Garmin G1000-tiger Ag-5B Manual
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Garmin G1000-tiger Ag-5B System Guide
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Cockpit Reference Guide for the Tiger AG-5B
Copyright 2005 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reects the operation of System Software version 0464.00 or later for the Tiger AG-5B. 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. Tel: 503/391.3411 Fax 503/364.2138 Garmin (Europe) Ltd., Unit 5, The Quadrangle, Abbey Park Industrial Estate, Romsey, Hampshire S051 9DL, U.K. Tel: 44/0870.8501241 Fax: 44/0870.8501251 Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099 Web Site Address: www.garmin.com Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. Garmin is a registered trademark of Garmin Ltd. or its subsidiaries, and G1000 is a trademark of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. NavData is a registered trademark of Jeppesen, Inc.; Stormscope is a registered trademark of L-3 Communications; and XM is a registered trademark of XM Satellite Radio, Inc.
190-00616-00 Rev. A
Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B
Printed in the U.S.A.
WARNINGS, CAUTIONS, & NOTES
WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain function. The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during ight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certied for use in applications requiring a certied terrain awareness system. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data. WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes. WARNING: The Garmin G1000, as installed in Tiger AG-5B aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the G1000. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit. WARNING: For safety reasons, G1000 operational procedures must be learned on the ground. WARNING: The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary signicantly from the altitude displayed by pressure altimeters, such as the GDC 74A Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft. WARNING: The Jeppesen database used in the G1000 system must be updated regularly in order to ensure that its information remains current. Updates are released every 28 days. A database information packet is included in the G1000 package. Pilots using an outdated database do so entirely at their own risk. WARNING: The basemap (land and water data) must not be used for navigation, but rather only for non-navigational situational awareness. Any basemap indication should be compared with other navigation sources. CAUTION: The illustrations in this guide are only examples. Never use the G1000 to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Airmans Information Manual (AIM) recommend avoiding by at least 20 miles any thunderstorm identied as severe or giving an intense radar echo.
RECORD OF REVISIONS
Part Number 190-00616-00 (Rev. A)
Change Summary Initial Release.
Revision Date of Revision Affected Pages A 7/05 i-Index-2
Description Initial release
This page intentionally left blank.
TABLE OF CONTENTS SECTION 1: SYSTEM OVERVIEW. 1-1
1.1 1.2 1.3 1.4 1.5 PFD/MFD Controls... 1-2 PFD Softkeys.. 1-4 MFD Softkeys... 1-6 MFD Page Groups... 1-8 Backlighting... 1-8
Code Selection.. 4-4 Flight ID Reporting.. 4-4
SECTION 5: AUDIO PANEL.. 5-1
5.1 COM Radio Selection.. 5-2 5.2 Marker Beacon Receiver.. 5-2 Marker Beacon Signal Sensitivity.. 5-2 5.3 Nav Radio Audio Selection.. 5-2 5.4 Intercom System (ICS) Isolation. 5-3 5.5 Intercom Squelch Control.. 5-3 5.6 Digital Clearance Recorder with Playback Capability... 5-4
SECTION 2: FLIGHT INSTRUMENTS.. 2-1
2.1 Airspeed Indicator.. 2-3 Speed Indication.. 2-3 Speed Ranges... 2-3 Airspeed Trend Vector.. 2-3 Vspeed References.. 2-3 2.2 Attitude Indicator.. 2-3 2.3 Altimeter... 2-4 Altitude Reference Bug.. 2-4 Altitude Trend Vector... 2-4 Barometric Setting Box.. 2-4 2.4 Vertical Deviation/Glideslope Indicator. 2-4 2.5 Marker Beacon Annunciations.. 2-4 2.6 Vertical Speed Indicator.. 2-5 2.7 Horizontal Situation Indicator (HSI). 2-5 Course Pointer.. 2-6 Course Deviation Indicator (CDI).. 2-6 Bearing Pointers and Information Windows. 2-6 Navigation Source.. 2-7 3.1 Engine Display.. 3-1 3.2 Lean Engine Display.. 3-1 Cylinder Select.. 3-1 3.3 Engine System Display.. 3-2 4.1 4.2 4.3 4.4 4.5 Radio Status Indications.. 4-3 Volume... 4-3 Automatic Squelch.. 4-3 Quickly Activating 121.500 MHz. 4-3 Frequency Auto-tuning... 4-3 Auto-tuning on the PFD... 4-3 Auto-tuning on the MFD.. 4-3 4.6 Transponder... 4-4 Mode Selection... 4-4 Ground Mode (Automatic).. 4-4 Reply Status... 4-4
