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Garmin G5 Electronic Flight Instrument Part 23 AML STC Maintenance Manual Including Instructions for Continued Airworthiness 190-01112-11 July 2016 Revision 1...
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Garmin. Garmin hereby 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...
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RECORD OF REVISIONS Revision Revision Date Description 7/22/16 Initial Release Garmin G5 Electronic Flight Instrument Part 23 AML STC Maintenance Manual 190-01112-11 Rev. 1 Page B...
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California's Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. WARNING Perchlorate Material – special handling may apply, See www.dtsc.ca.gov./hazardouswaste/ perchlorate. Garmin G5 Electronic Flight Instrument Part 23 AML STC Maintenance Manual 190-01112-11 Rev. 1 Page i...
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Keep the battery away from children. Only replace the battery with the approved replacement from Garmin. Using another battery presents a risk of fire or explosion. To purchase a replacement battery, see you Garmin dealer or the Garmin website. Contact your local waste disposal department to dispose of the device and battery in accordance with applicable local laws and regulations.
The following outline briefly describes the organization of this manual: Section 2: System Description Provides a complete description of the type design change associated with installing the G5. An overview of the system interface is also provided. Section 3: Control & Operation Presents basic control and operation information specifically tailored to maintenance practices.
• Roll The G5 has a Turn Rate Indicator located at the bottom of the PFD Page. Tick marks to the left and right of the displayed heading denote standard turn rates (3 deg/sec). A magenta Turn Rate Trend Vector...
A standard-rate turn is shown on the indicator by the trend vector stopping at the standard turn rate tick mark. The G5 displays slip/skid information as indicated by the location of the ball at the lower center portion of the indicator.
4.4 Battery Capacity Check 1. Without power applied to the aircraft, turn on the G5 by pressing the power button in the lower left corner of the unit. 2. Note the remaining battery capacity (%) at the top left corner of the display.
Data logging on the G5 may be used to help troubleshoot issues. Operational data is gathered from the G5 during flight or on ground and is stored in *.csv log files on the microSD™ card (if installed). Garmin G5 Electronic Flight Instrument Part 23 AML STC Maintenance Manual 190-01112-11 Rev.
Unplug any auxiliary power supplies. Removal 1. Insert a hex drive tool through the access hole in the front cover of the G5 as shown in Figure 6-1 loosen the unit from the mounting ring. Figure 6-1 G5 Hex Driver 2.
5. Insert a hex drive tool through the access hole in the front cover of the G5 as shown in Figure 6-1 and tighten the unit to the instrument panel using 10-12 in-lbs torque.
6.3 G5 Mounting Ring Replacement Removal 1. Loosen the G5 unit per Section 6.1. Do not remove the pitot and static lines or the electrical and GPS coaxial cable connectors from the G5 unit if access to the mounting ring can be gained while these items remain connected.
All test equipment must have current calibration records. 7.2 Pitot Static System Leak Check If the pitot and/or static system lines were removed from the G5 unit, perform a pitot static system leak check in accordance with the aircraft manufacturer’s approved data.
7.4 G5 Configuration Mode To enter configuration mode, hold down the knob while powering on the G5. Configuration selections are made by rotating and pressing the knob on the face of the G5 as necessary to select the correct configurations.
Internal GPS Receiver Enabled Navigation Navigation Data Disabled Note: This configuration Page is only present when RS-232 Input Format is configured for MapMx Garmin G5 Electronic Flight Instrument Part 23 AML STC Maintenance Manual 190-01112-11 Rev. 1 Page 15 of 18...
7.5.2 Calibration Procedure C: Air Data Static Pressure Calibration The Air Data configuration page has a selection for static pressure calibration. This procedure is used to perform an altimeter re-calibration. The altitude pressure sensor used in the G5 is very low drift and does not typically require re-calibration.
6. Select Done when the static pressure calibration is successfully completed. 7.6 Altimeter System Test If the G5 unit is replaced, in aircraft that are IFR certified, perform an altimeter system test of the G5 in accordance with 14 CFR Part 43 Appendix E.
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