Garmin 0060200 AIRCRAFT MOUNTED WEATHER RADAR TRANSMITTER User Manual 190 00498 00 0A indd
Garmin International Inc AIRCRAFT MOUNTED WEATHER RADAR TRANSMITTER 190 00498 00 0A indd
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Contents
- 1. PILOT MANUAL
- 2. INSTALLATION MANUAL
PILOT MANUAL
G1000 TM hazard avoidance pilot’s guide for the Cessna Citation Mustang Preliminary 190-00498-00_0A.indd 1 3/1/2005 10:33:38 AM Record of Revisions Revision Date of Revision Revision Page Range Draft 03/01/05 7-1 – 7-53 Description Pr el im in ar Initial release. Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00_0A.indd 2 190-00498-00 Draft 3/1/2005 10:33:38 AM WEATHER 7.1 WEATHER This document describes the Hazard Avoidance features of the G1000 system. The main hazards to flight safety are flying in or near weather, flying in close proximity to the terrain and other flight traffic in close proximity. CAUTION: GDL 69A NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays and relative age of the data that can be received, NEXRAD weather data should not be used for short-range avoidance of weather. The information contained in this section assumes understanding of the G1000 Multi Function Display. This section is divided into groups as follows: Weather • GDL 69A (XM Weather) • GWX 68 • WX 500 Stormscope WARNING: Use of any GDL 69A Weather Product for thunderstorm penetration is prohibited. Weather information provided by the GDL 69 is approved only for weather avoidance, not penetration. Pr el • TIS (Traffic Information System) • TAS (Traffic Advisory System) im Traffic in • Terrain Proximity • TAWS (Terrain Awareness Warning System) ar TAWS/Terrain 190-00498-00 Draft 190-00498-00_0A.indd 1 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-1 3/1/2005 10:33:39 AM WEATHER GDL 69A WEATHER AND DIGITAL AUDIO ENTERTAINMENT Radio IDs The GDL 69A are shipped with a Data Radio ID and an Audio Radio ID. You must obtain the Radio IDs of your receiver(s) before subscribing to XM services. The IDs are attached to the XM Satellite Radio Activation Instructions sheet included with the unit. They are also printed on a label on the back of the unit and are displayed on the XM Information Page. Contact the installer if you are unable to locate the Radio IDs. The GDL 69A is a remote sensor that is capable of receiving XM Weather and displaying it on the G1000 Multi Function Display and the Primary Flight Display Inset Map. The GDL 69A is also capable of receiving XM Radio Services. XM Weather and XM Radio operate in the Sband frequency range to provide continuous uplink capabilities at any altitude throughout North America. im Pr el NOTE: Refer to the G1000 Option pilot’s guide for information on the XM entertainment radio segment of the GDL 69A. 7-2 190-00498-00_0A.indd 2 Turn the large FMS knob to select the Auxiliary Page Group. Turn the small FMS knob to display the AUX - XM Page. ar 1. To activate the XM Radio Weather Service: 2. Press the INFO softkey to display the XM Information Page. 3. Contact XM Satellite Radio through the Internet or by telephone. Follow the directions provided by XM Satellite Radio. 4. Verify that the desired services are activated and press the DONE softkey. 5. Turn the large FMS knob to highlight ‘YES’ or ‘NO.’ Press the ENT key to complete activation. in NOTE: Before the GDL 69A can be used, the unit must be activated by XM Satellite Radio. The XM Satellite Radio Activation Instruction Sheet contains important information required to initiate XM Satellite Radio Subscription for the GDL 69A. This sheet was given to the aircraft owner at the time of delivery. Activating XM Radio Services Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:39 AM WEATHER Audio Radio ID ar Data Radio ID INFO Softkey Pr el im in Weather Products DONE Softkey Figure 7.1.1 XM Information Page 190-00498-00 Draft 190-00498-00_0A.indd 3 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-3 3/1/2005 10:33:39 AM WEATHER GDL 69 WEATHER Complete GDL 69 capabilities include: Flight Information Services (FIS) weather information provided by the GDL 69 is displayed on the following MFD Maps and Pages: • Graphical NEXRAD Data (NEXRAD) • Graphical METAR Data (METAR) • Textual METAR Data • Navigation Map Page (NEXRAD and XM Lightning only) • Textual Terminal Aerodrome Forecasts (TAF) • City Forecast Data • Weather Data Link Page (complete GDL 69 capability) • Graphical Wind Data (WIND) • Nearest Pages (NEXRAD and XM Lightning only) • Graphical Echo Tops (ECHO TOP) • Airport Information Page (NEXRAD and XM Lightning only) ar im • AUX - Trip Planning Map (NEXRAD and XM Lightning only) • Graphical Lightning Strikes (XM LTNG) el • WPT - Weather Information Page - part of the WPT - Airport Information Page (METAR and TAF information only) Pr FIS weather information is also displayed on the Primary Flight Display Inset Map. See the G1000 PFD Pilot’s Guide for more information. NOTE: Temporary Flight Restrictions (TFRs) are displayed on all pages. Cell Movement is always displayed with NEXRAD data. 7-4 190-00498-00_0A.indd 4 • Graphical Storm Cell Movement (CELL MOV) • NEXRAD Radar Coverage (displayed with NEXRAD data) in • Flight Planning Maps (NEXRAD and XM Lightning only) • Graphical Cloud Tops (CLD TOP) • SIGMETs/AIRMETs (SIG/AIR) • Surface Analysis including City Forecasts (SFC) • County Warnings (COUNTY) • Freezing Levels (FRZ LVL) • Hurricane Track (CYCLONE) • Temporary Flight Restrictions (TFR) NOTE: FIS (also known as Flight Information Services - Broadcast, or FIS-B) supplies real-time weather information and other flight advisory information for enhanced situational awareness, 24 hours a day, 7 days a week. Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:40 AM WEATHER Displaying Weather Data on the Navigation Map Page To display weather data on the Navigation Map Page: When appropriately configured, the Navigation Map Page displays NEXRAD, Cell Movement, TFRs and XM Lightning data. This capability improves situational awareness, which makes it easier to relate storm activity to airports, navaids, obstacles and other ground references. 1. Press the MAP softkey. 2. Press the NEXRAD or XM LTNG softkey to display the desired weather. Press the applicable softkey again to remove weather data from the Navigation Map Page. Navigation Map Page Weather Control Softkeys ar im in NEXRAD – pressing the NEXRAD softkey displays NEXRAD weather and coverage information. The NEXRAD option is mutually exclusive with the TOPO, TERRAIN and STORMSCOPE options. That is, when NEXRAD is activated, TOPO and/or TERRAIN and/or STORMSCOPE are turned off. The following softkeys control the display of GDL 69 weather data on the Navigation Map Page: Pr el XM LTNG – pressing the XM LTNG softkey displays XM lightning information. XM Lightning is mutually exclusive with the STORMSCOPE option. 190-00498-00 Draft 190-00498-00_0A.indd 5 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-5 3/1/2005 10:33:40 AM WEATHER im Pr el NEXRAD Weather Cell Movement Status XM Lightning Status in ar NEXRAD Storms/Legend NEXRAD Softkey XM Lightning Softkey Figure 7.1.2 Navigation Map Page Displaying NEXRAD Weather 7-6 190-00498-00_0A.indd 6 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:40 AM WEATHER Navigation Map Setup Options The crew can customize the display of GDL 69 weather data on the Navigation Map Page by using the Map Setup Weather Group Options Menu. The following options are available: • NEXRAD DATA - Turns the display of NEXRAD data and radar coverage on or off and selects the desired display range. ar in NOTE: Stormscope (when installed) and all GDL 69 Weather Products are mutually exclusive. Stormscope is not a GDL 69 Weather Product. • XM LTNG - Turns the display of XM Lightning on or off and selects the desired display range. Figure 7.1.3 Map Setup Options el im • CELL MOVEMENT - Turns the display of storm cell movement on or off. The Cell Movement option is only shown when NEXRAD is turned on. Pr NOTE: In Figure 7.1.3, the Stormscope menu options are only shown when the Stormscope unit is installed. 