SECTION 6: AUTOMATIC FLIGHT CONTROL. 6-1 SECTION 7: NAVIGATION.. 7-1
7.1 Navigation Map Page.. 7-1 Select the MAP Page Group... 7-1 7.2 Direct-to Navigation... 7-1 Direct-to Navigation from the MFD.. 7-1 Direct-to Navigation from the PFD. 7-2 7.3 Airport Information.. 7-3 Select the Airport Information Page.. 7-3 Enter a Waypoint Facility Name or City Location. 7-3 Access Runway Information... 7-3 Access Frequency Information.. 7-3 7.4 Intersection Information.. 7-4 Select the Intersection Information Page.. 7-4 Access Information on an Intersection.. 7-4 7.5 NDB Information... 7-4 Select the NDB Information Page.. 7-4 View Information on a Specic NDB.. 7-4 7.6 VOR Information... 7-5 Select the VOR Information Page.. 7-5 Access Information on a VOR.. 7-5 7.7 User Waypoint Information Page.. 7-5 7.8 Nearest Airports... 7-5 Nearest Airport Information on the MFD.. 7-5 Nearest Airports Information on the PFD.. 7-6 7.9 Nearest Intersections.. 7-6 Select the Nearest Intersections Page.. 7-6 View Information on the Nearest Intersection. 7-7 7.10 Nearest NDB.. 7-7 Select the Nearest NDB Page.. 7-7 Access Information on a Specic NDB. 7-7 v
Figure 1-2 PFD Top Level Softkeys
INSET Press to display the Inset Map in the lower left corner of the PFD. OFF Press to remove the Inset Map DCLTR (3) Press momentarily to select the desired amount of map detail. The declutter level appears adjacent to the DCLTR softkey. No declutter: All map features are visible Declutter 1: Declutters land data Declutter 2: Declutters land and SUA data Declutter 3: Declutters large NAV data remaining (removes everything except the active ight plan) TRAFFIC Press to display TIS trafc on the map. TOPO Press to display topographical data (i.e., coastlines, terrain, rivers, lakes, etc.) and elevation scale on the inset map. TERRAIN Press to display terrain information on the inset map. STRMSCP (optional) Press to display the Stormscope lightning data on the inset map (within a 200 nm radius of the aircraft). NEXRAD (optional) Press to display NEXRAD precititation data on the inset map. XM LTNG (optional) Press to display the XM Radio lightning data on the inset map. BACK Press to return to the previous level softkey conguration. PFD Press to display the additional softkeys for additional congurations to the PFD. METRIC Press to display the current and reference altitudes in meters, in addition to feet. Pressing the metric softkey also changes the barometric setting to hectopascals.
DFLTS Press to reset default settings on the PFD. BRG1 (bearing) Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the the appropriate information. NAV1 Displays NAV1 waypoint frequency or identier and DME information in the BRG1 information window. GPS Displays GPS waypoint identier and GPS distance information in the BRG1 information window. OFF Removes the BRG1 information window. 360 HSI Press to display the 360 compass rose. ARC HSI Press to display the 140 viewable arc. BRG2 (bearing) Press to cycle through the following Nav sources, making the pointer the indicator for the corresponding source and displaying the the appropriate information. NAV2 Displays NAV2 waypoint frequency or identier and DME information in the BRG2 information window. GPS Displays GPS waypoint identier and GPS distance information in the BRG2 information window. OFF Removes the BRG2 information window. STD BARO Press to set the barometric pressure to 29.92 inches of mercury (1013 hPa by pressing the METRIC softkey). BACK Press to return to the previous level softkeys. OBS Press to select OBS mode on the CDI when navigating by GPS (only available with active leg). CDI Press to change navigation mode on the CDI between GPS, VOR1 and VOR2. XPDR Press to display the transponder mode selection softkeys. STBY Press to select standby mode. ON Press to select mode A.
ALT Press to select altitude reporting mode. VFR Press to automatically squawk 1200 (only in the U.S.A., refer to ICAO standards for VFR codes in other countries). CODE Press to display transponder code selection softkeys 0-7. 0 through 7 Press numbers to enter code. IDENT Press to provide special aircraft position identication to Air Trafc Control (ATC). BKSP Press to remove numbers entered one at a time. BACK Press to return to the previous level softkeys.
IDENT Press to provide special aircraft position identication to Air Trafc Control (ATC). BACK Press to return to the previous level softkeys.
