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Except as expressly provided herein, no part of this addendum 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 permis- sion to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium...
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Warnings and Cautions WARNING: Terrain data are obtained from third party sources. Garmin is not able to independently verify the accuracy of this data which should be used only as an aid for situational awareness. Terrain data must not be used as the sole basis for deci- sions or maneuvers to avoid terrain or obstacles.
Introduction Table of Contents Table of Contents Part One: Traffic Information Service (TIS) Interface 1 Section 1: TIS Operation and Symbology ...1 TIS Operation ...1 How TIS differs from TCAS ...2 TIS Limitations ...2 Improving TIS ...3 TIS Symbology ...3 Section 2: Control and Display ...5 TIS Traffic Display Status and Pilot Response ...5 Traffic Page ...6...
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Terrain Proximity 120° Arc or 360° Rings ...60 Terrain Proximity Aviation Data ...60 Terrain Proximity Legend ...61 Terrain Proximity Limitations...62 System Status ...62 Part Six: Garmin GTS 8XX Series Interface ...63 Introduction ...63 GTS 8XX Series Description ...63 Power-up Self-Test ...63 User-initiated Test ...64 Voice Announcements ...64...
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TIS Traffic display is available to aircraft equipped with a Mode S Data Link such as the Garmin GTX 330 Transponder. TIS Traffic from a GTX 330 Transpon- der can then be displayed on a Garmin 400W/500W Series unit.
The range accuracy of TIS and TCAS is similar. TIS Limitations NOTE: This section on TIS Limitations is not compre- hensive. Garmin recommends the user review the TIS Limitations section of the Aeronautical Information Manual, Section 1-3-5. TIS is NOT intended to be used as a collision avoidance system and does not relieve the pilot of responsibility to “see and avoid”...
and avoid.” Some of the more common examples of these errors follow: • When client or intruder aircraft maneuvers excessively or abruptly, the tracking algorithm may report incorrect horizontal position until the maneuvering aircraft stabilizes. • When a rapidly closing intruder is on a course that crosses the client aircraft course at a shal- low angle (either overtaking or head on) and either aircraft abruptly changes course within...
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Part One: Section 1 TIS Operation and Symbology The TIS audio alert is generated from the GTX 330 whenever the number of Traffic Ad- visories on the 400W/500W display increases from one scan to the next. Limiting Traffic Advisories only reduces the “nuisance” alerting due to proximate aircraft.
Section 2: Control and Display TIS Traffic Display Status and Pilot Response • STBY — When the 400W/500W displays STBY in the upper right hand corner of the display the TIS system is in standby mode and cannot display traffic data. •...
Part One: Section 2 TIS Controls and Display Traffic Ground Track Traffic ground track is indicated in the 400W/500W display by a “target track vector”, a short line displayed in 45° increments, extending in the direction of target movement. Traffic Target Track Vector. Traffic Warning Window When the unit is on any page (other than the NAV Traffic Page or when a TAWS/Terrain, or Dead...
Map Page TIS traffic is displayed on the Map Page in addition to the Traffic Page. The Map Page displaying traffic. Configuring TIS Traffic Data on the Map Page To configure TIS traffic on the Map Page: Turn the small right knob to select the Map Page.
Part One: Section 2 TIS Controls and Display Highlighting TIS Traffic Using Map Page Panning Another Map Page feature is panning, which allows you to move the map beyond its current limits without adjusting the map scale. When you select the panning function —...
Section 3: TIS Operational Procedures Introduction TIS warns the user with voice and visual traffic advisories whenever it predicts an intruder to be a threat (see illustration). Voice and visual data are sent from the GTX 330. The user should not start evasive maneuvers using information from the 400W/500W display or on a traffic advisory only.
Part One: Section 3 TIS Operational Procedures Manual Override The user can manually switch between standby (STBY) and operating (OPER) mode of operation to manually override automatic operation. To place the display into operating mode from the standby mode (to display TIS traffic): Turn the cursor on and highlight “STBY”.
IDs. Weather and/or audio data from your GDL 69/69A are provided by XM Satellite Radio, a company separate and independent from Garmin Corporation. Have your radio hardware IDs ready before contact- ing XM Satellite Radio. During the process, you can select services for subscription.
Part Two: Section 2 XM Weather XM WPT Pages When a GDL 69 or GDL 69A is installed, two XM- related pages are added to “airport” pages in the WPT page group: • Textual METAR Page. The Textual METAR page shows the text of the most recent METAR (Meteorological Aerodrome Report) that has been received for an airport.
• Winds Aloft (WINDS). The Winds Aloft selection provides the pilot with wind speed and direction. The winds at a given altitude are selected in the Winds Aloft Alt below the WINDS selection. The selected altitude is shown along with the product time. •...
