Garmin GIA 63 Installation Manual page 42

1.6.7 GIA 63W Updated NAV/COM and GIA 63H TSO/ETSO Deviations
Table 1-17. GIA 63W Updated NAV/COM and GIA 63H TSO/ETSO Deviations
TSO/ETSO
TSO-C9c
ETSO-C9c
TSO-C34e
ETSO-2C34f
TSO-C36e
ETSO-2C36f
ETSO-2C37e
ETSO-2C38e
TSO-C40c
ETSO-2C40c
TSO-C52b
ETSO-C52b
TSO-C54
GIA 63 Installation Manual
Page 1-32
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.
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.
1. Garmin was granted a deviation from TSO-C34e to use DO-160E instead of DO-160B, and
DO-178B instead of DO-178A
1. Garmin was granted a deviation from ETSO-2C34f to use DO-160E instead of DO-160D.
1. Garmin was granted a deviation from TSO-C36e to use DO-160E instead of DO-160B, and
DO-178B instead of DO-178A.
1. Garmin was granted a deviation from ETSO-2C36f to use DO-160E instead of DO-160D.
2. Garmin was granted a deviation from ETSO-2C36f to use ED-46B amendment 2 in addition to ED
46B.
1. Garmin was granted a deviation from ETSO-2C37e to use DO-160E instead of DO-160D.
2. Garmin was granted a deviation from ETSO-2C37e to use ED-23B amendment 3 in addition to
ED-23B.
1. Garmin was granted a deviation from ETSO-2C38e to use DO-160E instead of DO-160D.
2. Garmin was granted a deviation from ETSO-2C38e to use ED-23B amendment 3 in addition to
ED-23B.
1. Garmin was granted a deviation from TSO-C40c to use DO-160E instead of DO-160B, and
DO-178B instead of DO-178A.
1. Garmin was granted a deviation from ETSO-2C40c to use DO-160E instead of DO-160D.
2. Garmin was granted a deviation from ED-22B paragraph 5.2.9 to have a deflection response of
0.5 to 2.7 seconds instead of 0.5 to 2 seconds.
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-160E instead of DO-160C. The
justification for this deviation is to use the latest accepted environmental standards.
1. Garmin was granted a deviation from ETSO-C52b to use DO-160E instead of DO-160D.
2. Garmin was granted a deviation from AS-8008 paragraph 3.6 to limit flight director operation to
attitudes considered safe for the certified aircraft.
1. Garmin was granted a deviation from TSO-C54 to use RTCA DO-160E instead of SAE AS 403A.
Deviation
190-00303-05
Rev. Y