(optional) XM LTNG BACK ALERTS
DCLTR-1 DCLTR-2 DCLTR-3
Press the BACK or OFF softkey to return to the top level softkeys
Figure 1-3 PFD Softkey Flow Chart 1
Press the DFLTS softkey to change the PFD metric values to standard
Press the STD BARO or BACK softkeys to return to the top level softkeys
Figure 1-4 PFD Softkey Flow Chart 2 Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B 1-5
Press the BACK softkey to return to the top level softkeys
CODE IDENT BACK ALERTS
IDENT BKSP BACK ALERTS
Figure 1-5 PFD Softkey Flow Chart 3
IDENT Press to provide special aircraft position identication to Air Trafc Control (ATC). TMR/REF Press to display the Timer/References window. NRST Press to display the Nearest Airports window. ALERTS Press to display the Alerts window.
ENGINE Pressing this softkey makes available the LEAN and SYSTEM and softkeys which in turn access the Lean Page and the System Page, respectively. MAP pressing this softkey enables the following softkeys:
TRAFFIC pressing this softkey displays/ removes Trafc on the Navigation Map. TOPO pressing this softkey displays or removes topographic information on the Navigation Map. TERRAIN pressing this softkey displays/ removes terrain and obstacle data on the Navigation Map. STRMSCP (optional) pressing this softkey displays/removes Stormscope lightning data on the Navigation Map. NEXRAD (optional) pressing this softkey displays/removes precipitation data on the Navigation Map. XM LTNG (optional) pressing this softkey displays/removes XM Radio lightning data on the Navigation Map.
Altitude Reference Bug
The Altitude Reference Bug can be set to any desired altitude. The bug acts as a visual reference to indicate the desired altitude is approaching. To set the altitude reference bug: 1. Turn the ALT knobs to set the altitude reference bug. The small ALT knob sets the hundreds and the large ALT knob sets the thousands. This altitude also appears in the altitude reference box above the altimeter.
Vertical Deviation/Glideslope Indicator
Figure 2-8 Marker Beacon and Vertical Deviation
Altitude Trend Vector
The end of the trend vector displays approximately what the altitude will be in 6 seconds if the current rate of vertical speed is maintained.
VERTICAL SPEED INDICATOR
Vertical Speed Pointer
Figure 2-9 Vertical Speed Indicator
The actual vertical speed is displayed inside the pointer.
HORIZONTAL SITUATION INDICATOR (HSI)
The HSI compass can be displayed as a 360 rose or 140 arc by pressing the PFD softkey, followed by the 360 HSI or the ARC HSI softkey.
Turn Rate Indicator Lateral Deviation Scale Navigation Source Aircraft Symbol Course Deviation Indicator Rotating Compass Rose OBS Mode TO/FROM Indicator Heading Bug Course Pointer Flight Phase Turn Rate and Heading Trend Vector Heading Lubber Line
Figure 2-10 Horizontal Situation Indicator
Turn Rate Indicator and Heading Trend Vector
Each tick mark is at 9 (half standard rate tick mark) and 18 (standard rate tick mark) degrees to the left and right of the lubber line. A wide magenta line displays the current turn rate, up to 24 degrees. A magenta arrowhead appears at 25 degrees. This trend vector provides the pilot with a prediction of what the heading will be in 6 seconds at the present turn rate.
Bearing Pointers and Information Windows
Pressing the PFD softkey provides access to the BRG1 and BRG2 softkeys. The BRG1 pointer is a single line pointer. The BRG2 pointer is a double line pointer.
Bearing 1 Pointer Bearing 2 Pointer
Figure 2-14 Turn Rate Indicator and Heading Trend Vector
The course pointer is a single line arrow (GPS, VOR1 and LOC1) or double line arrow (VOR2 and LOC2) which points in the direction of the set course.
Bearing 1 Information Window Bearing 2 Information Window Figure 2-14 HSI with Bearing Information Distance to Bearing Source Waypoint Identier Course Deviation Lateral Deviation TO/FROM Indicator Scale Figure 2-15 Arc CDI and Compass Rose CDI Bearing Pointer Source Icon Figure 2-15 BRG1 Information Window Distance to Bearing Source Waypoint Identier Bearing Pointer Source Icon Figure 2-16 BRG2 Information Window
Pressing and holding the COM Frequency Toggle key for approximately two (2) seconds automatically tunes the selected COM radio to the emergency frequency.
Following is a list of important codes: 1200 VFR code in the U.S. (please refer to the ICAO standards for VFR codes in other countries). 7000 VFR code commonly used in Europe (please refer to the ICAO standards). 7500 Hijack code. 7600 Loss of communication code. 7700 Emergency code. 7777 Military interceptor operations code (NEVER ENTER THIS CODE). 0000 Code for military use (in the U.S.).
The STBY, ON and ALT softkeys can be accessed by pressing the XPDR softkey. Ground Mode (Automatic) GND is displayed when the aircraft is on the ground.
Figure 4-8 Ground Mode
Flight ID Reporting
If so congured, the Flight ID may be entered in the Timer/Reference window. If conguration is set to SAME AS TAIL the aircraft tail number will always be displayed.
