GTN 6XX/7XX
Contents
1. The terrain display is intended to serve as a situational awareness tool only By itself it may not provide either the accuracy or the fidelity on which to base decisions and plan maneuvers to avoid terrain or obstacles NOTE Terrain and TAWS are separate features and mutually exclusive If TAWS B is shown on the bottom right of the dedicated terrain page then TAWS is installed 2 7 TAWS Function Optional Flight crews are authorized to deviate from their current ATC clearance to the extent necessary to comply with TAWS warnings Navigation must not be predicated upon the use of TAWS If an external TAWS annunciator panel is installed in the aircraft this annunciator panel must be fully functional in order to use the TAWS system NOTE Terrain and TAWS are separate features and mutually exclusive If TAWS B is shown on the bottom right of the dedicated terrain page then TAWS is installed 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 10 of 26 FAA APPROVED 2 8 Datalinked Weather Display Optional This limitation applies to datalinked weather products from SiriusXM via a GDL 69 69A FIS B via a GDL 88 and Connext via a GSR 56 Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information provided by data link weather products may not accurately depict current weather conditions Do not use the indicated data link weather product age to determ2. Display of marker beacon annunciators optional Remote audio panel control optional Remote transponder control optional Remote audio entertainment datalink control optional TSO C151b Class B TAWS optional Supplemental calculators and timers Control of GSR 56 Iridium Satellite Phone and SMS Text optional x lt X gt lt gt lt gt lt gt lt gt lt gt lt gt lt gt lt gt lt gt lt Xx Xx gt lt gt lt XxX Xx lt lt gt lt gt lt gt lt OK x gt lt gt lt gt x lt lt Xx lt Xx lt Xx x lt x lt X lt gt x lt gt x lt gt x lt Table 1 GTN Functions The GPS navigation functions and optional VHF communication and navigation radio functions are operated by dedicated hard keys a dual concentric rotary knob or the touchscreen AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 5 of 26 Active Com Channel Standby Com Active Nav Standby Nav Channel Channel Channel Volume Squelch On Audio Panel Xpdr Panel Off and Nav ID On Off Controls Controls HOME Key IDENT 1 17 95 Photo Sensor 1200 SD Card AT 108 08 Home Display Function Keys Direct To Key Large and Locking Small Knobs Screw Annunciations Hints Figure 1 GTN 750 Control and Display Layout Active Com Nav Standby Com Nav Channel Channel Volume Squelch On Function Off and Nav ID On Off Keys Home Dis
3. AFM is applicable to the software versions shown in Table 2 The Main and GPS software versions are displayed on the start up page immediately after power on All software versions displayed in Table 2 can be viewed on the System System Status page Software Version Sor vare Temi or later FAA Approved versions for this STC Main SW Version 4 10 GPS SW Version 5 0 Com SW Version 2 10 Nav SW Version 6 02 Table 2 Software Versions 2 4 SD Card It is required that the SD card be present in the unit at all times AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 9 of 26 2 5 Ground Operations Do not use SafeTaxi or Chartview functions as the basis for ground maneuvering SafeTaxi and Chartview functions do not comply with the requirements of AC 20 159 and are not qualified to be used as an airport moving map display AMMD SafeTaxi and Chartview are to be used by the flight crew to orient themselves on the airport surface to improve flight crew situational awareness during ground operations 2 6 Terrain Proximity Function All Units Terrain and obstacle information appears on the map and terrain display pages as red and yellow tiles or towers and is depicted for advisory use only Aircraft maneuvers and navigation must not be predicated upon the use of the terrain display Terrain and obstacle information is advisory only and is not equivalent to warnings provided by TAWS
