User manual GARMIN G1000-CESSNA MUSTANG COCKPIT REFERENCE GUIDE
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Manual abstract: user guide GARMIN G1000-CESSNA MUSTANGCOCKPIT REFERENCE GUIDE
Detailed instructions for use are in the User's Guide.
[. . . ] G1000
®
Integrated Flight Deck
Cockpit Reference Guide for the Cessna Citation Mustang
FLIGHT INSTRUMENTS NAV/COM/TRANSPONDER/AUDIO PANEL AUTOMATIC FLIGHT CONTROL SYSTEM GPS NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ADDITIONAL FEATURES ABNORMAL OPERATION ANNUNCIATIONS & ALERTS APPENDIX INDEX
Copyright © 2006, 2007 Garmin Ltd. All rights reserved.
This manual reflects the operation of System Software version 0435. 09 or later for the Cessna Citation Mustang. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions.
Garmin International, Inc. , 1200 East 151st Street, Olathe, Kansas 66062, U. S. A. Tel: 913/397. 8200 Fax: 913/397. 8282 Garmin AT, Inc. , 2345 Turner Road SE, Salem, OR 97302, U. S. A. [. . . ] Select the 360 Softkey to return to the 360° default display. Rotate the Joystick clockwise to display a larger area or rotate counterclockwise to display a smaller area. Color
Red Yellow Black
4)
Terrain/Obstacle Location
Terrain/Obstacle above or within 100' below or above aircraft altitude. Terrain/Obstacle between 100' and 1000' below current aircraft altitude. Terrain/Obstacle is more than 1000' below aircraft altitude.
Potential Impact Point Projected Flight Path
100' Threshold
Unlighted Obstacle
1000'
Unlighted Obstacle (Height is less than 1000' AGL)
Lighted Obstacle (Height is less than 1000' AGL)
Unlighted Obstacle (Height is greater than 1000' AGL)
Lighted Obstacle (Height is greater than 1000' AGL)
Potential Impact Points
TAWS Colors & Symbols
Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI)
Phase of Flight
Enroute Terminal Approach Departure
Level Flight
700 ft 350 ft 150 ft 100 ft
Descending
500 ft 300 ft 100 ft 100 ft
Terrain & Obstacle Clearance Thresholds for Alerting
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-01 Rev. C
Hazard Avoidance Premature Descent Alert (PDA)
700
Height Above Terrain (Feet)
600
500
400
300
200
"Too Low, Terrain"
100
Runway 1 Threshold
2
3
4
5
6
7
8
9
10
11
12
13
14
15
Distance From Destination Airport (nm)
PDA Alerting
Excessive Descent Rate Alert (EDR)
6000 5500 5000 4500 4000 3500 3000 2500 2000 1500 1000 500 0
Height Above Terrain (Feet)
IN "S
" TE RA K
"PULL UP"
2000
4000
6000
8000
10000
12000
Descent Rate
Excessive Descent Rate Alerting
190-00600-01 Rev. C Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
39
Hazard Avoidance Negative Climb Rate After Takeoff Alert (NCR)
The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the pilot when the system determines that the aircraft is losing altitude (closing upon terrain) after takeoff. The aural message "Don't Sink" is given for NCR alerts, accompanied by an annunciation and a pop-up terrain alert on the display.
Height Above Terrain (Feet)
1000
800
600
400
"DON'T SINK"
200
0
20
40
60
80
100
120
140
Altitude Loss (Feet)
Height Above Terrain (Feet)
1000 900 800 700 600 500 400 300 200 100
0
"DON'T SINK"
500
1000
1500
2000
2500
3000
3500
4000
Sink Rate (Feet Per Minute)
Negative Climb Rate (NCR) Alerting
"Five-Hundred" Aural Alert
The purpose of the aural alert message "Five-hundred" is to provide an advisory alert to the aircrew that the aircraft is five-hundred feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message "Five-hundred" is heard.
Enable/Disable Aviation Data
1) 2) 3) While the TAWS Page is displayed, press the MENU Key. Turn the small FMS Knob to select "Show (or Hide) Aviation Data". Press the ENT Key.
40
Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-01 Rev. C
Hazard Avoidance TAWS Inhibit
Inhibit TAWS While the TAWS Page is displayed, press the INHIBIT Softkey. 2) Turn the small FMS Knob to select `Inhibit TAWS'. Enable TAWS While the TAWS Page is displayed, press the INHIBIT Softkey. OR 1) While the TAWS Page is displayed, press the MENU Key. 2) Turn the small FMS Knob to select `Enable TAWS'. 3) Press the ENT Key.
NOTE: If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach, a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix.
AIRBORNE COLOR WEATHER RADAR
WARNING: Begin transmitting only when it is safe to do so. If it is desired to transmit while the aircraft is on the ground, no personnel or objects should be within 11 feet of the antenna. CAUTION: In Standby Mode, the antenna is parked at the center line. It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly.
Displaying Weather on the Weather Radar Page
1) 2) Turn the large FMS Knob to select the Map Page Group. Turn the small FMS Knob to select the Weather Radar Page.
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190-00600-01 Rev. C Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang
Hazard Avoidance
3) 4) Select the MODE Softkey. [. . . ] · Updated database obtained from the Garmin website. · Existing 010-00330-42 Supplemental Database SD Cards from both PFD and MFD.
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Garmin G1000 Cockpit Reference Guide for the Cessna Citation Mustang 190-00600-01 Rev. C
Appendix
After the data has been copied to the appropriate data cards, perform the following steps: 1) Insert one SD card in the bottom card slot of the MFD and one in the bottom card slot of each PFD. The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD. [. . . ]
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