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1.6.4 GIA 63W TSO/ETSO Deviations
TSO/ETSO
TSO-C9c
1. Garmin was granted a deviation from TSO-C9c to use SAE AS 402B instead of AS-
402A.
2. Garmin was granted a deviation from TSO-C9c to use DO-160E instead of specified
environmental tests.
3. Garmin was granted a deviation from TSO-C9c subpart A (c), which requires marking
the weight of the unit on the unit. Garmin will provide this information in the installation
manual in lieu of marking on the serial tag. Garmin does not currently list the weight on
other avionics units.
4. Garmin was granted a deviation from SAE AS 402B paragraph 4.4.1 to limit autopilot
engagement to attitudes considered safe for the certified aircraft.
5. Garmin was granted a deviation from SAE AS 402B paragraph 4.3.2 to not provide
servo effort indications when the automatic pilot is not engaged.
ETSO-C9c
1. Garmin was granted a deviation from ETSO-C9c to use SAE AS-402B instead of AS-
402A.
2. Garmin was granted a deviation from ETSO-C9c to use DO-160E instead of the
specified environmental tests.
3. Garmin was granted a deviation from AS-402B paragraph 4.3.2 to not provide servo
effort indications when the automatic pilot is not engaged.
4. Garmin was granted a deviation from AS-402B paragraph 4.4.1 to limit autopilot
engagement to attitudes considered safe for the certified aircraft.
TSO-C34e
1. Garmin was granted a deviation from TSO-C34e to use DO-160E instead of DO-160B,
and DO-178B instead of DO-178A.
ETSO-2C34f 1. Garmin was granted a deviation from ETSO-2C34f to use DO-160E instead of DO-
160D.
TSO-C36e
1. Garmin was granted a deviation from TSO-C36e to use DO-160E instead of DO-160B,
and DO-178B instead of DO-178A.
GIA 63/GIA 63W Installation Manual
190-00303-05
Deviation
Page 1-17
Revision S
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