190-00498-00 Draft 190-00498-00_0A.indd 7 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-7 3/1/2005 10:33:41 AM WEATHER To customize the Navigation Map Page: 4. On the Navigation Map page, press the Menu key. 2. While the ‘Map Setup’ selection is highlighted on the Page Menu, press the ENT key. 3. Turn the small FMS knob to display the group selection window. Turn the FMS knob to select the ‘Weather Group’ and press the ENT key. Displaying Weather Data on the Nearest Pages In addition to the Navigation Map Page, the Nearest Pages displays Stormscope, NEXRAD and XM Lightning data. Pr el im in ar 1. While the Map Setup menu is displayed, turn the large FMS knob to highlight and move between the product selections. When an item is highlighted, turn the small FMS knob to select the desired option and press the ENT key. Figure 7.1.4 Weather Display on the Nearest NDB Page 7-8 190-00498-00_0A.indd 8 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:41 AM WEATHER Displaying METAR and TAF on the Airport Information Page NOTE: TAF is an airport forecast, generally stan` dard around the world. TAF forecasts significant weather changes, temporary changes, probable changes and expected changes in weather conditions. METAR and TAF text is displayed on the Airport Information Page when the WX softkey is pressed. Once the WX softkey is pressed the page title changes from ‘WPT - Airport Information’ to ‘WPT - Weather Information’. The METAR data is first displayed in a decoded fashion, then the raw text is displayed. TAF information is only displayed in its raw form. Turn the large FMS knob to select the WPT Page Group. 2. Turn the small FMS knob to select the Airport Information Page. 3. Press the WX softkey to display METAR and TAF text (METAR and TAF information is updated every 12 minutes). ar 1. Pr el im in NOTE: METAR is the Aviation Routine Weather Report, generally standard around the world. Temperatures are given in Celsius. The atmospheric pressure is reported in hecto pascals everywhere but the US where it is reported in inches of mercury. Standard temperature and atmospheric pressure are 59° F (15°C) and 29.92 in. Hg (1013.2 hPa). To display METAR and TAF text on the Airport Information Page: 190-00498-00 Draft 190-00498-00_0A.indd 9 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-9 3/1/2005 10:33:42 AM METAR Text Pr el im in ar WEATHER TAF Text WX Softkey Figure 7.1.5 METAR and TAF Text Displayed on the Airport (Weather) Information Page 7-10 190-00498-00_0A.indd 10 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:42 AM WEATHER Displaying Weather Data on the Flight Plan Page Maps NEXRAD and XM Lightning Data can be displayed on the AUX - Trip Planning Page Map by pressing the NEXRAD and XM LTNG softkeys. NEXRAD and XM Lightning Data can be displayed on the Flight Plan Page Maps by pressing the NEXRAD and XM LTNG softkeys. ar Displaying Weather Data on the AUX – Trip Planning Page Map Pr el im in Figure 7.1.6 AUX - Trip Planning Page Map Displaying NEXRAD Weather Figure 7.1.7 Stored Flight Plan Page Map Displaying Weather Data 190-00498-00 Draft 190-00498-00_0A.indd 11 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-11 3/1/2005 10:33:43 AM WEATHER Displaying Weather on the Weather Data Link Page To select the Weather Data Link Page: Turn the large FMS knob to select the Map Page Group. 2. Turn the small FMS knob to select the Weather Data Link Page. Pr el im in ar The Weather Data Link Page displays all available weather products. The display of the weather data can either be selected by softkeys located at the bottom of the display or through the Weather Data Link Setup menu. 1. Figure 7.1.8 Weather Data Link Page 7-12 190-00498-00_0A.indd 12 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:43 AM WEATHER Weather Data Link Page Softkeys NEXRAD Limitations The following softkeys perform the GDL 69A weather functions on the Weather Data Link Page: Certain limitations exist regarding the NEXRAD radar displays. Some, but not all, are listed here for the crew’s awareness: NEXRAD Abnormalities Pr el ar im in NOTE: WSR-88D weather surveillance radar or NEXRAD (NEXt generation RADar) is a Doppler radar system that has greatly improved the detection of meteorological events such as thunderstorms, tornadoes and hurricanes. An extensive network of NEXRAD stations provides almost complete radar coverage of the continental United States, Alaska and Hawaii. The unobstructed range of each NEXRAD is 124 nautical miles. • NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics (hail vs. rain, etc). • NEXRAD base reflectivity is sampled at the minimum antenna elevation angle. An individual NEXRAD site cannot depict high altitude storms at close ranges, and has no information about storms directly over the site. • The resolution of displayed NEXRAD data is 2 kilometers. Therefore, when zoomed in on the display, each square block is 2 kilometers. The intensity level reflected by the square will be the highest level sampled within the 2 kilometer square area. NEXRAD – press the NEXRAD softkey to show NEXRAD weather and radar coverage information (both are activated at the same time). Composite data from all of the NEXRAD radar sites in the United States is shown. This data is composed of the maximum reflectivity from the individual radar sweeps. The display of the information is color-coded to indicate the weather level severity. The update rate is every five minutes. Refer to the legend for a description of the color code. There are possible abnormalities regarding displayed NEXRAD images. Some, but not all, of those include: NEXRAD Intensity Colors are used to identify the different NEXRAD echo intensities (reflectivity) measured in dBZ (decibels of Z). “Reflectivity” is the amount of transmitted power returned to the radar receiver. Reflectivity (designated by the letter Z) covers a wide range of signals (from very weak to very strong). So, a more convenient number for calculations and comparison, a decibel (or logarithmic) scale (dBZ), is used. The dBZ values increase as the strength of the signal returned to the radar increases. • Ground Clutter • Strobes and spurious radar data • Sun strobes, when the radar antenna points directly at the sun • Interference from buildings or mountains, which may cause shadows • Military aircraft deploy metallic dust which can cause alterations in radar scans 190-00498-00 Draft 190-00498-00_0A.indd 13 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-13 3/1/2005 10:33:44 AM WEATHER RADAR COVERAGE – The display of Radar Coverage is always active when NEXRAD and ECHO TOPS are selected and indicates the currently available NEXRAD Radar coverage and ECHO TOPS areas by showing the area in a grayishpurple color where information is not being collected. Areas where radar capability exists, but is not active or is off-line, will not be shown as available. Areas where radar coverage is not available will be shown in grayish-purple. The update rate is every five minutes. CLD TOP – press the CLD TOP softkey to show the cloud top altitude