Barometric Setting• Selected Altitude• VNV Target Altitude
80 Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang 190-00494-02 Rev. B
Flight Instruments
SYSTEM
OVERVIEW
FLIGHT
AUDIO PANEL EICAS INSTRUMENTS
& CNS
FLIGHT
MANAGEMENT
HAZARD
ADDITIONAL AFCS AVOIDANCE
INDEX APPENDICES FEATURES
Blank Page
190-00494-02 Rev. B
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
81
Engine Indicationndication & Crew Alerting Systemystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX Noteote: Refer to the Airplane Flight Manual (AFM) for limitations.
The Cessna Citation Mustang’s Engine Indication and Crew Alerting System (EICAS) offers improved flight operations and reduces crew workload by automatically monitoring critical system parameters and providing system alerts during all phases of flight. In combination with the EICAS, aural alerts, additional avionics messages, and master indicators are used to inform the crew of aberrant flight conditions. The EICAS is also designed to provide an improved level of maintenance data for the ground crew.
The EICAS can be divided into two major functions:
• The Engine Indication System (EIS) displays electrical, fuel, engine, pressurization, and flight control information.
• The Crew Alerting System (CAS) displays advisories, cautions, and warnings to communicate conditions, statuses, and system failures. CAS messages are grouped by level of importance and color-coded based on urgency in the CAS pane in the lower left of the EICAS Display.
EICAS information is normally displayed on the left side of the Multi Function Display (MFD).
Figure 3-1 Multi Function Display (Normal)EICAS Display
Section 3 Engine Indicationndication & Crew Alerting Systemystem (EICAS)
Garmin G1000 Pilot’s Guide for the Cessna Citation Mustang
190-00494-02 Rev. B
82
Engine Indicationndication & Crew Alerting Systemystem
SYSTEM
OVERVIEW
FLIGHT
INSTRUMENTS
EICAS
AUDIO PANEL
& CNS
FLIGHT
MANAGEMENT
HAZARD
AVOIDANCE
AFCS
ADDITIONAL
FEATURES
APPENDICES
INDEX
In the event of a display failure, depending on the failed display(s), the remaining display(s) may be re-configured to present Primary Flight Display (PFD) symbology together with EICAS information (refer to the System Overview for more information about reversionary mode).
In reversionary mode, the data is pared down to a single column on any display. The N1, N2, and ITT indicators are presented in the same way, but all other parameters are shown as readouts only. The following are not shown:
• Total fuel• Cabin altitude rate• Destination elevation• Battery current• Aileron and rudder trim
　
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(36)