Garmin GIA 63 Installation Manual page 25

1.6.2 GIA 63 TSO/ETSO Deviations
TSO/ETSO
TSO-C9c
ETSO-C9c
TSO-C34e
TSO-C36e
TSO-C37d
TSO-C38d
TSO-C40c
TSO-C52b
ETSO-C52b
190-00303-05
Rev. Y
Table 1-12. GIA 63 TSO/ETSO Deviations
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-160D 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.
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-160D 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.
1. Garmin was granted a deviation from TSO-C34e to use DO-160D Change 3 instead of DO-160B,
and DO-178B instead of DO-178A.
1. Garmin was granted a deviation from TSO-C36e to use DO-160D Change 3 instead of DO-160B,
and DO-178B instead of DO-178A.
1. Garmin was granted a deviation from TSO-C37d to use DO-160D Change 3 instead of DO-160B,
and DO-178B instead of DO-178A.
2. Garmin was granted a deviation from TSO-C37d paragraph (a)(1) to allow using RTCA document
DO-186a Change 2 instead of RTCA document DO-186 to specify minimum performance standards.
3. Garmin was granted a deviation from TSO-C37d by allowing a 6dB reduction of transmitter power
during the Normal Operating Conditions - Emergency Operation Voltage as described in RTCA
document DO-186a paragraph 2.5.13.1 and RTCA document DO-160C paragraph 16.5.2.1.
4. Garmin was granted a deviation from TSO-C37d paragraph (a)(5) to allow 8.33 kHz spacing in
addition to the 25 kHz spacing.
5. Garmin was granted a deviation from TSO-C37d paragraph (b)(1) to allow the marking to call out
8.33 kHz spacing in addition to the 25 kHz spacing.
1. Garmin was granted a deviation from TSO-C38d to use DO-160D Change 3 instead of DO-160B,
and DO-178B instead of DO-178A.
2. Garmin was granted a deviation from TSO-C38d paragraph (a)(1) to allow using RTCA document
DO-186a Change 2 instead of RTCA document DO-186 to specify minimum performance standards.
3. Garmin was granted a deviation from TSO-C38d paragraph (a)(5) to allow 8.33 kHz spacing in
addition to the 25 kHz spacing.
1. Garmin was granted a deviation from TSO-C40c to use DO-160D Change 3 instead of DO-160B,
and DO-178B instead of DO-178A.
1. Garmin was granted a deviation from SAE AS 8008 paragraph 3.6 to limit flight director operation
to attitudes considered safe for the certified aircraft.
2. Garmin was granted a deviation from TSO-C52b to use DO-160D instead of DO-160C.
1. Garmin was granted a deviation from AS-8008 paragraph 3.6 to limit flight director operation to
attitudes considered safe for the certified aircraft.
Deviation
GIA 63 Installation Manual
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