determined from satellite imagery. Refer to the legend for a description of the CLOUD TOPS color coding. The update rate is every 15 minutes. Pr el im in ar ECHO TOP – press the ECHO TOP softkey to show the location, elevation and direction the highest radar echo. This may not indicate the top of a storm or clouds, only the highest radar return echo. The information is derived from NEXRAD information and indicates the highest altitude at which precipitation is falling. ECHO TOPS and Radar coverage are activated at the same time. ECHO TOPS are mutually exclusive from both NEXRAD and CLOUD TOPS, that is, when ECHO TOPS is activated, NEXRAD and CLOUD TOPS are removed. Refer to the Legend for a description of the ECHO TOPS coding. The update rate is every 7.5 minutes. NOTE: Cloud Tops and Echo Tops use the same color scaling to represent altitude. Turning on both products at the same time is not allowed. LTNG – pressing the LTNG softkey shows the location of cloud-to-ground lightning strikes. The update rate is every five minutes. NOTE: Strike location falls within a 2 km region. Therefore, the exact location of the strike is not displayed. 7-14 190-00498-00_0A.indd 14 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:44 AM WEATHER NOTE: AIRMETs are broadcast for weather phenomena that potentially affect all aircraft. AIRMET (acronym for “AIRman’s METeorological information) gives valuable information about the following conditions: moderate icing, moderate turbulence, sustained winds 30 knots or greater at the surface, widespread area with a ceiling of less than 1,000 feet and/or visibility less than 3 miles and extensive obscurement of mountains. These are important to light aircraft, that have limited flight capabilities due to lack of equipment and/or instrumentation. ar im in SIG/AIR – pressing the SIG/AIR softkey shows SIGMET and AIRMET information to advise the crew of potentially hazardous weather. The advisory covers an area of at least 3,000 square miles at any one time. The update rate is every 12 minutes. CELL MOV – pressing the CELL MOV softkey shows the storm cells identified by the groundbased system. The movement is depicted by an arrow. The update rate is every 12 minutes. Pr el NOTE: SIGMETs are broadcasted for hazardous weather that is considered of extreme importance to all aircraft. SIGMETs (acronym for “SIGnificant METeorological information”) warn of the following weather hazards: severe icing, severe and extreme turbulence, dust storms, sandstorms or volcanic ash lowering visibility to less than 3 miles. A Convective SIGMET (WST) is issued for hazardous convective weather (such as tornadoes, thunderstorms, hail) and covers severe or greater turbulence, severe icing and low-level wind shear. A localized SIGMET is a significant weather condition occurring at a localized geographical position. 190-00498-00 Draft 190-00498-00_0A.indd 15 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-15 3/1/2005 10:33:44 AM WEATHER When enabled, the following AIRMETs can be displayed: • • • • • Icing Turbulence IFR conditions Mountain obscuration Surface winds ar in METAR – press the METAR softkey to display METARs (METeorological Aviation Reports). METARS are shown as colored flags at airports providing METAR reports. Refer to the legend for a description of the color code. The update rate is every 12 minutes. Refer to the legend for a description of the color coding. Figure 7.1.9 Weather Legends Window el im To view the available legends: Pr LEGEND – press the LEGEND softkey to display the Weather Legend Window. Turn the FMS knob to scroll up or down through the legend list. Press the FMS knob or the ENT key to remove the legend display. The Weather Legends Window describes the graphic symbols and color coding of the information for each product that is active. 7-16 190-00498-00_0A.indd 16 1. Press the LEGEND softkey to display the available legends. 2. Turn either the small or large FMS knob to scroll through the legends if more are available than fit in the window. 3. To return to the previous page and remove the legend window, press the LEGEND, ENT, CLR key, or the FMS knob. OR 4. On the Weather Data Link Page, press the LEGEND softkey which displays the Page Menu Options. Turn either the large or small FMS knob to select ‘Weather Legend’ and press the ENT key. Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:45 AM WEATHER MORE WX – press the MORE WX softkey to display the following group of softkeys for additional weather control: FRZ LVL – press the FRZ LVL softkey to display contour lines for freezing levels. The update rate is every 12 minutes. NOTE: City Forecast and METAR information is only displayed within the installed Aviation Database service area. ar NOTE: When no data is shown at a given altitude for any of the weather features, the data for that altitude has not been received or the data is out of date and has been removed from the display. Wait for the next update. The update rate is every 12 minutes. Pr el im in SFC – pressing the SFC softkey for Surface Analysis shows current or forecast conditions. The city forecasts information is combined with the surface conditions. The SFC softkey label changes to reflect the forecast time selected. Forecasts are available for intervals of 12, 24, 36 and 48 hours. The update rate is every 12 minutes. 190-00498-00 Draft 190-00498-00_0A.indd 17 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-17 3/1/2005 10:33:45 AM WEATHER ar Pr el im in COUNTY – pressing the COUNTY softkey provides specific public awareness and protection weather warnings for Tornado, Severe Thunderstorm and Flood conditions provided by the National Weather Service (NWS). Refer to the Legend for a description of the county warning icon. The update rate is every 5 minutes. CYCLONE – pressing the CYCLONE softkey shows the current location of cyclones (hurricanes) and their projected track at various time intervals. The update rate is 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. The WIND softkey label changes to reflect the winds aloft altitude selected. The update rate is every 12 minutes. 7-18 190-00498-00_0A.indd 18 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:45 AM WEATHER Weather Data Link Page Setup The crew can customize the display of XM Weather data on the Weather Data Link Page using the Weather Setup Menu. To customize the display of weather data on the Weather Data Link Page: 2. While the Weather Setup selection is highlighted on the Page Menu, press the ENT key. If necessary, turn the small FMS knob to select ‘Weather Setup’ and then press the ENT key. While the Weather Data Link Setup Menu is displayed, turn the large FMS knob to highlight and move between the product selections. Turn the small FMS knob to select an option for each selection and press the ENT key. Map Panning Information-Weather Data Link Page Map panning moves the map beyond its current limits without adjusting the map range. When the panning function is selected by pushing the joystick, a panning arrow flashes on the Weather Data Link Page. Panning over AIRMETs, County Warnings, TFRs, Echo Tops, METARs, SIGMET’s and Cell Movement displays text information for the selection. This information is displayed in the same location as the “map pointer information” on the Navigation Map Page. Pr el im in 3. Figure 7.1.10 Weather Data Link Page Menu On the Weather Data Link Page, press the Menu key. ar 1. 190-00498-00 Draft 190-00498-00_0A.indd 19 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-19 3/1/2005 10:33:45 AM WEATHER To display information for selected weather products: Push in the joystick to display the panning arrow. 