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MARCH 18, 2011 

GARMIN Ltd. or its Subsidiaries, c/o 
Garmin International 1200 E. 151

st

 Street 

Olathe, KS 66062 USA 

AIRPLANE FLIGHT MANUAL SUPPLEMENT or 

SUPPLEMENTAL AIRPLANE FLIGHT MANUAL 

for STC SA02019SE-D GARMIN GTN  

NAVIGATION SYSTEM 

 

190-01007-A2 Rev. 1  

Page 27 of 31 

FAA APPROVED DATE: _________________ 

4.5

 

Coupling the Autopilot during approaches 

 

CAUTION 

When the CDI source is changed on the GTN, autopilot mode may change. 
Confirm autopilot mode selection after CDI source change on the GTN. Refer to 
the FAA approved Flight Manual or Flight Manual Supplement for the autopilot. 

 

…

  This installation prompts the pilot 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 ........................................................................... 

PRESS

 

“Enable APR Output” Button .................................................................... 

PRESS

 

 
If coupled, Autopilot will revert to ROL mode at this time. 
 
Autopilot .......................................................... 

ENGAGE APPROACH MODE

 

 

…

  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 ...................................................... 

CONFIRM AVAILABLE

 

Autopilot .......................................................... 

ENGAGE APPROACH MODE

 

 

…

  The autopilot does not support any vertical capture or tracking in this 

installation. 

  
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. 

Summary of Contents for GTN 625

Page 1: ......

Page 2: ......

Page 3: ...ware 15 2 7 SD Card 15 2 8 Navigation Database 15 2 9 Ground Operations 16 2 10 Approaches 16 2 11 Autopilot Coupling 17 2 12 Terrain Proximity Function All Units 17 2 13 TAWS Function Optional 17 2 1...

Page 4: ...T MANUAL for STC SA02019SE D GARMIN GTN NAVIGATION SYSTEM 190 01007 A2 Rev 1 Page 4 of 31 FAA APPROVED DATE _________________ 7 3 Auto ILS CDI Capture 28 7 4 Activate GPS Missed Approach 29 7 5 Terrai...

Page 5: ...LPV X X X X X VHF Com Radio 118 00 to 136 990 MHz 8 33 or 25 kHz increments X X X VHF Nav Radio 108 00 to 117 95 MHz 50 kHz increments X X LOC and Glideslope non precision and precision approach guid...

Page 6: ...KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE D GARMIN GTN NAVIGATION SYSTEM 190 01007 A2 Rev 1 Page 6 of 31 FAA APPROVED DATE ______________...

Page 7: ...erators require operational approval from the FAA The Garmin GNSS navigation system as installed in this aircraft complies with the equipment requirements of AC 90 100A for RNAV 2 and RNAV 1 operation...

Page 8: ...LOA in accordance with AC 20 153 for database integrity quality and database management practices for the Navigation database Flight crew and operators can view the LOA status at FlyGarmin com then s...

Page 9: ...gation Satellite System GPS Global Positioning System GPSS GPS Roll Steering GTN Garmin Touchscreen Navigator HSI Horizontal Situation Indicator IAP Instrument Approach Procedure IFR Instrument Flight...

Page 10: ...PROVED DATE _________________ SDF Simplified Directional Facility SUSP Suspend TACAN Tactical Air Navigation System TAS Traffic Awareness System TAWS Terrain Awareness and Warning System TCAS Traffic...

Page 11: ...ow or later revisions must be immediately available to the flight crew whenever navigation is predicated on the use of the GTN y GTN 6XX Cockpit Reference Guide P N 190 01004 04 Rev A y GTN 7XX Cockpi...

Page 12: ...installations require an external GPS annunciator panel If installed this annunciator must be fully functional to use the GTN for IFR operations Single engine piston aircraft under 6 000 lbs maximum...

Page 13: ...pace System on RNP and RNAV procedures when SBAS signals are not available the availability of GPS RAIM shall be confirmed for the intended route of flight In the event of a predicted continuous loss...

Page 14: ...flight plan from the database in their entirety rather than loading route waypoints from the database into the flight plan individually Selecting and inserting individual named fixes from the databas...

Page 15: ...route oceanic and terminal navigation is prohibited unless the pilot verifies and uses a valid compatible and current Navigation database or verifies each waypoint for accuracy by reference to current...

Page 16: ...and fly an instrument approach procedure is indicated by the title of the procedure and notes on the IAP chart Navigating the final approach segment that segment from the final approach fix to the mis...

Page 17: ...ap 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 Terrai...

Page 18: ...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 en...

Page 19: ...t Olathe KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE D GARMIN GTN NAVIGATION SYSTEM 190 01007 A2 Rev 1 Page 19 of 31 FAA APPROVED DATE _____...

Page 20: ...ures 3 1 1 TAWS WARNING Red annunciator and aural PULL UP Autopilot DISCONNECT Aircraft Controls INITIATE MAXIMUM POWER CLIMB Airspeed BEST ANGLE OF CLIMB SPEED After Warning Ceases Power MAXIMUM CONT...

Page 21: ...Loss Of Integrity mode LOI The mode is indicated on the GTN by an amber DR or LOI If the Loss Of Integrity annunciation is displayed revert to an alternate means of navigation appropriate to the route...

Page 22: ...S LOC VOR DME ADF Are Available Navigation USE ALTERNATE SOURCES If No Alternate Navigation Sources Are Available DEAD RECKONING DR MODE Navigation USE GTN NOTE y All information normally derived from...

Page 23: ...tely upon viewing the message the unit will revert to Terminal navigation mode alarm limits If the position integrity is within these limits lateral guidance will be restored and the GPS may be used t...

Page 24: ...ystem 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...

Page 25: ...ed at the expense of basic instrument flying in IMC and basic see and avoid in VMC Garmin provides training tools with the Pilot s Guide and PC based simulator Pilots should take full advantage of the...

Page 26: ...system CAUTION 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...

Page 27: ...nce 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 PRESS Enable APR Output Button...

Page 28: ...ly available to the flight crew y GTN 6XX Pilot s Guide P N 190 01004 03 Rev A or later y GTN 7XX Pilot s Guide P N 190 01007 03 Rev A or later 7 2 Leg Sequencing The GTN supports all ARINC 424 leg ty...

Page 29: ...0 Latitude in all longitudes y The Obstacle Database has an area of coverage that includes the United States and Europe and is updated as frequently as every 56 days y To avoid unwanted alerts TAWS ma...

Page 30: ...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 m...

Page 31: ...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 perfor...

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