4. An absolute motion vector pointed towards your ownship symbol does not necessarily mean the traffic target is getting closer to your aircraft Relative motion vectors are always colored green and depict the motion of the traffic target relative to your ownship symbol The direction the traffic target is pointed may vary greatly from the motion vector and a target may be getting closer to your aircraft independent of the direction the target is pointed A green relative motion vector pointed towards your ownship indicates that the traffic target is converging on your aircraft If more than one target is occupying the same area of the screen the GTN will combine the two or more traffic targets into one traffic group The presence of an asterisk to the left of a target indicates that traffic has been grouped The highest priority traffic target in the group is displayed to the pilot When applied to airborne targets the asterisk will be displayed in white or cyan depending on the traffic depiction color used in the installation The asterisk will be brown for grouped ground targets The asterisk will not turn amber even if an alerted target is included in the group An alerted target may be placed in the same group as non alerted targets In this case the alerted target will be displayed Two alerted targets will not be placed in the same group All alerted targets will be displayed on the screen Traffic targets displayed on the dedicated traffic
5. The GTN can be interfaced to a Garmin transponder for control and display of squawk code mode and additional transponder functions The activation of the Enable ES button on the transponder page does not indicate the aircraft is in full compliance with an ADS B Out solution in accordance with TSO C166b 1090ES Consult your transponder documentation for additional information 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 26 of 26
6. after CDI source change on the GTN Refer to the FAA approved Flight Manual or Flight Manual Supplement for the autopilot Analog only autopilots should use APR mode for coupling to LNAV approaches Autopilots which support digital roll steering commands GPSS may utilize NAV mode and take advantage of the digital tracking during LNAV only approaches O This installation prompts the flight crew and requires the pilot to enable the approach outputs just prior to engaging the autopilot in APR mode To couple an approach Once established on the final approach course with the final approach fix as the active waypoint the GTN will issue a flashing message indication Flashing Message Button eee eeeesecesecsse cess cseeeeeeeeeeeeeeeeens PRESS Enable APR Output Button 0 0 eee ceeeeeeeeeeeeeeeeeeeeereees PRESS If coupled Autopilot will revert to ROL mode at this time AUtOpPIlOt c sis EE ENGAGE APPROACH MODE O This installation supports coupling to the autopilot in approach mode once vertical guidance is available To couple an approach Once established on the final approach course with the final approach fix as the active waypoint the GTN will enable vertical guidance Vertical Guidance cccccccccccececeeeceeeeees CONFIRM AVAILABLE AUP Ot oinarrie a ENGAGE APPROACH MODE O The installation does not support any vertical capture or vertical tracking 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS
7. e All overlaying StormScope data on the main map display The flight crew must use the dedicated StormScope page on the GTN system to display StormScope data StormScope must be operated in accordance with Section 7 8 when no heading is available 3 2 7 DATA SOURCE PRESSURE ALTITUDE SOURCE INOPERATIVE OR CONNECTION TO GTN LOST MESSAGE Without a barometric altitude source to the GTN the following features will not operate e Automatic leg sequencing of legs requiring an altitude source The flight crew must manually sequence altitude legs as prompted by the system 3 2 8 UNRECOVERABLE LOSS OF ALL ELECTRICAL GENERATORS OR ALTERNATORS Remove power from all equipment which is not necessary for flight including GTN 2 if installed AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 15 of 26 Section 4 NORMAL PROCEDURES Refer to the Cockpit Reference Guide defined in Section 2 1 of this document or the Pilot s Guide defined in Section 7 1 for normal operating procedures and a complete list of system messages and associated flight crew actions This includes all GPS operations VHF communication and navigation traffic data linked weather StormScope TAWS and Multi Function Display information The GTN requires a reasonable degree of familiarity to avoid becoming too engrossed at the expense of basic instrument flying in IMC and basic see and avoid in VMC Garmin provides training tools with the
