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190-01754-01 Rev. 4 

FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 

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7-3

 

turn rate tick mark, corresponding to a predicted heading of 18˚ from the current heading. At rates 
greater  than  4  deg/sec,  an  arrowhead  appears  at  the  end  of  the  magenta  trend  vector  and  the 
prediction is no longer valid. 
 
The  Airspeed  Indicator  may  be  displayed  as  a  vertical  tape  or  a  round  dial.    When  the  Airspeed 
Indicator is displayed as a tape, it  displays a range of 70 knots on a rolling number gauge using a 
vertical tape.    Numeric labels and major tick marks are shown at intervals of 10 knots.    Minor tick 
marks are at intervals of 5 knots.    The current airspeed is displayed in the black pointer.    The True 
Airspeed (TAS) is displayed above the scale in white digits and the Ground Speed (GS) is displayed 
below the scale in magenta digits. 
 
The Altimeter may be displayed as a vertical tape or a round dial.    When the Altimeter is displayed 
as a tape, it displays 400 feet of barometric altitude values at a time on a rolling number gauge using 
a  moving  tape.  Numeric  labels  and  major  tick  marks  are  shown  at  intervals  of  100  feet.  Minor  tick 
marks are at intervals of 20 feet. The current altitude is displayed in the black pointer. The barometric 
pressure setting is displayed below the Altimeter in inches of mercury (in Hg) or hectopascals (hPa) 
when metric units are selected. 
 
The Selected Altitude is displayed above the Altimeter in the box indicated by a selection bug symbol. 
A bug corresponding to this altitude is shown on the  altimeter; if the Selected Altitude exceeds the 
range shown on the tape, the bug appears at the corresponding edge of the tape. 
 
The  Altitude  Alerting  function  provides  the  pilot  with  visual  and  aural  alerts  when  approaching  the 
Selected  Altitude.  Whenever  the  Selected  Altitude  is  changed,  the  Altitude  Alerter  is  reset.  The 
following will occur when approaching the Selected Altitude:   
 

 

Passing  within  1000  feet  of  the  Selected  Altitude,  the  Selected  Altitude  (shown  above  the 
Altimeter) flashes for 5 seconds and an aural tone is generated.   
 

 

When the aircraft passes within 200 ft of the Selected Altitude, the Selected Altitude flashes 
for 5 seconds and an aural tone is generated to indicate that the aircraft is approaching the 
selected altitude. 
 

 

After reaching the Selected Altitude, if the pilot flies outside the deviation band (±200 Feet of 
the Selected Altitude), the Selected Altitude changes to Amber text on a black background, 
flashes for 5 seconds, and an aural tone is generated. 

 

The Vertical Speed Indicator (VSI) may be displayed as a tape or an arc segment.    The VSI displays 
the aircraft vertical speed using a non-moving tape labeled at 500, 1000 and every 1000 fpm up to the 
maximum with minor tick marks every 100 feet up to 1000 fpm. The current vertical speed is displayed 
using a white arrow along the scale. 
 

7.2  Vertical Deviation Indicators 

 
The Vertical Deviation (Glideslope) Indicator (VDI) appears to the left of the altimeter whenever an ILS 
frequency is tuned in the active NAV field of an external navigator. A green diamond acts as the VDI 
Indicator. The green 'G' indicates an external glideslope source. If a localizer frequency is tuned and 
there is no glideslope signal, “NO GS” is annunciated. 
 

Summary of Contents for G3X Touch

Page 1: ......

Page 2: ...y grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and to print one copy of this manual o...

Page 3: ...REV NO PAGE NO S DESCRIPTION DATE OF APPROVAL FAA APPROVED 1 ALL Original Issue 03 15 19 Robert Murray ODA STC Unit Administrator 2 2 2 2 5 Added limitation for installations with an autopilot other t...

Page 4: ...FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 190 01754 01 Rev 4 Page ii This page intentionally left blank...

Page 5: ...Angle 2 2 2 8 ADAHRS Normal Operating Mode 2 2 2 9 Aerobatic Maneuvers 2 2 2 10 Other Autopilots 2 2 2 11 Synthetic Vision 2 2 2 12 Moving Maps 2 2 2 13 Terrain Display 2 2 2 14 Terrain Alerts 2 3 2 1...

Page 6: ...ORE STARTING ENGINE 4 1 4 2 AFTER STARTING ENGINE 4 1 4 3 COM Radio Tuning Optional 4 2 4 4 Lateral Navigation 4 2 4 5 APPROACHES 4 3 4 6 Barometric Minimums Alert 4 14 4 7 TRANSPONDER Operation Optio...

Page 7: ...ude air data heading and navigation information to the pilot Multi Function Display MFD Provides pilot awareness of factors that may affect the overall conduct of the flight such as advanced moving ma...