Part Two: Section 2 XM Weather almost complete coverage of the continental United States, Alaska, and Hawaii. The unobstructed range of each NEXRAD is up to 250 nautical miles. When enabled, composite data from all the NEXRAD radar sites in the United States is shown. This data are composed of the maximum reflectivity from the individual radar sweeps.
NEXRAD Intensity Colors are used to identify the different NEXRAD echo intensities (reflectivity) measured in dBZ (deci- bels 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).
Part Two: Section 2 XM Weather XM Weather Label and NEXRAD Source U.S. XM Weather Label and NEXRAD Source Canada NOTE: The only weather product available for Canada is Canadian NEXRAD. NEXRAD Limitations Certain limitations exist regarding the NEXRAD radar displays. Some, but not all, are listed for the user’...
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To display METARs on the XM Weather page: While viewing the XM Weather page, check the upper left corner to see whether “METAR” or another weather product is displayed in the upper left corner. If another weather product (rather than “METAR”) is shown, press the small right (CRSR) knob to highlight the product name, such as “NEXRAD”.
Part Two: Section 2 XM Weather Textual METAR Page When the GDL 69/69A is installed, a Textual METAR page is added among the APT (airport) pages of the WPT page group. This page can be accessed from the XM Weather page as well as from the WPT page group.
Textual METAR/TAF Code The current airport weather reports on the Textual METAR page (and the airport weather forecasts on the TAF page, too) use a rather cryptic format originally devised for teleprinters. You can find information about this format in an FAA publication, Aviation Weather Formats: METAR/TAF, which can be down- loaded from the FAA Web site.
Part Two: Section 2 XM Weather Press ENT. The first item is the pop-up Page Menu will be “Review TFR?”. Press ENT again to see the TFR Information page. Press ENT when done viewing the TFR Informa- tion page. The fields of the TFR Information page are as fol- lows: •...
Cell Movement (CELL MOVE) When enabled, Cell Movement shows the storm cells identified by the ground-based system. The movement is depicted by an arrow. The tip of the arrow represents where the cell is expected to be in 10 minutes from the time the cell location was deter- mined.
Part Two: Section 3 XM Weather Winds Aloft The Winds Aloft selection provides the pilot with a graphic display of predicted winds at any one of 15 selectable altitudes. The winds at a given altitude are selected in the Winds Aloft Alt selection. The selected altitude is shown along with the product effective time.
Winds Aloft Altitude The Winds Aloft Altitude selection provides the pilot with the ability to select any wind altitude from the ground up to 42,000 feet in 3,000 foot increments. When no data are shown at a given altitude, the data for that altitude has not been received.
Part Two: Section 4 XM Audio audio ID, because the GDL 69 is a data-only receiver.) • Audio Signal. The Audio Signal field indicates the signal strength of the GDL 69A’ s audio signal. (In the case of a GDL 69, this field shows “antenna”...
Each of these time stamps is a date-time group in “DDHHMMZ” format, where: • DD is the day of the month • HH is the hour of the day • MM is the minute of the hour • Z is a time zone designator indicating that the date and time are for standard time on the Greenwich meridian: that is, UTC (Coordi- nated Universal Time).
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Part Two: Section 4 XM Audio The XM Audio page allows you to control the functions of the XM Audio receiver in the GDL 69A, such as, category and channel selection, artist selection, and volume. Pressing the MENU key displays the Page Menu selections. Selecting categories Press the small right (CRSR) knob to high- light the category names.
XM Audio Menu The XM Audio Menu provides choices for selecting a channel, displaying the channel, artist, or title, enabling audio output, and controlling the volume. While viewing the XM Audio page, press the MENU key. Turn the large or small right knobs to high- light the choices.
Part Two: Section 4 XM Audio Enter Channel Number You may directly select a specific channel by using the “Enter Channel Number” item from the Page Menu. While viewing the XM Audio page, press the MENU key. Turn the large right knob to highlight “Enter Channel Number.”...
Display Artist In List The name of the artists in the range of displayed channels can be shown in the middle pane by using the “Display Artist In List” item from the Page Menu. While viewing the XM Audio page, press the MENU key.
Part Two: Section 4 XM Audio Enable/Mute Audio Output The Enable/Mute Audio Output selection of the Page Menu allows you to toggle the audio output On or Off. When Audio Output is muted, a green slash will cross over the music symbol in the song pane. While viewing the XM Audio page, press the MENU key.
TAWS uses terrain and obstacle information sup- plied by government sources. The data undergoes veri- fication by Garmin to confirm accuracy of the content, per TSO-C151b. However, the displayed information should never be understood as being all-inclusive.
Part Three: Section 2 TAWS Operation Section 2: TAWS Operation TAWS Alerting TAWS uses information provided from the GPS receiver to provide a horizontal position and altitude. GPS altitude is derived from satellite measurements. GPS altitude is converted to a mean sea level (MSL)- based altitude (GPS-MSL altitude) and is used to determine TAWS alerts.