8. page may be selected in order to obtain additional information about a traffic target or to view all targets in a grouped target When a grouped target is selected the Next button on the dedicated traffic page will cycle through all targets located in close proximity to where the screen has been touched AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 Page 25 of 26 7 14 GWX 70 Weather Radar Optional The GWX 70 Weather Radar uses Doppler technology to provide advanced features to the flight crew such as turbulence detection and ground clutter suppression These features that rely on Doppler technology are only supported with on GWX 70 units that have a 12 inch antenna or lager Turbulence detection is only supported at display ranges 40 160 nautical miles NOTE Turbulence detection does not detect all turbulence especially that which is occurring in clear air The display of turbulence indicates the possibility of Severe or greater turbulence as defined in the Aeronautical Information Manual 7 15 Charts Optional The GTN 750 725 can display both procedure charts and weather data on the main map page at the same time When datalinked Nexrad or Precipitation is overlaid on the main map page the weather data is displayed below an overlaid procedure chart When airborne weather radar is overlaid on the main map page the radar data is displayed above an overlaid procedure chart 7 16 Transponder Control Optional
9. 14 7 15 7 16 190 01007 A5 Rev 2 Databases External Switches Airspace Depiction and Alerts GDL 88 ADS B Traffic System Interface Optional GWX 70 Weather Radar Optional Charts Optional Transponder Control Optional Page 4 of 26 AFMS GTN GPS SBAS System NO IFR GPS FAA APPROVED Section 1 GENERAL 1 1 Garmin GTN Navigators The Garmin GTN navigation system is a GPS system with a Satellite Based Augmentation System SBAS comprised of one or more Garmin TSO C146c GTN 625 635 650 725 or 750 navigator s and one or more Garmin approved GPS SBAS antenna s GTN system functions are shown in Table 1 x GTN 625 x GTN 725 GPS SBAS Navigation Not approved for IFR navigation VHF Com Radio 118 00 to 136 990 MHz 8 33 or 25 kHz increments VHF Nav Radio 108 00 to 117 95 MHz 50 kHz increments LOC and Glideslope non precision and precision approach guidance for Cat 1 minimums 328 6 to 335 4 MHz tuning range Moving map including topographic terrain aviation and geopolitical data Display of datalink weather products SiriusXM FIS B x x GTN 635 x x x GTN 650 x x x GTN 750 x lt x lt x lt x x lt x x lt Connext all optional E a 4 Control and display of airborne weather radar optional Display of terminal procedures data optional Display of traffic data including ADS B optional Xx xX X Display of StormScope data optional X X X
10. 2 e Power to the optional GMA 35 is powered through a circuit breaker labeled AUDIO 7 10 Databases Database versions and effective dates are displayed on the start up page immediately after power on Database information can also be viewed on the System System Status page The Obstacle Database coverage area includes the United States and Europe AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 Page 23 of 26 7 11 External Switches External switches may be installed and interfaced to the GTN These switches may be stand alone or integrated with a TAWS or GPS annunciator Table 3 lists the switches and function they perform Switch Label Function CDI Toggles between GPS VLOC sources This switch may be part of an external annunciator panel COM CHAN DN Toggles down through the preset com frequencies COM CHAN UP Toggles up through the preset com frequencies COM RMT XFR Transfers the com active standby frequencies NAV RMT XFR Transfers the nav active standby frequencies OBS Performs an OBS or SUSP function This switch is part of an external annunciator panel and is placarded with the following Green OBS indicates OBS or SUSP mode GTN annunciator bar indicates which is active Push OBS button to change OBS or SUSP mode OBS SUSP Performs an OBS or SUSP function TERR INHB Toggles the TAWS Inhibit function on off This switch is part of an external annunciator panel The te