Page 8: ...FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 190 01754 01 Rev 4 P a g e 1 2 Single 7 Portrait GDU PFD with MFD in split mode No EIS Single 10 GDU PFD MFD EIS Optional...

Page 9: ...190 01754 01 Rev 4 FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS P a g e 1 3 Dual 7 Portrait GDUs PFD MFD EIS Optional One 10 One 7 Portrait GDU PFD MFD EIS Optional...

Page 10: ...ociated engine sensors MFD functions are supported by an internal GPS receiver or an external IFR GPS navigator interface G3X Touch flight displays can be seamlessly integrated with a variety of radio...

Page 11: ...uch to a Garmin IFR navigator an installation could maintain IFR capability by retaining non Garmin GPS and or VHF Nav radios along with their standalone dedicated CDI NOTE Refer to the Airplane Fligh...

Page 12: ...FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 190 01754 01 Rev 4 P a g e 1 6 This page intentionally left blank...

Page 13: ...nt AHRS Attitude Heading Reference System ALT Altitude AML Approved Model List AMMD Airport Moving Map Display AOA Angle of Attack AP Autopilot APV Approach with Vertical Guidance ARINC Aeronautical R...

Page 14: ...min Navigator Transponder GP Glide Path GPS Global Positioning System GS Glide Slope or Ground Speed GSU Garmin Sensor Unit ADAHRS GTN Garmin Touch Navigation GTP Garmin Temperature Probe HDG Heading...

Page 15: ...REV Revision or Reversion RNAV Area Navigation RPM Revolutions per Minute SBAS Satellite Based Augmentation System SD Card Secure Digital Card SFD Standby Flight Display SL30 Garmin nav com transceive...

Page 16: ...FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 190 01754 01 Rev 4 P a g e 1 10 YD Yaw Damper...

Page 17: ...190 01754 01 Rev 4 FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS P a g e 1 11 This page intentionally left blank...

Page 18: ......

Page 19: ...or IFR operations 2 3 Navigation Systems for IFR Operations Aircraft approved for IFR operations must use one of the following Garmin navigation systems GNC 300XL GPS 155XL GNS 4XX W GNS 5XX W GNS 480...

Page 20: ...ating Mode IFR operations are prohibited unless the ADAHRS is receiving valid GPS signals or Air Data 2 9 Aerobatic Maneuvers Do not conduct aerobatic maneuvers if uninterrupted attitude information i...

Page 21: ...d with a fuel flow gauge which measured metered fuel pressure may have this gauge replaced by a gauge which measures fuel flow directly When these gauges are replaced in accordance with this STC the f...

Page 22: ...perational regulation regarding portable electronic devices Data provided to a portable electronic device from the G3X Touch Bluetooth interface is not approved to replace any aircraft display equipme...

Page 23: ...if installed Equipment Number installed Req d EIS Display 1 1 Engine Adaptor Unit GEA 24 1 1 The following engine indications must be functional on the EIS display if these gauges are present on the...

Page 24: ...FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 190 01754 01 Rev 4 P a g e 2 6 This page intentionally left blank...

Page 25: ...ta from the G5 will be displayed on the G3X Touch If installed the GFC 500 autopilot will function normally 3 2 Attitude Failure GSU 25 AHRS FAIL Attitude failure is indicated by removal of the sky gr...

Page 26: ...n PFD Continuous high low aural tone 1 Aircraft Attitude MAINTAIN REGAIN AIRCRAFT CONTROL 2 FD Mode Bar on PFD PRESS to cancel disconnect tone and extinguish annunciator 3 6 G3X Touch Altimeter Barome...

Page 27: ...HRS REVERT and ECS FAIL messages will be displayed This will restore the autopilot and flight director 3 9 G3X Touch Failure Annunciations If a G3X Touch function fails a large red X is typically disp...

Page 28: ...or attitude airspeed altitude and heading reference 2 Refer directly to the navigation source for navigation information such as GPS 3 If autopilot is engaged verify autopilot mode and cross check aga...

Page 29: ...um takeoff power and best angle of climb airspeed NOTE Only the climb maneuver is recommended unless operating in VMC or it is determined based on all available information that turning in addition cl...

Page 30: ...e appropriate action to correct condition causing engine parameter exceedance The engine parameter has exceeded the warning threshold AP Manually fly the airplane Silence the autopilot disconnect tone...

Page 31: ...Keep Wings Level Fly aircraft manually and crosscheck attitude indication with standby attitude indicator and other sources of attitude information Limit aircraft attitude to 10 bank and 5 pitch as AH...

Page 32: ...orrect condition causing engine parameter exceedance The engine parameter has exceeded the caution threshold GPSS De select GPSS on the G3X Touch and select desired alternate autopilot lateral mode Th...

Page 33: ...n and Select 4 Select External GPS for IFR or VFR flight or 5 Select Internal for VFR only flight 6 Press and Hold BACK Button to return to normal PFD display G3X Touch CDI source Touch the HSI displa...