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To display the TAWS Page, select the NAV group and turn the small right knob until the TAWS Page is displayed. Terrain information, aircraft ground track, and GPS-derived MSL altitude are displayed on the page. Altitude is shown in increments of 20 feet or in increments of 10 meters, depending on unit configuration.
TAWS Inhibit switch toggles the TAWS inhibit on and off in the same manner as using the Page Menu selection. TAWS Manual Test Garmin TAWS provides a manual test capability which verifies the proper operation of the aural and visual annunciations of the system prior to a flight.
TAWS Symbols The symbols and colors in the following figure and table are used to represent obstacles and potential impact points on the TAWS Page. TAWS uses yellow and red to depict terrain information relative to aircraft altitude. Each color is associated with an alert severity level. Ter- rain graphics and visual annunciations also use these color assignments.
General Database Information Garmin TAWS uses terrain and obstacle informa- tion supplied by government sources. The data under- goes verification by Garmin to confirm accuracy of the content, per TSO-C151b. However, the displayed information should never be understood as being all-inclusive.
Database Updates Terrain/obstacle databases are updated periodi- cally with the latest terrain and obstacle data. Visit the Garmin website to check for newer versions of terrain/ obstacle databases. Compare database cycle numbers to determine if a newer version is available.
Part Three: Section 2 TAWS Alerts Section 3: TAWS Alerts Alerts are issued when flight conditions meet parameters that are set within TAWS software algorithms. TAWS alerts typically employ either a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed.
Part Three: Section 3 TAWS Alerts Excessive Descent Rate Alert (EDR) The purpose of the Excessive Descent Rate alert is to provide suitable notification when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. The parameters for the alert as defined by TSO-C151b are shown in the Descent Rate graph.
TAWS Not Available Alert Garmin TAWS requires a 3-D GPS navigation solu- tion along with specific vertical accuracy minimums. Should the navigation solution become degraded, or if the aircraft is out of the database coverage area, the an- nunciation “TER N/A”...
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TAWS Pop-Up Alert Annunciation None None None None None NOTE: TAWS Caution Alerts are displayed as constant black text on a yellow background; TAWS Warning Alerts are displayed as constant white text on a red background. TAWS Alerts Summary Aural Message “TAWS System Failure”...
Part Three: Section 3 TAWS Alerts Pilot Actions If a TAWS warning and associated aural are received, the pilot should immediately respond to the aural and pull up with maximum power and climb rate unless the terrain or obstacle is clearly identified visually and determined to not be a safety of flight factor.
HTAWS uses terrain and obstacle information sup- plied by government sources. The data undergoes veri- fication by Garmin to confirm accuracy of the content. However, the displayed information should never be understood as being all-inclusive.
Part Four: Section 2 HTAWS Operation Section 2: HTAWS Operation HTAWS Alerting HTAWS uses information provided from the GPS receiver to provide a horizontal position and altitude. GPS altitude is derived from satellite measurements. GPS altitude is converted to a mean sea level (MSL)- based altitude (GPS-MSL altitude) and is used to determine HTAWS alerts.
To display the HTAWS Page, select the NAV group and turn the small right knob until the HTAWS Page is displayed. Terrain information, aircraft ground track, and GPS-derived MSL altitude are displayed on the page. Altitude is shown in increments of 20 feet or in increments of 10 meters, depending on unit configuration.
Part Four: Section 2 HTAWS Operation Inhibit Mode HTAWS provides an “inhibit mode”. This mode is designed to deactivate aural and visual alerts when they are deemed unnecessary by the aircrew. Pilots should use discretion when inhibiting the HTAWS system and always remember to enable the system when appropri- ate.
Reducing HTAWS Protection To reduce protection: Select the HTAWS Page and press MENU. Turn the large or small right knob to highlight “Reduce Protection?”. Press ENT. Protection is reduced. The “RP Mode” annunciation is displayed in the ter- rain annunciator field whenever protection is reduced.
Part Four: Section 2 HTAWS Operation HTAWS Manual Test Garmin HTAWS provides a manual test capability which verifies the proper operation of the aural and visual annunciations of the system prior to a flight. “Test HTAWS” selection To manually test the HTAWS system: Select the HTAWS Page and press MENU.
HTAWS Symbols The symbols and colors in the following figures and table are used to represent obstacles and potential impact points on the HTAWS Page. Each color is associated with a height above terrain. The zoom range of obstacles (on the TAWS and NAV pages) is controlled by the NAV map’ s “Setup Map” menu option in the “Terrain”...
