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shows the current turn rate. 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.
The G5 receives a GPS input via one of the following methods:
•
GPS antenna
•
GTN 6XX/7XX series navigator
•
GNS 4XXW/5XXW series navigator
The following functions are provided by the GPS input:
•
Ground Track
•
Ground Speed (GS)
The G5 installation is connected to the aircraft Pitot / Static system which provides the following
functions:
•
Secondary Airspeed indicator
•
Secondary Barometric altimeter
•
Secondary Vertical speed
•
Secondary Altimeter Barometric Setting
•
Secondary Altimeter
•
Secondary Altitude Display
•
Selected altitude setting, bug and visual altitude alerting
•
Secondary Vertical Speed Indicator
•
Vspeed references
2.2 Battery
The G5 has an external lithium-ion battery that provides up to 4 hours of emergency power.
Garmin G5 Electronic Flight Instrument Part 23 AML STC Maintenance Manual
Figure 2-2 G5 Battery
Page 3 of 18
190-01112-11
Rev. 1