11. 5 and 750 can interface to a GMA 35 remotely mounted audio panel and marker beacon receiver Controls for listening to various radios activating the cabin speaker clearance playback control and marker beacon are accessed by pressing the Audio Panel button on the GTN display screen Volume controls for the audio panel are accessed by pressing the Intercom button on the GTN display screen AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 Page 21 of 26 7 7 Traffic System Optional This system is configured for the following type of traffic system The Garmin GTN 6XX or GTN 7XX Cockpit Reference Guide or Garmin GTN 6XX or GTN 7XX Pilot s Guide provides additional information regarding the functionality of the traffic device No traffic system is interfaced to the GTN A TAS TCAS I traffic system is interfaced to the GTN A TIS traffic system is interfaced to the GTN A TCAD traffic system is interfaced to the GTN A Garmin GDL 88 ADS B traffic system is interfaced to the GTN A Garmin GDL 88 ADS B traffic system is interfaced to the GTN The GDL 88 ADS B traffic system is also interfaced to an on board traffic system OOaaaaQq 7 8 StormScope Optional When optionally interfaced to a StormScope weather detection system the GTN may be used to display the StormScope information Weather information supplied by the StormScope will be displayed on the StormScope page of the GTN system For detailed
12. Garmin International Inc 1200 E 151 Street Olathe KS 66062 U S A FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for the Garmin GTN 625 635 650 725 or 750 GPS SBAS Navigation System as installed in Make and Model Airplane Registration Number Serial Number GPS FUNCTIONS NOT APPROVED FOR IFR NAVIGATION This document serves as an Airplane Flight Manual Supplement or as a Supplemental Airplane Flight Manual when the aircraft is equipped in accordance with Supplemental Type Certificate SA02019SE D for the installation and operation of the Garmin GTN 625 635 650 725 or 750 GPS SBAS Navigation System This document must be incorporated into the FAA Approved Airplane Flight Manual or provided as an FAA Approved Supplemental Airplane Flight Manual The information contained herein supplements the information in the FAA Approved Airplane Flight Manual For limitations procedures loading and performance information not contained in this document refer to the FAA Approved Airplane Flight Manual markings or placards FAA Approved By 7 E oe Michael Warren ODA STC Unit Administrator Garmin International Inc ODA 240087 CD Date 2 APK 20 2 AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 1 of 26 LOG OF REVISIONS Revision Page Description FAA Approved Number Section 2 11 2 e Modified limitation See Page 1 1 Complete Sup
13. Page 18 of 26 FAA APPROVED 4 6 Telephone amp SMS Text Optional Audio from the GSR 56 Iridium datalink is routed through your aircraft s audio panel Audio from the GSR 56 must be deactivated turned off unless making a phone call The primary indication of an incoming phone call or SMS text are the visual indications on the GIN Section 5 PERFORMANCE No change Section 6 WEIGHT AND BALANCE See current weight and balance data AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 19 of 26 Section 7 SYSTEM DESCRIPTIONS 7 1 Pilot s Guide The Garmin GTN 6XX or GTN 7XX Pilot s Guide part number and revision listed below contain additional information regarding GTN system description control and function The Pilot s Guides do not need to be immediately available to the flight crew e GTN 6XX Pilot s Guide P N 190 01004 03 Rev C or later e GTN 7XX Pilot s Guide P N 190 01007 03 Rev C or later 7 2 Leg Sequencing The GTN supports all ARINC 424 leg types Certain leg types require altitude input in order to sequence course to altitude for example If a barometric corrected altitude source is not interfaced to the GTN a popup will appear prompting the flight crew to manually sequence the leg once the altitude prescribed in the procedure is reached O This installation has a barometric corrected altitude source The GTN will automatically sequence altitude legs O This installation d
