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Garmin G500 Quick Reference

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Garmin G500 Quick Reference GARMIN G500 QUICK REFERENCE CAUTION: The GNS 430 and G500 units each have their G500 Equipped Seminole Differences own databases. Navigation, terrain and map • The G500 powers on and off with the battery master, not the avionics master. information on the G500 Multi-Function • There are no vacuum driven instruments, vacuum pumps, or suction gauge. Instruments are electrically powered. Display (MFD) may not be current and is • The standby attitude indicator must be erected on power-up by pulling the cage knob. not to be used for navigation. Use the G500 • Test the standby attitude battery as directed by the After Start Checklist by pressing and holding the “STBY PWR” MFD for traffic information only. button until amber LED begins flashing. A continuous green light beneath “TEST” during the full sequence indicates that the battery is good. A red light illuminated anytime during the test indicates that the battery is not charged and may require replacement. G500 Setup for Traffic on MFD • The standby attitude indicator warning light will blink for approximately 1 minute when the battery master switch is turned off. DO NOT press the SBY PWR button as it causes continuous operation of the gyro on its emergency battery. ATP recommends setting-up the MFD to display the Exit the airplane with either a blinking LED or red flag. decluttered Traffic Information Service (TIS) page. Configure • G500 equipped Seminoles do not have a conventional turn coordinator. A slip-skid indicator is located at the top of the the G500 screens during the After Start Checklist. attitude indicator. Step on the “brick” instead of the “ball”. Use the reference lines and the magenta line that appears 2 clicks above the heading indicator to identify a standard rate or half-standard rate turn. • Press ENT • Outside air temperature (OAT) displays on PFD under the airspeed tape. There is no OAT probe or analog gauge • Small MFD knob - (displays TIS page) between the windows. • Ground track can be identified on the heading indicator by a small magenta diamond near the lubber line (only visible when ground track is different than heading). • RNG 6 NM • The digital altitude and airspeed readouts are very sensitive and can cause some pilots to continuously make corrections for insignificant deviations. Pilot action - Don’t overcorrect for deviations of a few feet. Crosscheck digital and analog standby instruments to avoid the tendency to overcorrect. PFD Functions PRIMARY FLIGHT DISPLAY (PFD) Checklist Differences These buttons toggle the function of the PFD knob. Use the 2000 and later Seminole GNS 430 checklist with the following differences: Set heading bug - HDG (push PFD knob to set heading bug to current heading.) After Start Checklist add: “MFD ......................................ENT / TIS Page” after GPS line item. Set course - CRS (when in VLOC mode) add: “SBY ATTITUDE ............ PULL / RELEASE “ after NAVS line item. Set altitude bug and alerter - ALT Run Up Checklist “SUCTION GAUGE ..............................................................................N/A” Set V/S Bug - V/S Shutdown Terminate Checklist (do not use) add (final) item: Altimeter setting - BARO “SBY ATTITUDE ..............................................BLINKING or FLAGGED” (the STBY PWR warning light will blink for 1 minute when the battery master is selected off, then the unit automatically turns off and the red gyro warning flag appears. DO NOT press the SBY PWR button as it causes continuous operation of the gyro on its emergency battery. Exit the airplane with either a blinking LED or red flag.) NOTE: MULTI-FUNCTION DISPLAY (MFD) CDI needle indicates NAV source: green for VLOC / magenta for GPS. Revised 2015-06-02 GARMIN G500 QUICK REFERENCE continued... ADC Failure Electrical Failure AHRS Failure Heading Failure Indications - Complete loss of the Air Indication - In the event of a total loss of electrical Indications - Failure of the Attitude Indications - A complete Heading Data Computer (ADC) is indicated power, the G500 system will be inoperative / dark. and Heading Reference System (AHRS) Failure (magnetometer and GPS by a red X and yellow text over the The STBY PWR button on the standby attitude is indicated by a removal of the sky/ ground track failure) is indicated by airspeed, altimeter, vertical speed, indicator will begin blinking indicating it will turn off ground presentation, a red X across the digital heading presentation TAS and OAT displays. True airspeed in one minute. the Attitude Indicator, and a yellow being replaced with a red X and and wind calculations are also lost. Pilot Action - For attitude reference, press the “STBY “ATTITUDE FAIL” and “HDG” messages the compass rose digits being Pilot Action - Use standby airspeed PWR” button on the standby attitude indicator on the PFD. Rate-of-turn information removed. indicator and altimeter for speed while blinking to operate using its integral will not be available. Pilot Action - Use the magnetic and altitude data. There is no backup emergency battery. If the red warning flag appears Pilot Action - Use standby attitude compass and the GNS 430s for for the VSI, but known pitch attitudes on the standby attitude instrument face, the unit is indicator for attitude info and a heading information. using the attitude indicator, power powered off or inoperative and must not be used. combination of the magnetic compass settings, and airspeeds produce Use the standby airspeed, altimeter, compass, and and Garmin GNS 430 for heading. The consistent descent rates. GNS430 for remaining flight data. CDI will function normally..
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