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190-01754-01 Rev. 4 

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

P a g e

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3-7

 

CAUTION Annunciations 

– Amber

 

Annunciation 

Pilot Action 

Cause 

AP 

Manually fly the airplane 

Pilot has disconnected the autopilot 

YD 

NONE 

Yaw Damper has disconnected 

↑ TRIM UP ↑ 

Move the elevator trim in the nose up direction 
until the annunciation extinguishes. 

The autopilot is holding excessive force due 
to  the  aircraft  being  out  of  trim  due  to 
changes in airspeed or power.     

↓TRIM DOWN↓ 

Move  the  elevator  trim  in  the  nose  down 
direction until the annunciation extinguishes. 

The autopilot is holding excessive force due 
to  the  aircraft  being  out  of  trim  due  to 
changes in airspeed or power.     

MIN SPEED 

Add maximum available power.    Autopilot 
will lower aircraft nose to increase airspeed. 

Airspeed is too slow, approaching stall 
speed. 

MAX SPEED 

Reduce power.    Autopilot will raise aircraft 
nose to reduce airspeed. 

Airspeed is approaching maximum 
airspeed limit. 

HDG 

(amber 

background) 

Use standby compass 

Displayed heading is outside of the internal 
accuracy limits. 

 

Select full screen mode on display to view 
CAUTION annunciations. 

Display is in split screen mode and 
CAUTION annunciations are not displayed. 

AHRS ALIGN 

– 

Keep Wings 

Level 

Fly  aircraft  manually  and  crosscheck  attitude 
indication  with  standby  attitude  indicator  and 
other  sources  of  attitude  information.    Limit 
aircraft attitude to ±10º bank and ±5º pitch as 
AHRS Aligns - OK to taxi. 

Attitude  and  Heading  Reference  System  is 
aligning.    AHRS  may  not  align  with 
excessive pitch/bank angles. 

AHRS ALIGN 

Fly aircraft manually and crosscheck attitude 
indication with standby attitude indicator and 
other sources of attitude information 
(airspeed, heading, altitude, etc.) 

The AHRS monitors have detected a 
possible AHRS malfunction or an error with 
the attitude presentation.    The AHRS is 
attempting to realign itself.    The autopilot 
may automatically disconnect. 

ATT MISCOMP 

Cross-check the flagged information against 
other sources to identify erroneous 
information. 

Difference detected between the G3X 
Touch attitude display and the G5 attitude 
display.   

AHRS FAIL 

ATTITUDE FAIL 

Use standby attitude source, or, if AHRS 
REVERT message is also displayed, continue 
to use the G3X Touch.    Attitude will be from 
the G5. 

The GSU 25 AHRS has failed. 

AHRS REVERT 

Continue to use the G3X Touch.     

The GSU 25 AHRS has failed and attitude 
from the G5 is being displayed on the G3X 
Touch. 

AIR MISCOMP 

IAS MISCOMP 

Cross-check the flagged information against 
other sources to identify erroneous 
information. 

Difference detected between the G3X 
Touch airspeed or altitude and the G5 
airspeed or altitude. 

Содержание G3X Touch

Страница 1: ......

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 18: ......

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 48: ...FAA Approved AFMS or Supplemental AFM for the Garmin G3X Touch EFIS 190 01754 01 Rev 4 P a g e 4 16 This page intentionally left blank...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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