2. Move the joystick to place the panning arrow on AIRMETs, TFRs, METARs or SIGMETs. Press the ENT key to display pertinent information for the selected product. Panning Information Map Panning Arrow Pr el im in ar 1. Note that pressing the ENT key when panning over an AIRMET or a SIGMET displays an information box that gives the actual text of that alert. Panning over an airport with METAR information does not display more information but allows the crew to press the ENT key and select that Airport’s Information Page and displays the actual text. Pressing the ENT key when panning over a TFR displays TFR specific information for the panned TFR. Figure 7.1.11 Panning on the Weather Data Link Page 7-20 190-00498-00_0A.indd 20 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:46 AM WEATHER Weather Product Symbols Figure 7.1.12 depicts the symbol for each weather product (read from left to right). When a weather product is active, the product symbol is displayed in the lower right of the screen. in ar NEXRAD Cloud Top/Echo Top XM Lightning Cell Movement SIGMETs/AIRMETs METARs City Forecast Surface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings im • • • • • • • • • • • • Pr el Echo Top (Cloud Top and Echo Top Mutually Exclusive) Figure 7.1.12 Weather Product Symbols 190-00498-00 Draft 190-00498-00_0A.indd 21 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-21 3/1/2005 10:33:46 AM WEATHER Weather Product Age Weather Product SIGMETs/AIRMETs City Forecasts County Warnings Cyclone Warnings Echo Tops Freezing Levels METARs Lightning NEXRAD Radar Coverage Cell Movement Surface Analysis TFRs Winds Aloft TAFs Clouds Tops Expires After “n” Minutes 60 60 60 60 30 60 90 30 30 30 30 60 60 60 60 60 Pr el im in ar The times for each of the enabled products are displayed on the right side of the display. Times are based on Zulu times when the data was assembled on the ground, not the time the data was received by the FIS sensor. When the age of a weather product is greater than half of the expiration time, the product time will change from cyan to amber in color. Current weather products use an age stamp, ‘Age: _ _ _’ in minutes. Reported (forecasted) weather products use a date/time stamp; ‘_ _/_ _ /_ _:_ _’. 7-22 190-00498-00_0A.indd 22 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:46 AM WEATHER To select the System Status Page: Although it is the responsibility of the facility that installed the GDL 69A to correct any hardware problems, the crew can perform some quick troubleshooting steps to find the possible cause of a failure. First, ensure that the owner/operator of the aircraft in which the GDL 69A is installed has subscribed to XM Radio and that it has been activated. Perform a quick check of the circuit breakers to ensure the GDL 69A has power applied. If a failure still exists, review the messages listed in the table at the end of this section. The advisory messages may provide insight to a possible failure. For troubleshooting purposes, the Status, Serial Number and Software Version numbers for the GDL 69A are displayed in the LRU Information Window on the System Status Page. 1. Turn the large FMS knob to select the AUX Page Group. 2. Turn the small FMS knob to select the System Status Page. Figure 7.1.19 LRU Information Window Pr el im in ar GDL 69 Troubleshooting 190-00498-00 Draft 190-00498-00_0A.indd 23 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-23 3/1/2005 10:33:47 AM WEATHER Description Antenna is not connected Updating encryption code Loss of signal Acquiring channel audio or information ar Channel not in service Missing channel information in Message CHECK ANTENNA – XM Radio Page, the active channel is replaced with this message UPDATING – XM Radio Page, the active channel is replaced with this message NO SIGNAL – XM Radio Page, the active channel is replaced with this message ; also displayed on the Weather Data Link Page when the signal strength is too low for the receiver LOADING – XM Radio Page, the active channel is replaced with this message OFF AIR – XM Radio Page, the active channel is replaced with this message --- (XM Radio Page, the active channel is replaced with this message ) WEATHER DATA LINK FAILURE – Weather Data Link Page, displayed in the center of the screen in yellow ACTIVATION REQUIRED – Weather Data Link Page, displayed in the center of the screen in yellow im No communication with the GDL 69 within the last five minutes el XM Data receiver is not activated Pr Table 7.1.1 Advisory Messages 7-24 190-00498-00_0A.indd 24 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:47 AM WEATHER GWX 68 AIRBORNE WEATHER RADAR Table 7.1.3 shows six different colors associated with levels of ground mapping return intensity. Ground Mapping Return None Least Reflective Moderate Return Heavy Return Very Heavy Return TBS The GWX 68 Airborne Weather Radar System provides weather detection and ground mapping capability. The primary function of the weather radar system is to find storms along the flight path. Weather detection gives the crew the ability to recognize potentially dangerous thunderstorm cells. The GWX 68 weather radar system also provides ground mapping, giving the ability to distinguish landscape features and bodies of water. Black Cyan Yellow Magenta Red Blue ar Table 7.1.3 Ground Mapping Colors in Weather radar return strength is shown in six different colors to show intensities of rainfall (black, green, yellow, red, magenta, and white). Color Color el Magenta Red Yellow Green Black White Pr Rainfall Rate Very Heavy Rainfall Heavy Rainfall Medium Rainfall Light Rainfall No Rainfall TBS im Table 7.1.2 shows six different colors associated with the levels of rainfall or storm intensity. Table 7.1.2 Weather Radar Rainfall Rate Colors Ground mapped radar return strength is shown using the colors black, cyan, yellow, magenta, and blue. In the ground mapping mode, internal parameters are selected to increase returns from ground targets and decrease returns from weather targets. 190-00498-00 Draft 190-00498-00_0A.indd 25 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-25 3/1/2005 10:33:47 AM WEATHER Operating Modes The G1000 controls and softkeys supply all the controls and functions to operate the weather radar. The radar antenna is automatically stabilized in pitch and roll axes. The crew can manually adjust the radar tilt, gain and range. The crew selects the different weather radar modes. ar el im WX – When selected, the radar is in the weather detection mode. Weather data is shown on the MFD. in STBY – The radar is in standby, the antenna scan stopped, the transmitter inhibited. STBY is shown on the PFD and MFD. The RT (Receiver Transmitter) has a warm-up period of approximately 60 seconds. If any active mode is selected before this period, the WAIT legend will be shown on the PFD and MFD. OFF – Deenergizes the weather radar subsystem. Pr GMAP (GROUND MAPPING) – In this mode, returns from ground targets and decrease returns from weather targets are shown. TEST – In this mode, a test pattern is shown on the MFD to verify system operation. A TEST legend is shown on the MFD. The transmitter radiates microwave energy because it is on. 7-26 190-00498-00_0A.indd 26 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:47 AM Pr el im in ar WEATHER Figure 7.1.20 Radar Initializing 190-00498-00 Draft 190-00498-00_0A.indd 27 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-27 3/1/2005 10:33:48 AM WEATHER Pr el im in ar When TEST mode is selected, a test pattern is shown on the MFD to verify system operation. Figure 7.1.21 Radar Test Pattern 7-28 190-00498-00_0A.indd 28 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:48 AM Pr el im in ar WEATHER Figure 7.1.22 Radar Fail 190-00498-00 Draft 190-00498-00_0A.indd 29 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-29 3/1/2005 10:33:48 AM Pr el im in ar WEATHER Figure 7.1.23 Sector Scan at +26 Degrees 7-30 190-00498-00_0A.indd 30 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:49 AM TAWS/TERRAIN 7.2 TAWS/TERRAIN TAWS/Terrain Proximity Page Operations There are two terrain/obstacle viewing options available (relative to the position of the aircraft), an ARC (120°) display and a 360° default display. TAWS/TERRAIN PROXIMITY PAGE To change the viewing mode between 360° and ARC: The TAWS/Terrain Proximity Page displays the following information: Pr el • Heading Box (North Up, Track Up, DTK Up, HDG Up). Heading on the TAWS/Terrain Proximity Page displays ‘HDG Up’ map data unless there is no valid heading. Additional TAWS only information: 2. Press the VIEW softkey. Then press the ARC softkey. 