14. Pilot s Guide and PC based simulator Pilots should take full advantage of these training tools to enhance system familiarization 4 1 Unit Power On Database ccccssessscccececsessnsscecececsessntsaeceeeees REVIEW EFFECTIVE DATES Self Test si cciseisiacdicheivelenietecelies VERIFY OUTPUTS TO NAV INDICATORS Self Test TAWS Remote Annunciator BUTS Po EEE A A Padaisen etre tn neo ILLUMINATED DEER Races ses E S EE EE E E EEA ILLUMINATED TERR N A a a n a ebea woes ILLUMINATED TERRSEN HE a n a aa E lecoendevence ILLUMINATED Self Test GPS Remote Annunciator N LOC pa ht eh ILLUMINATED GPSen ranan a a a n ILLUMINATED Telephone Audio if equipped Pilot Co pilot Passenger sssicsioseisiesssestessesssersotsesie seant DEACTIVATED 4 2 Before Takeoff System Messages and Annunciators seeeeseeeseeeersererrsreerrserers CONSIDERED 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 16 of 26 FAA APPROVED 4 3 HSI and EHSI Operation If an HSI is used to display navigation data from the GTN the pilot should rotate the course pointer as prompted on the GTN If an EHSI is used to display navigation data from the GTN the course pointer may autoslew to the correct course when using GPS navigation When using VLOC navigation the course pointer will not autoslew and must be rotated to the correct course by the pilot For detailed information about the functionality of the EHSI system refer to the FAA approved F
15. TAWS INHIBIT The TAWS Forward Looking Terrain Avoidance FLTA and Premature Descent Alerts PDA functions may be inhibited to prevent alerting if desired Refer to GTN Cockpit Reference Guide for additional information To Inhibit TAWS Home Hard eyssc iis thes os oes teeistiatoeectisietn EE E EEA E tee eets PRESS Lerrain BU O destek ces Soedeesscaea sca seed ecdeus caaueseae TOE S RSS PRESS Menu Button E A E E E E eva ea anette PRESS TAWS Inhibit Button ce ceccscccssceceesseeeceeaeees PRESS TO ACTIVATE 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 14 of 26 FAA APPROVED 3 2 5 TER N A and TER FAIL If the amber TER N A or TER FAIL status annunciator is displayed the system will no longer provide TAWS alerting or display relative terrain and obstacle elevations The crew must maintain compliance with procedures that ensure minimum terrain and obstacle separation 3 2 6 DATA SOURCE HEADING SOURCE INOPERATIVE OR CONNECTION TO GTN LOST MESSAGE Without a heading source to the GTN the following features will not operate e GPSS will not be provided to the autopilot for heading legs The autopilot must be placed in HDG mode for heading legs e Map cannot be oriented to Heading Up e All overlaying traffic data from a TAS TCAS I or GDL 88 interfaced to an on board traffic system on the main map display The flight crew must use the dedicated traffic page on the GTN system to display TAS TCAS I or GDL 88 traffic data
16. g source as indicated by the HDG N A label at the upper right corner of the StormScope page strikes must be cleared after each heading change AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 11 of 26 2 11 Flight Planner Calculator Functions The Fuel Planning page uses Fuel on Board or Fuel Flow as received from an on board fuel totalizer as entered by the pilot at system startup or as entered by the pilot when on the Fuel Planning page This is not a direct indication of actual aircraft fuel flow or fuel on board and those values are only used for the Fuel Planning page The fuel required to destination is only a calculated and predicted value based on the data entered into the planner It is not a direct indication of how much fuel the aircraft will have upon reaching the destination 2 12 Glove Use Covered Fingers No device may be used to cover fingers used to operate the GTN unless the Glove Qualification Procedure located in the Pilot s Guide Cockpit Reference Guide has been successfully completed The Glove Qualification Procedure is specific to a pilot glove GTN 725 750 or GTN 625 635 650 combination 2 13 Demo Mode Demo mode may not be used in flight under any circumstances 2 14 Active Weather RADAR Radar is broadcasting energy while in Weather or Ground mapping modes If the GTN system is configured to control an airborne weather radar unit observe all safety precautions includi
17. ine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather product may be significantly older than the indicated weather product age Do not rely solely upon data link services to provide Temporary Flight Restriction TFR or Notice to Airmen NOTAM information Not all TFRs and NOTAMS can be depicted on the GIN 2 9 Traffic Display Optional Traffic may be displayed on the GTN when connected to an approved optional TCAS I TAS TIS or ADS B traffic device These systems are capable of providing traffic monitoring and alerting to the flight crew Traffic shown on the display may or may not have traffic alerting available The display of traffic is an aid to visual acquisition and may not be utilized for aircraft maneuvering 2 10 StormScope Display Optional StormScope lightning information displayed by the GTN is limited to supplemental use only The use of the StormScope lightning data on the display for hazardous weather thunderstorm penetration is prohibited StormScope lightning data on the display is intended only as an aid to enhance situational awareness of hazardous weather not penetration It is the flight crew s responsibility to avoid hazardous weather using official weather data sources When the GTN StormScope page is operating without a headin
