Garmin GIA 63 Installation Manual

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GIA 63 Installation Manual 190-00303-05Page 1-32 Rev. Y1.6.7 GIA 63W Updated NAV/COM and GIA 63H TSO/ETSO DeviationsTable 1-17. GIA 63W Updated NAV/COM and GIA 63H TSO/ETSO DeviationsTSO/ETSO DeviationTSO-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 specifiedenvironmental tests.3. Garmin was granted a deviation from TSO-C9c subpart A (c), which requires marking the weightof the unit on the unit. Garmin will provide this information in the installation manual in lieu of markingon 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 engagementto 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 effortindications 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 specifiedenvironmental tests.3. Garmin was granted a deviation from AS-402B paragraph 4.3.2 to not provide servo effortindications when the automatic pilot is not engaged.4. Garmin was granted a deviation from AS-402B paragraph 4.4.1 to limit autopilot engagement toattitudes 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, andDO-178B instead of DO-178AETSO-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, andDO-178B instead of DO-178A.ETSO-2C36f 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 ED46B.ETSO-2C37e 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 toED-23B.ETSO-2C38e 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 toED-23B.TSO-C40c 1. Garmin was granted a deviation from TSO-C40c to use DO-160E instead of DO-160B, andDO-178B instead of DO-178A.ETSO-2C40c 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 of0.5 to 2.7 seconds instead of 0.5 to 2 seconds.TSO-C52b 1. Garmin was granted a deviation from SAE AS 8008 paragraph 3.6 to limit flight directoroperation 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. Thejustification for this deviation is to use the latest accepted environmental standards.ETSO-C52b 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 toattitudes considered safe for the certified aircraft.TSO-C54 1. Garmin was granted a deviation from TSO-C54 to use RTCA DO-160E instead of SAE AS 403A.