3. To return to the 360 degree viewing display press the 360 softkey, OR: 4. Press the MENU key. The page menu is displayed with ‘View Arc’ or ‘View 360º’ highlighted. Press the ENT key on the desired selection. in im • Range marking rings (1 nm, 1/2 nm, 2.5/5 nm, 5/10 nm, 12.5/25 nm, 25/50 nm, 50/100 nm and100/200 nm). Select the TAWS/Terrain Proximity Page ar • Current aircraft location. 1. CAUTION: Terrain and obstacle data are provided only as an aid to situational awareness. Aural messages or textual annunciations are displayed to the crew during flight operations regarding the presence of terrain or obstacles. To change the map range on the TAWS/Terrain Proximity Page: 1. Turn the joystick clockwise to zoom out or turn the joystick counter-clockwise to zoom in. Map ranges are 1 nm, 1/2 nm, 2.5/5 nm, 5/10 nm and 12.5/25 nm, 25/50 nm, 50/100 nm and 100/200 nm. • TAWS annunciator box – terrain alerts for both warnings/caution situations and TAWS status information. • North arrow indicator, when not orientated in North-Up display. 190-00498-00 Draft 190-00498-00_0A.indd 31 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-31 3/1/2005 10:33:49 AM TAWS/TERRAIN Aircraft Altitude 100' Threshold 1000' AGL Figure 7.2.1 Terrain Scale • CAUTION • WARNING el YELLOW Indication WARNING: Obstacle height is at or above 100’ below the current aircraft altitude. CAUTION: Obstacle height is between 100’ and 1000’ below the current aircraft altitude. Pr Obstacle Shapes Unlighted Obstacle (Height is less than 1000’ AGL) 190-00498-00_0A.indd 32 ar im RED Each level is associated with a color. The G1000 will adjust colors on the TAWS/Terrain Proximity Page automatically as the aircraft altitude changes. 7-32 Obstacle Color in The TAWS/Terrain Proximity Page displays obstacle data with heights greater than 200 feet Above Ground Level (AGL) located at their geographical position throughout the world. Obstacles are displayed in two levels: Displaying Obstacle Data Lighted Obstacle (Height is less than 1000’ AGL) Unlighted Obstacle (Height is greater than 1000’ AGL) Lighted Obstacle (Height is greater than 1000’ AGL) Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:50 AM TAWS/TERRAIN Navigation Map Display Conditions Displaying Terrain Data on the Navigation Map Page The Map Setup Page Menu has ‘OBSTACLE DATA’ and ‘TERRAIN DATA’ feature On/Off options. The Terrain Obstacle features are summarized in the table below: Obstacle Feature Navigation Map Page OFF OFF NO OBSTACLES DISPLAYED OFF ON CAUTION AND WARNING OBSTACLES DISPLAYED ON OFF CAUTION AND WARNING OBSTACLES DISPLAYED ON ON SAFE, CAUTION, AND WARNING OBSTACLES DISPLAYED To display terrain data on the Navigation Map Page: 1. Press the MAP softkey. 2. Press the TERRAIN softkey. Press the TERRAIN softkey again to remove terrain data from the Navigation Map Page. im in NOTE: Obstacles are only displayed at certain map zoom ranges, on certain map fields, and will only be displayed if an obstacle database is loaded in the system. ar Terrain Feature Terrain data can be displayed on the Navigation Map Page by pressing the TERRAIN softkey. Terrain symbology (mountain icon) appears next to the map range in the bottom right corner of the page indicating the presence of terrain data on the map. TERRAIN softkey Figure 7.2.2 TERRAIN Softkey Pr el NOTE: The table above is only for the Navigation Map Page. The Terrain Proximity Page always shows ONLY caution and warning obstacles. NOTE: Terrain data can also be displayed by using the ‘On/Off’ Navigation Map Page option. See the Navigation Map Page setup section for details. 190-00498-00 Draft 190-00498-00_0A.indd 33 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-33 3/1/2005 10:33:50 AM TAWS/TERRAIN TAWS In order to operate properly, the Garmin TAWS/Terrain system requires a valid 3D GPS position solution and a valid terrain/airport terrain/obstacle database. Garmin’s Terrain Awareness Warning System (TAWS) satisfies TSO-C151b Class B requirements for certification. Class B TAWS is required for all Part 91 aircraft operations with 6 or more seats and for Part 135 turbine aircraft operations with 6 to 9 passenger seats (FAR Parts 91.223, 135.154). Garmin TAWS greatly increases situational awareness and aids in reducing accidental Controlled Flight Into Terrain (CFIT). CAUTION: It is always the ultimate responsibility of the crew to navigate safely throughout the course of flight. Garmin TAWS is designed to be an aid to situational awareness, not to be relied on as a primary source of terrain and obstacle avoidance. Pr el im in ar Figure 7.2.3 shows the Navigation Map Page with terrain features. Figure 7.2.3 Obstacles on Navigation Map Page 7-34 190-00498-00_0A.indd 34 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:51 AM TAWS/TERRAIN System Compairison Garmin TAWS and TERRAIN share several common operational characteristics. Table 7.2.1 compares the features and abilities of the two systems: Function Pr el im in ar TSO-C151b Class B Certified TAWS/TERRAIN Display ( Shows terrain elevations relative to the aircraft ) Visual Alerting ( Includes popup alerting ) Aural Alerting External Visual Alerting Capability Reduced Terrain Clearance (RTC) Avoidance ( Forward Looking Terrain Avoidance (FLTA) sub-function ) Imminent Terrain Impact (ITI) Avoidance ( Forward Looking Terrain Avoidance (FLTA) sub-function ) Premature Descent Alert (PDA) Excessive Rates of Descent ( Ground Proximity Warning System (GPWS) Alerting sub-function ) Negative Climb Rate/Altitude Loss After Takeoff ( Ground Proximity Warning System (GPWS) Alerting sub-function ) “Five Hundred” Voice Callout ( Ground Proximity Warning System (GPWS) Alerting sub-function ) Inhibit Capability ( Inhibits FLTA and PDA visual and aural alerting ) Manual System Test Capability Worldwide Terrain Database Airport Layer Database Obstacle Database TAWS Yes Terrain No Yes Yes Yes Yes Yes Yes No No Yes Yes Yes Yes Yes Yes Yes No Yes No Yes No Yes Yes Yes Yes Yes Yes No Yes Yes Yes Table 7.2.1 TAWS/TERRAIN Feature Comparison 190-00498-00 Draft 190-00498-00_0A.indd 35 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-35 3/1/2005 10:33:51 AM TAWS/TERRAIN Basic Operation TAWS/TERRAIN/PROXIMITY Page Terrain information, aircraft ground track and GPS-derived MSL altitude are displayed on the screen. Altitude is shown in increments of 20 feet or in increments of 10 meters, depending on unit configuration. The ‘G’ to right of the