WARNING (Red) CAUTION (Yellow) HTAWS Alert Coloring and Symbology General Database Information Garmin HTAWS uses terrain and obstacle infor- mation supplied by government sources. The data undergoes verification by Garmin to confirm accuracy of the content. However, the displayed information should never be understood as being all-inclusive.
Database Updates Terrain/obstacle databases are updated periodi- cally with the latest terrain and obstacle data. Visit the Garmin website to check for newer versions of terrain/ obstacle databases. Compare database cycle numbers to determine if a newer version is available.
Part Four: Section 3 HTAWS Alerts Obstacle Database Areas of Coverage The following describes the area of coverage avail- able in each database. Regional definitions may change without notice. Database Coverage Area Limited to the United States plus United States (US) some areas of Canada, Mexico, Caribbean, and the Pacific.
NOTE: HTAWS Caution Alerts are displayed as constant black text on a yellow background; HTAWS Warning Alerts are displayed as constant white text on a red back- ground. Forward Looking Terrain Avoidance The unit will issue terrain alerts not only when the aircraft altitude is below the terrain elevation but also when the aircraft is projected to come within minimum clearance values of the terrain.
“TAWS FAIL” annunciation. HTAWS FAILED Display HTAWS Alert Summary The aural alert voice gender is configurable to be either male or female. See your Garmin installer for further information on configuring the alert system. 190-00356-30 Rev H...
Pilot Actions If a HTAWS warning and associated aural are received, the pilot should immediately maneuver the rotorcraft in response to the alert unless the terrain or obstacle is clearly identified visually and determined by the pilot not to be a factor to the safety of the operation. A HTAWS caution alert indicates terrain or obstacle nearby.
Part Four: Section 3 HTAWS Alerts Voice Call Out Selection The Voice Call Out (VCO) selection is available where HTAWS is installed. The VCO functionality pro- vides a voice annunciation of the aircraft’ s height above terrain or the nearest airport, heliport, runway, or helipad when that threshold is first crossed.
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Airport/Heliport Terrain “Cutouts” For software version 4.00 and later: when con- figured for helicopters (the helicopter icon will be displayed), black, circular or oblong “cutouts” will be displayed on the Terrain Page around airports and heli- ports, to enhance viewing of the information displayed for those locations.
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Terrain page, depending on the installed hardware and configuration. . Introduction Garmin Terrain Proximity is an optional non-TSO- certified terrain awareness feature of the 400W/500W series available in helicopter configurations to increase situational awareness and help reduce controlled flight into terrain (CFIT).
Part Five Terrain Proximity Terrain Proximity 120° Arc or 360° Rings Select the 120º Arc or 360º rings overlay for the Terrain Proximity page with the Page Menu. Press the MENU key to display the Page Menu. The “View 120°” or “View 360°” option will be highlighted.
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Terrain Proximity Legend Select the display of the Terrain color legend on the Terrain Proximity page from the Page Menu. Press the MENU key to display the Page Menu and turn the small right knob to highlight the Legend selection. Select “Show Legend”...
Obstacle is 250 ft, or more, below current aircraft altitude NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross- validates the data but cannot guarantee the ac- curacy and completeness of the data.
Garmin GTS 8XX Series Interface Introduction The Garmin GTS 8XX Series unit is a Traffic Advisory System (TAS - GTS 800 and GTS 820) or Traffic Alert and Collision Avoidance System (TCAS I - GTS 850). The GTS 8XX Series enhances flight crew situational awareness by displaying traffic information for transponder-equipped aircraft.
Part Six GTS 800 Interface To begin tracking intruder aircraft: Press the cursor knob and highlight STBY. Turn the small right knob to select OPER. Press ENT to confirm operating mode and begin tracking intruder aircraft. Operating Mode is confirmed by the display of “OPER”...
Altitude Display Mode The GTS 8XX has four altitude display modes: Normal (±2,700 feet, Above (-2,700 feet to +9,000 feet), Below (-9,000 feet to +2,700 feet), and Unre- stricted (±9,900 feet). The GTS 8XX continues to track up to 30 intruder aircraft within its maximum surveil- lance range, regardless of the altitude display mode selected.
TAS/TCAS Symbology NOTE: GTS 8XX series unit data is only displayed on the Map Page if suitable aircraft heading data is available. See the Garmin 400W or 500W Series Installation Manu- als available at your authorized Garmin service center for details.
Configuring Traffic Data on the Map Page Traffic is only displayed on the Map Page if aircraft heading data is available. When heading is not avail- able, Traffic Advisories are displayed as non-bearing banners on the Map Page. Selections for configuring traffic data are made from the Map Setup Menu on the Map Page.
Part Six GTS 800 Interface Highlighting Traffic Data Using Map Panning Another map page function is panning, which allows you to move the map beyond its current limits without adjusting the map scale. When you select the panning function—by pressing the small right knob—a target pointer flashes on the map display.