18. information about the capabilities and limitations of the StormScope system refer to the documentation provided with that system Heading Up mode If the GTN system is receiving valid heading information the StormScope page will operate in the heading up mode as indicated by the label HDG UP presented at the upper right corner of the display In this mode information provided by the StormScope system is displayed relative to the nose of the aircraft and is automatically rotated to the correct relative position as the aircraft turns Heading Not Available mode If the GTN system is not receiving valid heading information either because a compatible heading system is not installed or the interfaced heading system has malfunctioned the StormScope page will continue to operate without a heading source and indicate HDG N A in the upper right corner of the GTN display In this mode information provided by the StormScope system is displayed relative to the nose of the aircraft but is not automatically rotated to the correct relative position as the aircraft turns When operating in this mode StormScope strikes must be cleared after each turn the aircraft performs 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 22 of 26 7 9 Power e Power to the GTN is provided through a circuit breaker labeled NAV GPS 1 2 e Power to the optional GTN COM is provided through a circuit breaker labeled COMM 1
19. light Manual or Flight Manual Supplement for that system CAUTION The pilot must verify the active course and waypoint for each flight plan leg The pilot must verify proper course selection each time the CDI source is changed from GPS to VLOC 4 4 Autopilot Operation The GTN may be coupled to an optional autopilot if installed in the aircraft when operating as prescribed in the LIMITATIONS section of this manual Autopilots coupled to the GTN system in an analog NAV mode will follow GPS or VHF navigation guidance as they would with existing VOR receivers Autopilots that support GPSS or GPS Roll Steering in addition to the analog course guidance will lead course changes fly arcing procedures procedure turns and holding patterns if coupled in GPSS mode CAUTION The GTN cannot provide course deviation to the autopilot for heading legs Some autopilots do not allow the use of GPSS when course deviation is not provided For autopilot operating instructions refer to the FAA approved Flight Manual or Flight Manual Supplement for the autopilot AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 17 of 26 4 5 Coupling the Autopilot during approaches The GTN may be coupled to an optional autopilot if installed in the aircraft when operating as prescribed in the LIMITATIONS section of this manual CAUTION When the CDI source is changed on the GTN autopilot mode may change Confirm autopilot mode selection
20. ng e Do not operate in the vicinity of refueling operations e Do not operate while personnel are in the vicinity approximately 20 feet of the radar sweep area CAUTION If a radar system is installed it generates microwave radiation and improper use or exposure may cause serious bodily injury Do not operate the radar equipment until you have read and carefully followed the safety precautions and instructions in the weather radar user manual and or pilot s guide 2 15 Telephone Audio Telephone audio may not be distributed to the pilot or co pilot unless a phone call is active 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 12 of 26 FAA APPROVED Section 3 EMERGENCY PROCEDURES 3 1 Emergency Procedures 3 1 1 TAWS WARNING Red annunciator and aural PULL UP AUtOpilOts oheriou reie eei eo raaa EEE E E DISCONNECT Aircraft Controls ccccececeeeeeees INITIATE MAXIMUM POWER CLIMB Airspeed bee csiisilecceneceesdestveteseegtescedt desehesseess BEST ANGLE OF CLIMB SPEED After Warning Ceases POWER esthetic tees ctl sects is cts ate MAXIMUM CONTINUOUS Altitude ic 4 s2aand E CLIMB AND MAINTAIN SAFE ALTITUDE Advise ATC of Altitude Deviation if appropriate NOTE Only vertical maneuvers are recommended unless either operating in visual meteorological conditions VMC or the flight crew determines based on all available information that turning in addition to the vertical escape maneuver is the