Reply Status When the transponder sends replies to interrogations, an R indication appears momentarily in the reply status eld.
Figure 4-9 Reply Indication
Code Selection 1. 2. Press the XPDR softkey to display the transponder Mode Selection softkeys. Press the CODE softkey to display the transponder Code Selection softkeys, which includes the digit softkeys. Press the appropriate digit softkeys to enter the code in the four-digit code eld of the Transponder Status bar. Five seconds after the fourth digit has been entered, the transponder code becomes activated. When entering a code, press the BKSP softkey as needed to back up and change code digits.
4-4 Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B Figure 4-10 Timer/References Window
SECTION 5 AUDIO PANEL
SECTION 5: AUDIO PANEL
Transmitters (COM3 MIC is unavailable)
Transceiver Audio (COM 3 is unavailable)
Split COM (Not recommended for use in the Tiger AG-5B) Passenger Address Marker Beacon/Mute
Telephone (Unavailable) Speaker Marker Beacon Signal Sensitivity
Aircraft Navigation Radio Audio (ADF, DME and, AUX unavailable on Tiger AG-5B)
Aircraft Navigation Radio Audio
Recorded COM Audio Playback ICS Isolation
VOL/SQ Volume/Squelch VOL Annunciation SQ Annunciation Reversionary Mode
Figure 5-1 Audio Panel Controls
COM RADIO SELECTION
Marker Beacon Signal Sensitivity
The HI SENS key can be pressed for increased marker beacon signal sensitivity.
Pressing the COM1 MIC or COM2 MIC key selects the active transmitter (i.e., microphone). The associated receiver audio (COM1 or COM2) also becomes selected when the COM MIC key is pressed. To prevent deselecting the desired received audio when pressing another COM MIC key, press the already selected COM1 or COM2 key before pressing the other COM MIC key.
Figure 7-9 Nearest Airports Page
Nearest Airport Information on the MFD
Select the Nearest Airports Page 1. 2. Turn the large FMS knob to select the NRST page group. Turn the small FMS knob to select the rst rectangular page icon. Press the APT softkey located at the bottom of the display. The rst airport in the nearest airports list is highlighted. Turn the large FMS knob to highlight the desired airport.
Access Information on a VOR:
1. 2. With the VOR Information Page displayed, press the FMS knob to activate the cursor. Turn the large FMS knob to highlight the desired selection eld (identier, name or closest city). Turn the FMS knobs to enter an identier, name or city and press the ENT key. Press the FMS knob to remove the ashing cursor.
Access Information on a Specic Airport 1.
Access Runway Information for the Selected Airport 1. 2. Press the RNWY softkey located at the bottom of the display. Turn the small FMS knob to select the desired runway.
2. 3. Press the ENT key to display airport information. Press the ENT key again (cursor is on BACK) to return to the list.
Quickly Tune the COM Transceiver to a Nearby Airport Frequency 1. 2. 3. 4. Press the FREQ softkey located at the bottom of the display. Turn either FMS knob to select the desired frequency. Press the ENT key. The selected frequency is placed in the standby frequency tuning box. Press the Frequency Toggle key to place the frequency in the active eld.
Load an Airport COM Frequency into the Active COM 1. Turn the large FMS knob to place the cursor on the desired airport frequency shown in the window. 2. Press the ENT key and the selected frequency will become the standby frequency for the active COM. Press the Frequency Toggle key to make the frequency the active frequency.
Nearest Airports Information on the PFD
Bearing TO Airport Symbol Identier Distance
Primary COM Frequency
Figure 7-10 Nearest Airports Window
Press the NRST softkey to display the PFD Nearest Airports Window.
Figure 7-11 Nearest Intersections Page
View Information on a Specic Airport in the List 1. Turn the large FMS knob to place the cursor on the desired airport identier.
Select the Nearest Frequencies Page
Figure 7-14 Nearest User Waypoints Page
Select the Nearest User Waypoint Page
1. 2. Turn the large FMS knob to select the NRST page group. Turn the small FMS knob to select the fth rectangular page icon.
Turn the large FMS knob to select the NRST page group. Turn the small FMS knob to select the sixth rectangular page icon.
Select and Load the Nearest ARTCC, FSS, or Weather Frequency
1. 2. 3. With the Nearest Frequencies Page selected, press the ARTCC, FSS, or Wx softkey. Turn the large FMS knob to select the frequency. Press the ENT key to load the frequency into the COM frequency standby eld.
displayed. If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside, Ahead < 2 nm is displayed. If the aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside, Within 2 nm is displayed. If the aircraft has entered an airspace, Inside is displayed.
