Piper CHEROKEE CRUISER PA-28-140, Information Manual, Page: 195 / 212

190-01112-13 Rev. 5 AFMS, Garmin G5 AML STC
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SECTION 1 – GENERAL
The G5 Electronic Flight Instrument can display the following information to the pilot depending on the installation
and location of the G5 instrument.
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Primary attitude
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Primary slip and turn rate information
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Primary heading
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Secondary airspeed
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Secondary altimeter
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Secondary ground track
When installed in place of the attitude indicator, the primary function of the G5 is to provide attitude information to
the pilot. When installed in place of the rate of turn indicator, the primary function of the G5 is to provide turn
rate and slip ball information to the pilot. When installed in place of the directional gyro, the primary function of
the G5 is to provide directional information to the pilot.
NOTE:
The pilot is reminded to perform appropriate flight and navigation instrument cross checks for the
type of operation being conducted.
In case of a loss of aircraft electrical power, a backup battery (optional when installed as a DG/HSI) sustains the
G5 Electronic Flight Instrument for up to four hours.
An optional GAD 29B may be installed to provide course and heading datum to an autopilot based on the data
selected for display on the HSI.