MSL altitude display is a reminder that altitude is GPS-derived. Power Up During power-up of the G1000 unit, terrain/airport terrain/obstacle database versions and area of coverage are displayed along with a disclaimer. At the same time, the TAWS/TERRAIN system self-test begins. An aural message plays upon test completion: Database Updates • 360˚ View — Bird’s eye view from above aircraft depicts surrounding terrain on all sides. • 120˚ View — Bird’s eye view of terrain ahead of and 60˚ to either side of the aircraft flight path. Display Page Operation Pr el im in Terrain/airport terrain/obstacle databases are updated periodically with the latest terrain/airport terrain/obstacle data. Visit the Garmin website to check for newer versions of terrain/airport terrain/obstacle databases. Updated terrain data cards may be obtained from the Garmin website or by calling Garmin at one of the numbers listed in the front of this document. There are two main display settings from which the crew can choose: ar • “TAWS System Test, OK”, if the system passes the test. • “TAWS System Failure”, if the system fails the test. A failure of the test is annunciated for both TAWS and TERRAIN, if the self-test fails. TAWS and TERRAIN appears in the Navigation Map. To display terrain data on the Navigation Map Page: 1. Press the MAP softkey. 2. Press the TERRAIN softkey. Press the TERRAIN softkey again to remove terrain data from the Navigation Map Page. 7-36 190-00498-00_0A.indd 36 NOTE: The TAWS/TERRAIN/PROXIMITY Page gives a Heading Up display orientation, as indicated by the ‘HDG’ label shown on the display. To change the TAWS/TERRAIN display viewing angle between 360° and 120˚: 1. Select the TAWS/Terrain Proximity Page 2. Press the VIEW softkey. Then press the ARC softkey. 3. To return to the 360 degree viewing display press the 360 softkey, OR: 4. Press the MENU key. The page menu is displayed with ‘View Arc’ or ‘View 360º’ highlighted. Press the ENT key on the desired selection. Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:51 AM TAWS/TERRAIN Terrain/Obstacle Database Areas of Coverage TAWS/TERRAIN Failure Alert The following areas of coverage are available in each database. Regional definitions may change without notice. The TAWS/TERRAIN system continually monitors several system-critical items, such as database validity, hardware status and GPS status. Should the system detect a failure, one of the following messages is issued: TAWS/TERRAIN database versions may be viewed by going to AUX System Status Page. Pop-up terrain alerts are displayed only when the TERRAIN Page is not being viewed. Pop-up terrain alerts do not appear on the TERRAIN Page. ar Terrain Not Available im in Terrain Inhibited el Worldwide (WW): Latitudes: S60 to N75 Longitudes: W180 to E180 Americas (AME): Latitudes: S60 to N75 Longitudes: W180 to W30 Atlantic (ATL): Latitudes: S60 to N75 Longitudes: W30 to E90 No Alert or Status Pr Pacific (PAC): Latitudes: S60 to N75 Longitudes: E60 to E180 United States (US): Limited to the United States plus some areas of Canada, Mexico, Caribbean, and the Pacific. Terrain Test Terrain Failure Figure 7.2.4 TAWS Failure Messages The TAWS/TERRAIN Page displays “TERRAIN FAILED”. For TAWS units, the aural message “TAWS System Failure” is issued along with the “TER FAIL” annunciation. TAWS/TERRAIN Not Available Alert Garmin TAWS/TERRAIN requires a 3D GPS navigation solution along with specific vertical accuracy minimums. Should the navigation solution become degraded, if the terrain/airport terrain/obstacle databases are not available, or if the aircraft is out of the database coverage area, the annunciation ‘TER N/A’ is given in the annunciation window. The aural message “Terrain Not Available” is issued along with the ‘TER N/A’ annunciation. 190-00498-00 Draft 190-00498-00_0A.indd 37 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-37 3/1/2005 10:33:51 AM TAWS/TERRAIN Forward Looking Terrain Avoidance RTC/ITI Severity Levels The Forward Looking Terrain Avoidance alert (FLTA) is used by TAWS and is composed of two sub-functions: Reduced Required Terrain Clearance (RTC) Avoidance — Provides alerts when the aircraft flight path is above terrain, yet is projected to come within minimum clearance values shown in Table 7.2.2. When an RTC alert is issued, a potential impact point is displayed on the TAWS/ TERRAIN Proximity Page. Phase Of Flight Enroute Terminal Approach Departure Pr el im During the final approach phase of flight, RTC/ITI alerts are automatically inhibited when the aircraft is below 200’ AGL while within 0.5 nm of the approach runway or is below 125’ AGL while within 1 nm of the runway. CAUTION: Estimated potential impact in approximately 60 seconds after pop-up alert and annunciation. For TAWS, RTC/ITI caution alerts are accompanied by the aural message “Caution Terrain; Caution Terrain” OR “Terrain Ahead; Terrain Ahead”. ar in Imminent Terrain Impact (ITI) Avoidance — Provides alerts when the aircraft is below the elevation of a terrain cell in the aircraft’s projected path. ITI alerts are accompanied by a potential impact point displayed on the TAWS/ TERRAIN Proximity Page. The alert is given when the projected vertical flight path is calculated to come within minimum clearance altitudes in Table 7.2.2. Level Flight 700 ft. 350 ft. 150 ft. 100 ft. Descending 500 ft. 300 ft. 100 ft. 100 ft. Table 7.2.2 Minimum Terrain Clearance Values for RTC/ITI Alerts WARNING: Estimated potential impact in approximately 30 seconds after pop-up alert and annunciation. For TAWS, RTC/ITI warning alerts are accompanied by the aural message “Terrain, Terrain; Pull Up, Pull Up” OR “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”. 7-38 190-00498-00_0A.indd 38 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:52 AM TAWS/TERRAIN alerting ends at 0.5 nm from the runway threshold OR at an altitude of 125’ AGL while within 1 nm of the threshold. ar in CAUTION: The above annunciation and pop-up terrain alert are displayed during a PDA alert. For TAWS, the PDA alert is accompanied by the aural message “Too Low, Terrain”. • ILS Approach Loaded — PDA alerting begins when FAF is the active waypoint AND the aircraft is within 15 nm of the destination airport. Once the aircraft intercepts the glideslope, PDA will alert the crew if the aircraft descends 0.7 degrees below the glideslope. PDA alerting ends 0.5 nm from the runway threshold OR at an altitude of 125’ AGL while within 1 nm of the threshold. Premature Descent Alerting (PDA) Pr el im Garmin TAWS/TERRAIN issues a Premature Descent alert when the system detects that the aircraft is significantly below the normal approach path to a runway. The PDA alert mode is functional only during descent to land. There are three different scenarios to consider with PDA: • No Approach Loaded — PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0.5 nm from the runway threshold OR is at an altitude of 125’ AGL while within 1 nm of the threshold. During the final descent, algorithms will set a threshold for alerting based on speed, distance and other parameters. • Non-Precision Approach Loaded — PDA alerting begins when FAF is the active waypoint AND the aircraft is within 15 nm of the destination airport. Again, algorithms are used to set a threshold for alerting based upon various parameters. PDA 190-00498-00 Draft 190-00498-00_0A.indd 39 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-39 3/1/2005 10:33:52 AM TAWS/TERRAIN Glideslope Intercept Final Approach Fix 200' below FAF Altitude Runway Threshold CAUTION PDA Alert is 0.7 Below Glideslope 0.5 nm 15 nm im in The threshold for the Non-Precision Approach PDA descent is computed by algorithms based on varying flight conditions. ar Figure 7.2.5: Example of PDA alert threshold for ILS approach 200' below FAF Altitude Pr el Final Approach Fix Runway Threshold CAUTION 0.5 nm 15 n m Figure 7.2.6: Example of Non-Precision Approach PDA alert threshold. 