View Additional Details for a Listed Airspace
1. 2. 3. 4. 5. Select the Nearest Airspace Page. Press the FMS knob to activate the cursor. Turn the large FMS knob to scroll through the list, highlighting the desired airspace. Press the ALERTS softkey and turn either FMS knob to select the desired airspace. Press the FMS knob to remove the ashing cursor.
7.14 NEAREST AIRSPACES
View and Quickly Load the Frequency for a Controlling Agency
Figure 7-16 Nearest Airspaces Page
Select the Nearest Airspaces Page. Press the FREQ softkey and turn either FMS knob to select the desired frequency. Press the ENT key to load the frequency into the COM frequency standby eld.
Select the Nearest Airspaces Page
1. 2. Turn the large FMS knob to select the NRST page group. Turn the small FMS knob to select the seventh rectangular page icon.
Airspace Alerts Box
If the projected course takes the aircraft inside an airspace within the next ten minutes, Ahead is
To create a new ight plan using the MFD: 1. 2.
Figure 8-7 Delete Flight Plan Conrmation Garmin G1000 Cockpit Reference Guide for the Tiger AG-5B 8-3
Figure 8-10 Create FPL on MFD
Press the FPL key and press the small FMS knob to activate the cursor. Turn the small FMS knob to enter the rst character of the ight plan starting identier. Turn the large FMS knob to move the cursor to the next character eld. Turn the small FMS knob to enter the next character. Continue this process until the desired identier is entered. Press the ENT key and the cursor is now ready for entering of the next ight plan waypoint. Repeat steps 2 through 5 to enter the identier for each additional ight plan waypoint. Once all waypoints have been entered, press the FMS knob to return to the Active Flight Plan Window.
Turn the small FMS knob to display the Waypoint Information Page. Turn the small FMS knob to enter the rst character of the identier of the departure waypoint. Turn the large FMS knob to move the cursor to the next character eld. Repeat using the FMS knobs until the desired identier has been entered.
5. 6. 7.
Figure 8-11 Waypoint Info Window
4. 5. 6.
Press the ENT key. Repeat step number 3 to enter the identier for each additional ight plan waypoint. When all waypoints have been entered, press the FMS knob to return to the Flight Plan Catalog Page. The new ight plan is now in the list.
Figure 8-12 Creating Flight Plan on the PFD
LOAD A DEPARTURE
See the Procedures section for a discussion on loading and activating departure procedures.
Create a new ight plan using the PFD
NOTE: A ight plan cannot be entered using the PFD if another ight plan is active. NOTE: After the rst leg is entered (using the PFD only), it is immediately activated.
LOAD AN ARRIVAL
See the Procedures section for a discussion on loading and activating arrival procedures.
8.10 LOAD AN APPROACH
See the Procedures section for a discussion on loading and activating approach procedures.
8.11 REMOVE A DEPARTURE, ARRIVAL, OR APPROACH FROM A FLIGHT PLAN
1. With the Active or Stored Flight Plan Page displayed, press the small FMS knob to activate the cursor. Turn the large FMS knob to highlight the title for the approach, departure or arrival to be deleted. Titles appear in white directly above the procedures waypoints. Press the CLR key to display a conrmation window. With OK highlighted, press the ENT key to remove the selected procedure.
Turn the FMS knobs to make the desired changes, then press the ENT key. Press the FMS knob to return to the Flight Plan Catalog Page.
8.14 DELETE A WAYPOINT FROM THE FLIGHT PLAN
Figure 10-9 Weather Data Link Page
LTNG pressing the LTNG softkey shows the location of cloud-to-ground lightning strikes. The display is updated every ve minutes.
NOTE: Strikes depicted represent cloud to ground strikes within a 2 km radius of the actual strike location. Therefore, the exact location of the strike is not displayed.
NEXRAD press the NEXRAD softkey to show NEXRAD weather and radar coverage information. Areas where radar coverage is not available will be shown in grayish-purple. The display is updated every ve minutes.
CELL MOV pressing the CELL MOV softkey shows storm cell movement by displaying an arrow. pointing in the direction of predicted movement. The display is updated every 12 minutes. SIG/AIR pressing the SIG/AIR softkey shows SIGMET and AIRMET information. The display is updated every 12 minutes. METAR press the METAR softkey to graphically display METARs. METARS are shown as colored ags at airports providing METAR reports. The display is updated every 12 minutes. MORE WX press the MORE WX softkey to display the following group of softkeys for additional weather control: SFC pressing the SFC softkey for Surface Analysis shows current or forecast conditions. Forecasts are available for intervals of Current, 12, 24, 36, and 48 hours. Press the softkey corresponding to the desired forecast. The closest city forecast information is displayed in the legend. The display is updated every 12 minutes. FRZ LVL press the FRZ LVL softkey to display contour lines for freezing levels. The display is updated every 12 minutes. WIND press the WIND softkey to show wind speed and direction at a selected altitude from the ground up to 42,000 feet in 3,000 foot increments. After pressing the WIND softkey, press the softkey corresponding to the desired winds aloft altitude. The display is updated every 12 minutes. COUNTY pressing the COUNTY softkey provides specic public awareness and protection weather warnings for Tornado, Severe Thunderstorm, and Flood conditions provided by the National Weather Service (NWS). The display is updated every 5 minutes. CYCLONE pressing the CYCLONE softkey shows the current location of cyclones (hurricanes and tropical storms) and their projected track at various time intervals. The display is updated every 12 minutes.