21. ocalizer Performance with Vertical Guidance NOTAM Notice to Airmen OBS Omnibearing Select RMT Remote SBAS Satellite Based Augmentation System SD Secure Digital SUSP Suspend AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 7 of 26 TAS Traffic Awareness System TAWS Terrain Awareness and Warning System TCAS Traffic Collision Avoidance System TFR Temporary Flight Restriction TIS Traffic Information Service VHF Very High Frequency VFR Visual Flight Rules VLOC VOR Localizer VMC Visual Meteorological Conditions VOR VHF Omnidirectional Range XFR Transfer 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 8 of 26 FAA APPROVED Section 2 LIMITATIONS 2 1 Cockpit Reference Guide The Garmin GTN 6XX or GTN 7XX Cockpit Reference Guide part number and revision listed below or later revisions must be immediately available to the flight crew whenever navigation is predicated on the use of the GIN e GTN 6XX Cockpit Reference Guide P N 190 01004 04 Rev C e GTN 7XX Cockpit Reference Guide P N 190 01007 04 Rev C 2 2 Kinds of Operation This AFM supplement does not grant approval for IFR operations to aircraft limited to VFR operations The GPS navigation capability of this unit cannot be used as primary navigation for IFR operations This system is placarded in close proximity to the GTN GPS LIMITED TO VFR USE ONLY 2 3 Applicable System Software This AFMS
22. oes not have a barometric corrected altitude source The flight crew will be prompted to manually sequence altitude legs 7 3 Auto ILS CDI Capture Auto ILS CDI Capture will not automatically switch from GPS to VLOC for LOC BC or VOR approaches 7 4 Activate GPS Missed Approach O This installation will autoswitch from VLOC to GPS when the Activate GPS Missed Approach button is pressed O This installation will not autoswitch from VLOC to GPS when the Activate GPS Missed Approach button is pressed The pilot must manually switch from VLOC to GPS if GPS guidance is desired after the missed approach point 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 20 of 26 7 5 Terrain Proximity and TAWS e The Obstacle Database has an area of coverage that includes the United States and Europe and is updated as frequently as every 56 days e To avoid unwanted alerts TAWS may be inhibited when landing at an airport that is not included in the airport database NOTE The area of coverage may be modified as additional terrain data sources become available O This installation supports Terrain Proximity No aural or visual alerts for terrain or obstacles are provided Terrain Proximity does not satisfy the TAWS requirement of 91 223 O This installation supports TAWS B Aural and visual alerts will be provided This installation does support the TAWS requirement of 91 223 7 6 GMA 35 Audio Panel Optional The GTN 72
23. play HOME Key Photo Sensor SD Card a Message irect To Key Annunciation A nd Key Large and Locking Small Knobs Screw Annunciations Hints Xpadr Panel Controls Figure 2 GTN 635 650 Control and Display Layout 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 6 of 26 FAA APPROVED 1 2 Capabilities The GTN system and associated navigation interface in this aircraft have the following capability in addition to the core multifunction display capability O VHF Communication Radio O Primary VHF Navigation O TSO C151b Terrain Awareness and Warning System See section 2 7 1 3 Electronic Flight Bag The GTN 750 725 are operationally suitable as Class 3 Hardware Type B Software in accordance with AC 120 76B EFB electronic aeronautical information when using current FliteChart or ChartView data 1 4 Definitions The following terminology is used within this document ADS B Automatic Dependent Surveillance Broadcast AEG Aircraft Evaluation Group FAA APR Approach CDI Course Deviation Indicator EFB Electronic Flight Bag EHSI Electronic Horizontal Situation Indicator FIS B Flight Information Services Broadcast GPS Global Positioning System GPSS GPS Roll Steering GTN Garmin Touchscreen Navigator HSI Horizontal Situation Indicator IFR Instrument Flight Rules ILS Instrument Landing System LNAV Lateral Navigation LOC Localizer LOC BC Localizer Backcourse LP Localizer Performance LPV L