7-40 190-00498-00_0A.indd 40 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:54 AM TAWS/TERRAIN TAWS Alerts Excessive Descent Rate Severity Levels The following features are required to meet Class B requirements for a TAWS system per TSO-C151b. TAWS provides aural voice alerts along with regular display annunciation. With each alert type shown is an accompanying aural alert as well. CAUTION: The annunciation and pop-up terrain alert are accompanied by the aural message “Sink Rate”. Excessive Descent Rate Alert (EDR) ar "S IN 4000 3500 WARNING: The annunciation and pop-up terrain alert are accompanied by the aural message “Pull Up”. el 3000 im RA TE 4500 in 5000 2500 Pr Height Above Terrain (Feet) The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 7.2.7 shows the parameters for the alert as defined by TSO-C151b. 2000 1500 "PULL U "PULL UP" P" 1000 500 2000 4000 6000 8000 10000 12000 Descent Rate (FPM) Figure 7.2.7: Excessive Descent Rate Graph 190-00498-00 Draft 190-00498-00_0A.indd 41 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-41 3/1/2005 10:33:55 AM TAWS/TERRAIN Negative Climb Rate After Takeoff Alert (NCR) Alert Priority and Aural Alert Message Summary The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the crew 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. TSO-C151b requires the establishment of an internal priority scheme for alerts. In this way, the more important alerts will override lesser alerts. Table 7.2.3 shows the alert priority level in the Garmin TAWS system and gives a summary of the aural messages. The aural alert is configurable for either male or female voice. Different alert text phrases are available for several alerts. Contact a Garmin authorized service center for further information on configuring the alert system. TAWS System Test el “Five-Hundred” Aural Alert im in ar Garmin TAWS provides a manual test for the flight crew. With this feature, the crew can verify proper operation of the aural and visual system annunciation. Pr The purpose of the aural alert message “Five-hundred” is to provide an advisory alert to the crew that the aircraft is five-hundred feet above terrain. When the aircraft descends within 500 feet of terrain, the aural message “Fivehundred” is heard. There are no display annunciations or pop-up alerts that accompany the aural message. To manually test the TAWS system: 1. At the TAWS Page, press MENU. 2. Select the “Test Terrain?” option. 3. Press ENT to confirm the selection. An aural message is played giving the test results: • “TAWS System Test, OK”, if the system passes the test. • “TAWS System Failure”, should the system fail the test. NOTE: TAWS System Testing is disabled during flight. 7-42 190-00498-00_0A.indd 42 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:55 AM TAWS/TERRAIN Terrain Awareness Caution: RTC, ITI Alerts Obstacle Awareness Caution: ROC, IOI PDA Caution Alert Altitude Callout “500” Excessive Descent Rate Alert Caution Negative Climb after Takeoff Alert ar Obstacle Awareness Warning: ROC, IOI “Terrain, Terrain; Pull-Up, Pull-Up” Or “Terrain Ahead, Pull-Up; Terrain Ahead, Pull-Up” “Obstacle, Obstacle; Pull-Up, Pull-Up” Or “Obstacle Ahead, Pull-Up; Obstacle Ahead, Pull-Up” “Caution, Terrain; Caution, Terrain” Or “Terrain Ahead; Terrain Ahead” “Caution, Obstacle; Caution, Obstacle” Or “Obstacle Ahead; Obstacle Ahead” “Too Low, Terrain” “Five-hundred” “Sink Rate” “Don’t Sink” or “Too Low, Terrain” in Aural Message “Pull Up” im Alert Type Excessive Descent Rate Alert Warning Terrain Awareness Warning: RTC ITI Alerts el Priority Pr Table 7.2.3: TAWS Alert Summary 190-00498-00 Draft 190-00498-00_0A.indd 43 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-43 3/1/2005 10:33:55 AM in ar TAWS/TERRAIN Pr el im This page intentionally left blank. 7-44 190-00498-00_0A.indd 44 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:55 AM TRAFFIC 7.3 TRAFFIC TRAFFIC MAP PAGES The Traffic Map Page displays the following information: TIS (TRAFFIC INFORMATION SYSTEM) • Current aircraft location, surrounding TIS traffic, and range marking rings. TIS is a system used for detecting and tracking aircraft in the vicinity of your own aircraft. When ATC radar interrogates aircraft transponders, the replies are analyzed to determine range, bearing and the relative altitude of the intruder. The traffic is then displayed to the flight crew on the MFD. • The current traffic mode (OPERATE, STANDBY). • A traffic alert message (FAILED, DATA FAILED, NO DATA, UNAVAILABLE). • Traffic display banner (AGE 00:, TRFC COAST, TA OFF SCALE, TRFC RMVD, TRFC FAIL, NO TRFC DATA, TRFC UNAVAIL, TRAFFIC). ar CAUTION: TIS is unable to detect any intruding aircraft without an operating transponder. To select the Traffic Map Page: im TRANSPONDER STATUS BAR 1. in NOTE: Traffic Information Service (TIS) is not available in all areas. Pr el TIS surveillance data is up-linked by Air Traffic Control (ATC) radar through the GTX 33 Mode S Transponder. The Transponder Status Bar displays the transponder code, reply symbol and mode of operation on the Inset Map (PFD) and the Navigation and Traffic Map Pages on the MFD (refer to the MFD Pilot’s Guide). In order to receive and display TIS traffic information, the GTX 33 must not be in GND mode or STBY mode. Select the MAP group of pages. Turn the small FMS knob to select the Traffic Map Page. To display traffic on the Navigation Map Page: 1. Press the MAP softkey. 2. Press the TRAFFIC softkey. Press the TRAFFIC softkey again to remove traffic. NOTE: Traffic and terrain data can also be displayed by using the ‘On/Off’ Navigation Map Page option. See the Navigation Map Page setup section for details. Figure 7.3.3 shows the Traffic Map Page on the MFD. Figure 7.3.1 Transponder Status Bar When traffic is displayed within the TIS volume, the word TRAFFIC appears on the PFD. Figure 7.3.2 shows the Traffic Annunciation on the PFD. 190-00498-00 Draft 190-00498-00_0A.indd 45 Traffic symbols are similarly displayed on the Navigation map page. The traffic symbols are shown relative to other displayed features. Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-45 3/1/2005 10:33:55 AM TRAFFIC in ar Traffic Annunciation Traffic Map Range Pr Traffic Mode el im Figure 7.3.2 Traffic Annunciation on PFD Own Aircraft Figure 7.3.3 Traffic Map Page 7-46 190-00498-00_0A.indd 46 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:56 AM TRAFFIC TIS Symbology Category TIS traffic is displayed on the Traffic Map Page similarly to TCAS symbology. The main difference between TIS and TCAS is the source of surveillance data. TCAS uses an airborne interrogator with a half-second update rate. TIS uses the terminal Mode S ground interrogator and its Data Link to provide approximately a five-second update rate. The range accuracy of TIS and TCAS is similar. Appendix E describes the Traffic Information Service in detail. Other Traffic Proximate Traffic Traffic Advisory, Out of Range Traffic Advisory Traffic Map Page Operations Power-Up Test ar The TIS interface performs an automatic test during power-up. If the system passes the power-up test, the standby screen is displayed on the Traffic Map Page. If the system passes the power-up test while the aircraft