NOTE: Trafc Information Service (TIS) is only available when the aircraft is within the service volume of a TIS capable terminal radar site.
Trafc Advisory, aircraft is 400 above & Trafc out of Trafc Mode descending, moving in the direction of the line range
Displaying Trafc on the Trafc Map Page
1. 2. 3. Turn the large FMS knob to select the Map Page Group. Turn the small FMS knob to select the second rectangular page icon. Press the OPERATE softkey to begin displaying trafc. TIS OPERATIING is displayed in the Trafc mode eld. Press the STANDBY softkey to place the system in the Standby mode. TIS STANDBY will be displayed in the Trafc mode eld. Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area.
Last data update Proximity Trafc at same Trafc 1600 above & is older than 6 altitude, level ight & moving climbing, moving in the sec. resulting in in the direction of the line direction of the line Coast mode
Figure 10-11 Trafc Map Page
Displaying Trafc on the Navigation Map
1. 2. Ensure TIS is operating. With the Navigation Map displayed, press the MAP softkey. Press the TRAFFIC softkey. Trafc will now be displayed on the map.
If data is not received for a period longer than 6 seconds, the age of the present data will be displayed in the lower left of of the screen along with the annuciation that the system has entered Coast mode. The system will maintain the trafc display (up to 60 seconds) until the next data reception. If no data is received after 60 seconds, trafc will be removed from the display.
TIS Audio Alert
When a Trafc Advisory (TA) is displayed, an audio alert Trafc is given. Trafc Not Available will be heard whenever TIS service becomes unavailable.
10.5 TERRAIN AND OBSTACLE PROXIMITY
NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75 degrees (north or south).
Color RED YELLOW
Indication WARNING: Terrain/Obstacle at or within 100 below current aircraft altitude. CAUTION: Terrain/Obstacle between 100 and 1000 below current aircraft altitude.
Displaying Terrain and Obstacles on the Terrain Proximity Page
1. 2. 3. Turn the large FMS knob to select the Map Page Group. Turn the small FMS knob to select the last rectangular page icon. If desired, press the VIEW softkey to access the ARC and 360 softkeys. When the ARC softkey is pressed, a radar-like 120 view is displayed. Press the 360 softkey to return to the 360 default display. Rotate the Joystick clockwise to display a larger area or rotate counter-clockwise to display a smaller area.
Display is not receiving valid transponder information. Other Various Red X Indications A red X through any other display eld, such as engine instrumentation elds, indicates that the eld is not receiving valid data.
A red X may be the result of an LRU or an LRU function failure. The Figure 12-5 illustrates all possible ags and the responsible LRUs.
12.4 G1000 SYSTEM MESSAGE ADVISORIES
This section describes various G1000 system message advisories. Certain messages are issued due to an LRU or an LRU function failure. Such messages are normally accompanied by a corresponding red X annunciation as shown previously in the G1000 System Annunciation section.
NOTE: This Section provides information regarding G1000 message advisories that may be displayed by the system. Knowledge of the aircraft, systems, ight conditions, and other existing operational priorities must be considered when responding to a message. Always use sound pilot judgment. The Pilots Operating Handbook Supplement (POHS) takes precedence over any conicting guidance found in this section.
GIA 63 Integrated Avionics Units
GIA 63 Integrated Avionics Units GDC 74A Air Data Computer
GEA 71 Engine Airframe Unit OR GIA 63 Integrated Avionics Unit
GRS 77 AHRS OR GMU 44 Magnetometer
GDC 74A Air Data Computer Figure 12-5 G1000 System Failure Annunciations
GTX 33 Transponder OR GIA 63 Integrated Avionics Units
MFD & PFD Message Advisories
Message DATA LOST Pilot stored data was lost. Recheck settings. XTALK ERROR A ight display crosstalk error has occurred. PFD1 SERVICE PFD1 needs service. Return unit for repair. MFD1 SERVICE MFD1 needs service. Return unit for repair. PFD1 CONFIG PFD1 conguration error. Cong service reqd. MFD1 CONFIG MFD1 conguration error. Cong service reqd. SW MISMATCH GDU software mismatch. Xtalk is off. MANIFEST PFD1 software mismatch. Communication halted. MANIFEST MFD1 software mismatch. Communication halted. PFD1 COOLING PFD1 has poor cooling. Reducing power usage. MFD1 COOLING MFD1 has poor cooling. Reducing power usage. PFD1 KEY KEYSTK Key is stuck. MFD1 KEY KEYSTK Key is stuck. Comments The pilot prole data was lost. System reverts to default pilot prole and settings. The pilot may recongure the MFD & PFD with preferred settings, if desired. The MFD and PFD are not communicating with each other. The G1000 system should be serviced. The PFD and/or MFD self-test has detected a problem. The G1000 system should be serviced.