24. plement See Page 1 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 2 of 26 FAA APPROVED Table of Contents SECTION Section 1 GENERAL 1 1 Garmin GTN Navigators 1 2 Capabilities 1 3 Electronic Flight Bag 1 4 Definitions Section 2 LIMITATIONS 2 1 2 2 2 3 2 4 25 2 6 2 13 2 14 2 15 Cockpit Reference Guide Kinds of Operation Applicable System Software SD Card Ground Operations Terrain Proximity Function All Units TAWS Function Optional Datalinked Weather Display Optional Traffic Display Optional StormScope Display Optional Flight Planner Calculator Functions Glove Use Covered Fingers Demo Mode Active Weather RADAR Telephone Audio Section 3 EMERGENCY PROCEDURES 3 1 3 2 Emergency Procedures Abnormal Procedures Section 4 NORMAL PROCEDURES Unit Power On Before Takeoff HSI and EHSI Operation Autopilot Operation Coupling the Autopilot during approaches Telephone amp SMS Text Optional Section 5 PERFORMANCE Section 6 WEIGHT AND BALANCE Section 7 SYSTEM DESCRIPTIONS 7 1 Ted 73 74 7 5 7 6 7 1 7 8 7 9 Pilot s Guide Leg Sequencing Auto ILS CDI Capture Activate GPS Missed Approach Terrain Proximity and TAWS GMA 35 Audio Panel Optional Traffic System Optional StormScope Optional Power AFMS GTN GPS SBAS System NO IFR GPS FAA APPROVED PAGE OOOEernnrnInrnunn 190 01007 A5 Rev 2 Page 3 of 26 7 10 7 11 7 12 7 13 7
25. rrain display is still presented if TAWS is Inhibited Table 3 External Switches 7 12 Airspace Depiction and Alerts The GTN aides the flight crew in avoiding certain airspaces with Smart Airspace and airspace alerts Smart Airspace de emphasizes depicted airspace that is not near the aircraft s current altitude Airspace Alerts provide a message indication to the flight crew when the aircraft s current ground track will intercept an airspace type that has been selected for alerting NOTE Smart Airspace and Airspace Alerts are separate features Turning on off Smart Airspace does not affect Airspace Alerts and vice versa 190 01007 A5 Rev 2 AFMS GTN GPS SBAS System NO IFR GPS Page 24 of 26 7 13 GDL 88 ADS B Traffic System Interface Optional The GDL 88 is an ADS B traffic system that can interface to the GTN The nose of the ownship symbol on both the GTN main map page and dedicated traffic page serves as the actual location of your aircraft The center of the traffic target icon serves as the reported location for the target aircraft Motion vectors for traffic may be displayed in either absolute or relative motion The location of the traffic targets relative to the ownship are the same regardless of the selected motion vector Absolute motion vectors are colored either cyan or white depending on unit configuration Absolute motion vectors depict the reported track of the traffic target referenced to the ground
26. safest course of action or both AFMS GTN GPS SBAS System NO IFR GPS 190 01007 A5 Rev 2 FAA APPROVED Page 13 of 26 3 2 Abnormal Procedures 3 2 1 LOSS OF COM RADIO TUNING FUNCTIONS If alternate COM is available COMMUNICATIONS cee ee cece cece eeeseeccececssseeseeceesseesanense USE ALTERNATE COM If no alternate COM is available COM RMT XFR key if installed PRESS AND HOLD FOR 2 SECONDS NOTE This procedure will tune the active COM radio the emergency frequency 121 5 regardless of what frequency is displayed on the GTN Certain failures of the tuning system will automatically tune 121 5 without flight crew action 3 2 2 LOSS OF AUDIO PANEL FUNCTIONS GMA 35 Only Audio Panel Circuit Breakers nn i a a I a harao PULL NOTE This procedure will force the audio panel into fail safe mode which provides only the pilot with communications and only on a single COM radio If any non GTN 750 COM is installed communication will be only on that radio If only a GTN 750 is installed in the aircraft then the pilot will have only the GTN 750 COM available No other audio panel functions including the crew and passenger intercom will function 3 2 3 TAWS CAUTION Terrain or Obstacle Ahead Sink Rate Don t Sink When a TAWS CAUTION occurs take corrective action until the alert ceases Stop descending or initiate either a climb or a turn or both as necessary based on analysis of all available instruments and information 3 2 4
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