Page 34: ...transfer STBY frequency to Active frequency 1 Touch the Active COM frequency field 4 4 Lateral Navigation Changing the Navigation Source When an external navigator that supports both GPS and VOR ILS...

Page 35: ...ernal navigator 2 Select waypoint and make it the active waypoint 3 Set external navigator to OBS mode 4 G3X Touch CDI source Touch the HSI display on the PFD PFD Options window opens 5 Select the ext...

Page 36: ...on the PFD Enter the desired LOC course press ENTER 8 Establish Intercept Heading 9 Verify ACTIVE and ARMED modes on the PFD FD mode bar if using the autopilot FD 10 Upon reaching the LOC course turn...

Page 37: ...normal landing OR Press GO AROUND button and fly the missed approach procedure ILS GLIDE SLOPE INOPERATIVE 1 Load the approach into the External navigator Verify external navigator tunes the proper f...

Page 38: ...Source Select GPS on the external navigator 8 Select IAF waypoint and execute the Direct TO on the external navigator 9 G3X Touch CDI source Touch the HSI display on the PFD PFD Options window opens 1...

Page 39: ...3 Approach Minimums Set the barometric minimums alert bug On the PFD Touch the HSI Touch the Highlight Minimums window Enter Barometric Altitude Minimums and touch ENTER 4 G3X Touch CDI source Touch...

Page 40: ...roach course the CDI will automatically slew to the inbound course 13 Verify Course pointer slews to the front course 14 Upon reaching the GPS course turn inbound and follow the GPS course and GP vert...

Page 41: ...gation mode indicates the approach being flown LNAV or LP 12 Set Minimum Descent Altitude MDA Touch the Reference Altitude display Enter the Minimum Descent Altitude 13 At the Final Approach Fix FAF b...

Page 42: ...19 At Missed Approach Point Continue visually for a normal landing OR Press GO AROUND button and fly the missed approach procedure VOR APPROACH 1 Load the approach into the External navigator Verify...

Page 43: ...ECT TO the IAF on the External navigator 7 Navigation Source Select GPS on the external navigator 8 Select IAF waypoint and execute the Direct TO on the external navigator 9 G3X Touch CDI source Touch...

Page 44: ...rs to Final on the external navigator Verify CDI changes slews to the localizer front course 8 Navigation Source Select LOC on the external navigator 9 G3X Touch CDI source Touch the HSI display on th...

Page 45: ...The airplane will navigate in GPS mode throughout the intermediate portion of the approach procedure 13 When established inbound to the FAF Navigation Source Select LOC on the external navigator 14 V...

Page 46: ...plane is established on a defined leg of the procedure 8 Set Missed Approach Altitude Touch the Reference Altitude display Enter the Missed Approach Altitude 4 6 Barometric Minimums Alert A barometric...

Page 47: ...he top of the PFD Automatic Flight Control System window opens 2 Highlight and Select ESP The green ESP status bar extinguishes ESP is disabled 3 Press and Hold the BACK button to close the Automatic...

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Page 49: ...190 01754 01 Rev 4 FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS P a g e 5 1 5 PERFORMANCE No change...

Page 50: ...FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 190 01754 01 Rev 4 P a g e 5 2 This page intentionally left blank...

Page 51: ...190 01754 01 Rev 4 FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS Page 6 1 6 WEIGHT AND BALANCE See current weight and balance data...

Page 52: ...FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 190 01754 01 Rev 4 Page 6 2 This page intentionally left blank...

Page 53: ...played over a virtual blue sky and synthetic ground with a white horizon line The Attitude Indicator displays the pitch indicated by the Amber symbolic aircraft on the pitch scale roll and slip skid i...

Page 54: ...in Menu enabled BACK Key Press to return to the previous screen Press and hold to return to the default MFD Page The Standard Rate Turn Bank Angle Pointers are green pointers displayed on the roll sca...

Page 55: ...shown on the altimeter if the Selected Altitude exceeds the range shown on the tape the bug appears at the corresponding edge of the tape The Altitude Alerting function provides the pilot with visual...

Page 56: ...pending on the external navigator s configured Amber LOI Loss of GPS integrity Amber or Magenta VFR An external GPS source is configured but there is not enough guidance data for IFR use Amber REV Ext...

Page 57: ...r will automatically do so if the installed PFD display fails The display of PFD information on an MFD is a duplication of the original PFD information and is not an independent compilation of data fr...

Page 58: ...ode a green ON indication and transponder code appear in the mode field of the Transponder Data Box Altitude Mode Automatic or Manual ALT Mode is automatically selected when the aircraft becomes airbo...

Page 59: ...existing aircraft pitot static system to determine the aircraft s angle of attack AOA The AOA indications and warnings presented on the G3X system are for reference only and are not intended as repla...

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