The PFD and/or MFD conguration settings do not match backup conguration memory. The G1000 system should be serviced. The MFD and PFD have different software versions installed. The G1000 system should be serviced. The PFD and/or MFD has incorrect software installed. The G1000 system should be serviced.
The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the G1000 system should be serviced. A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times. The G1000 system should be serviced if the problem persists.
GDC 74A Message Advisories
Alerts Window Message Comments GDC1 CONFIG GDC1 conguration GDC 74A conguration settings do not match those of backup conguration error. Cong service reqd. memory. The G1000 system should be serviced. MANIFEST GDC1 software The GDC 74A has incorrect software installed. The G1000 system should be mismatch. Communication halted. serviced. BACKUP PATH Airdata using backup The GDC 74A is using a backup communications data path. The G1000 system data path. should be serviced when possible.
Miscellaneous Message Advisories
Alerts Window Message Comments FPL WPT LOCK Flight plan waypoint Upon power-up, the G1000 system detects that a stored ight plan waypoint is is locked. locked. This occurs when an aviation database update eliminates an obsolete waypoint. The ight plan cannot nd the specied waypoint and ags this message. This can also occur with user waypoints in a ight plan that is deleted. Remove the waypoint from the ight plan if it no longer exists in any database, OR update the waypoint name/identier to reect the new information. FPL WPT MOVE Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved. aviation database update. Verify that stored ight plans contain correct waypoint locations. TIMER EXPIRD Timer has expired. The system noties the pilot that the timer has expired. DB CHANGE Database changed. This occurs when a stored ight plan contains procedures that have been manually Verify user modied procedures. edited. This alert is issued only after an aviation database update. Verify that the user-modied procedures in stored ight plans are correct and up to date. FPL TRUNC Flight plan has been This occurs when a newly installed aviation database eliminates an obsolete aptruncated. proach or arrival used by a stored ight plan. The obsolete procedure is removed from the ight plan. Update ight plan with current arrival or approach. APPR VPROF Approaching VNAV Aircraft is approaching VNAV prole. Prepare to climb or descend to meet VNAV prole. prole. APPR TRG ALT Approaching target Aircraft is approaching target altitude. Prepare to level aircraft. altitude.
Miscellaneous Message Advisories (Cont.)
Alerts Window Message Comments LOCKED FPL Cannot navigate locked This occurs when the pilot attempts to activate a stored ight plan that contains ight plan. locked waypoint. Remove locked waypoint from ight plan. Update ight plan with current waypoint. WPT ARRIVAL Arriving at waypoint Arriving at waypoint [xxxx], where [xxxx] is the waypoint name. -[xxxx] STEEP TURN Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to turn. INSIDE ARSPC Inside airspace. The aircraft is inside the airspace. ARSPC AHEAD Airspace ahead less Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace within 10 minutes. than 10 minutes. ARSPC NEAR Airspace near and Special use airspace is near and ahead of the aircraft position. ahead. ARSPC NEAR Airspace near less Special use airspace is within 2 nm of the aircraft position. than 2 nm. LEG UNSMOOTH Flight plan leg will The approaching ight plan waypoints are too close to allow for smooth turns. not be smooth. Prepare for steep turns ahead and expect noticeable course deviations. APPR INACTV Approach is not The system noties the pilot that the loaded approach is not active. Activate apactive. proach when required. SLCT AUTOSEQ Select auto The system noties the pilot to select auto-sequence mode. Press the OBS softkey to sequence mode. deactivate the OBS mode. The system noties the pilot to load the approach frequency for the appropriate NAV SLCT FREQ Select appropriate frequency for approach. receiver. Select the correct frequency for the approach. SLCT NAV Select NAV on CDI for The system noties the pilot to set the CDI to the correct NAV receiver. Set the CDI approach. to the correct NAV receiver. NO WGS84 WPT Non WGS 84 The selected waypoint [xxxx] does not use the WGS 84 datum. Cross-check position waypoint for navigation -[xxxx] with alternate navigation sources. TRAFFIC FAIL Trafc device has The trafc information system TIS has failed. The G1000 system should be serviced. failed. STRMSCP FAIL Stormscope has Stormscope has failed. The G1000 system should be serviced. failed. Stormscope is using the backup communication path. The G1000 system should be BACKUP PATH Stormscope using backup path. serviced when possible.