is airborne, traffic is immediately displayed on the Traffic Page in the operating mode. in The Traffic Advisory (TA) solid yellow circle indicates that traffic meets the TA advisory criteria. The presence of TA traffic beyond the selected display range is indicated by one half of a yellow circle at the edge of the display. The position of the half-symbol represents the bearing of the traffic. Symbol Pr el im Altitude separation from your aircraft is displayed above the target symbol if the traffic is above your altitude or below the symbol if they are below. Altitude trend is displayed as an up arrow (+500 ft/min), down arrow (-500 ft/min) or no symbol if less than 500 ft/min rate in either direction. Traffic Ground Track is indicated on the Traffic Map Page by a “Track Vector”. The track vector line is projected from the TA symbol at the angle of the TA relative track. Proximate traffic is shown as a white diamond with a solid box inside. Other traffic is displayed as a hollow white diamond. Proximate traffic and other traffic symbols indicate that traffic is not yet considered a threat, so no Traffic Advisory is generated. 190-00498-00 Draft 190-00498-00_0A.indd 47 If the system fails the power up test, the ‘NO DATA’, ‘DATA FAILED’ or ‘FAILED’ message is displayed. • The ‘FAILED’ message indicates the GTX 33 transponder has failed. • The ‘DATA FAILED’ message indicates data is being received from the GTX 33 but a failure was detected in the data stream. • The ‘NO DATA’ message indicates that data is not being received from the GTX 33. Contact a Garmin authorized service center for repair. Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-47 3/1/2005 10:33:57 AM TRAFFIC Changing the Map Range • OPERATE – when the Traffic Map Page displays ‘OPERATE’ in the status box on the Traffic Map Page, the TIS system is operational and displays traffic on the Traffic and Map Pages. To change the map range: 1. Turn the joystick clockwise to zoom out or turn the joystick counter-clockwise to zoom in. Map ranges are 2 nm, 6 nm and 12 nm. The crew can switch between the standby (STBY) and operate (ON) modes to manually override automatic operation using the page menu or softkeys. NOTE: If the intruder aircraft is non-altitude reporting only the range and bearing will be displayed. To switch between operating modes: 2. Press the STBY or ON softkey to switch between modes. ‘STANDBY’ or ‘OPERATE’ is displayed in the status box located in the upper left corner of the Traffic Map Page, OR: el im The TIS Traffic Advisory (TA) should alert the crew to look for intruding aircraft any time a yellow circle traffic symbol appears and voice warning is announced. Conduct a visual search for the intruder. Maintain visual contact to ensure safe separation. Press the MENU key. The page menu is displayed with ‘Standby Mode’ or ‘Operate Mode’ highlighted. Press the ENT key on the desired selection. ar 3. in Once the aircraft is airborne the system switches from ground or standby mode to operating mode. The G1000 displays ‘OPERATE’ in the upper left hand corner of the display and begins to display traffic on the Traffic or Map Page. Press the MODE softkey. Operating Mode 1. Pr When the aircraft is on the ground the system switches from operating mode to ground or standby mode. The Traffic Map Page displays ‘GND’ or ‘STANDBY’. • STANDBY – when the Traffic Map Page displays ‘STANDBY’ in the status box on the Traffic Map Page, the TIS system is in standby mode and cannot display traffic data. • GND – when the Traffic Map Page displays ‘GND’ in the status box on the Traffic Map Page, the TIS system does not display traffic data. The GTX 33 does not reply to Mode A or Mode C interrogations but does send Mode S acquisition replies. The ground mode is entered automatically. It is not a crew selectable mode. 7-48 190-00498-00_0A.indd 48 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 190-00498-00 Draft 3/1/2005 10:33:57 AM TRAFFIC TIS Audio Alert • TRAFFIC - on the PFD, when the system receives a traffic advisory a flashing ‘TRAFFIC’ alert is displayed in the upper left hand portion of the display. The PFD inset map also automatically displays traffic data. in • “Traffic” - TIS traffic alert is received. • TA OFF - the ‘TA OFF’ scale banner displayed in the lower left corner of the display indicates that a traffic advisory is outside the selected display range. The traffic advisory off-range banner is removed when the traffic advisory is within the selected display range. ar A TIS audio alert is generated whenever the number of TAs on the Traffic Map Page display increases. Limiting audio to TAs only reduces the amount of nuisance alerting due to proximate aircraft. For example, when the first TA is displayed, the crew is alerted audibly. As long as a single TA aircraft remains on the TIS display, no further audio alert is generated. If a second TA aircraft appears on the display, a new audio alert is sounded. If the number of TAs on the TIS display decreases and then increases, a new audio alert is sounded. The TIS audio alert is also generated whenever TIS service becomes unavailable. The volume of the audio alerts and the choice between a male or female voice is configured during installation. The following TIS audio alerts are available: • TRFC RMVD - the ‘TRFC RMVD’ banner indicates that traffic has been removed from the display due to the age of the data. Data is too old to “coast” when the time period is 12-60 seconds from the last receipt of a TIS message. The crew should be aware that traffic may be present but not shown. TIS Traffic Status im • “Traffic Not Available” - TIS service is not available or out of range. Traffic Banner Pr el The MFD indicates the following TIS traffic status to the flight crew. • AGE - if traffic data is not refreshed within 6 seconds, an age indicator (i.e., ‘AGE 00:06’) is displayed in the lower left corner of the display, when displaying traffic. After another 6 seconds, if data is still not received, the traffic is removed from the display. The quality of displayed traffic is reduced as the traffic data becomes stale. CAUTION: TIS warns the crew with voice and visual traffic advisories whenever it predicts an intruder to be a threat. The display and advisories are intended only for assistance in visually locating the traffic and lack the resolution and coordination ability necessary for evasive maneuvering. Always attempt to visually clear the airspace before maneuvering your aircraft in response to a TA. See Appendix E for detailed TIS information. • TRFC COAST - the ‘TRFC COAST’ (traffic coasting) banner located above the AGE timer indicates that displayed traffic is held even though the data is stale. The quality of displayed traffic is reduced. 190-00498-00 Draft 190-00498-00_0A.indd 49 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 7-49 3/1/2005 10:33:57 AM y ar in im el Pr 190-00498-00 Draft 190-00498-00_0A.indd 3 Garmin G1000 Hazard Avoidance Pilot’s Guide for the Cessna Citation Mustang 3/1/2005 10:33:57 AM Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p: 913.397.8200 f: 913.397.8282 Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p: 503.391.3411 f: 503.364.2138 Garmin (Europe) Ltd. Unit 5, The Quadrangle Abbey Park Industrial Estate Romsey, SO51 9DL, U.K. p: 44/0870.8501241 f: 44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p: 886/2.2642.9199 f: 886/2.2642.9099 www.garmin.com © 2005 Garmin Ltd. or its subsidiaries 190-00498-00_0A.indd 4 190-00498-00 Rev. A 3/1/2005 10:34:04 AM
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