NO.: 0824 Rev C TO: DATE: SUBJECT: REVISION C: All G1000/G900X/G950 Owners and Operators 20 November 2009 GDU 104X CRS/BARO Knob Interference Added note regarding Service Bulletin 0823 in Affected Products section
AFFECTED PRODUCTS NOTE The knob interference issued described in this service alert is resolved by complying with Service Bulletin 0823 Revision C, therefore units that comply with SB0823 Rev C are not affected by this alert. All G1000/G900X/G950 installations with the following 10-inch GDU 104X displays are affected: Unit Garmin Part Number 011-00972-00 011-00972-02 011-00972-03 GDU 1042 GDU 1043 GDU 1044 GDU 1044B 011-01080-00 011-01079-00 011-01078-01 011-01274-00 Affected Serial Number Range 86500310 - - - - - - - - 51201502
NOTE GDU 104X installations with GDU software version 3.02 and later can view unit serial numbers on the AUX SYSTEM STATUS page. Refer to Figure 1 for an example.
Copyright 2009 Garmin Ltd. or its subsidiaries All Rights Reserved Except as expressly provided herein, no part of this document may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express prior written consent of Garmin. Garmin hereby grants permission to download a single copy of this document and of any revision to this document onto a hard drive or other electronic storage medium to be viewed and to print one copy of this document or of any revision hereto, provided that such electronic or printed copy of this document or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this document or any revision hereto is strictly prohibited.
Example GDU 104X Serial Numbers
Figure 1 NOTE If the GDU 104X serial number on the AUX SYSTEM STAUS page displays 0 or if the GDU software version does not display the unit serial numbers, proceed to Step 1 of the IMMEDIATE ACTION REQUIRED section of this service alert. The following G1000-equipped aircraft may include one or more of the affected GDU 104X displays listed above. Cessna 172R/172S/182T/T182T/206H/T206H Cessna 350/400 Columbia 350/400 Diamond DA40/40F/40D/DA42 Mooney M20M/M20R/M20TN Piper PA 32 Saratoga Quest Kodiak 100 Hawker Beechcraft G36 Bonanza Hawker Beecncraft G58 Baron Tiger AG-5B All G900X/G950 aircraft installations may also include one or more of the affected GDU 104X displays listed above.
Service Alert 0824 November 20, 2009
Page 2 of 4 Revision C
DESCRIPTION Garmin has identified an issue, whereby the large (outer) BARO knob and the small (inner) CRS knob may interfere with each other.
Small (inner) CRS Knob
Large (outer) BARO Knob
Figure 2 IMMEDIATE ACTION REQUIRED PFD and MFD CRS/BARO Knob Interference Test 1. Apply power to the G1000/G900X/G950. 2. Press the CDI softkey on the Primary Flight Display(s) (PFD) to enter VOR mode on the HSI. 3. Rotate the large (outer) BARO knob (refer to Figure 2) a minimum of three complete revolutions in each direction while monitoring the Horizontal Situation Indicator/Digital Course Indicator (refer to Figure 3) on the PFD. If a change in the Horizontal Situation Indicator/Digital Course Indicator is produced while turning the BARO knob contact your local Garmin Service Center or OEM Dealer to replace the knobs. NOTE In some installations the Digital Course Indicator does not display unless the field is actively being edited. In these instances, if the Digital Course Indicator does not appear while turning the BARO knob, no interference is present. 4. Rotate the small (inner) CRS knob (refer to Figure 2) a minimum of three complete revolutions in each direction while monitoring the Barometric Altimeter Setting (refer to Figure 3) on the PFD. If a change in the Barometric Altimeter Setting is produced while turning the CRS knob contact your local Garmin Service Center or OEM Dealer to replace the knobs. 5. Repeat Steps 3 and 4 for each affected GDU. NOTE When testing the Multi Function Display (MFD), the indications must be monitored on the PFD.
Page 3 of 4 Revision C
Barometric Altimeter Setting
Horizontal Situation Indicator/Digital Course Indicator
Figure 3 MAINTENANCE RECORDS If no interference is observed, the pilot performing the check should make the following aircraft logbook entry: On dd/mm/yyyy the CRS/BARO knobs on installed displays were checked for interference with none found per Garmin Service Alert 0824. Signed - (pilot name here)
Page 4 of 4 Revision C
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