Garmin GIA 63, Installation Manual

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GIA 63 Installation Manual 190-00303-05
Page 1-16 Rev. Y
TSO-C92c 1. Garmin was granted a deviation from TSO-C92c to use DO-160D Change 3 instead of DO-160C.
2. Garmin was granted a deviation from TSO-C92c to not include the version and levels of software
or the modification status of hardware in the appliance number.
TSO-C129a 1. Garmin was granted a deviation from TSO-C129a to use DO-160D Change 3 instead of DO-
160C.
2. Garmin was granted a deviation from TSO-C129a to eliminate the annunciation for pending CDI
scale change 3.0 NM from the FAF.
3. Garmin was granted a deviation from TSO-C129a involving the use of GPS calibrated altitude in
approach mode based on the enclosed TSO deviation request dated August 24, 1994 and the
approval letter dated November 29, 1994.
4. Garmin was granted a deviation from TSO-C129a to extend automatic CDI sensitivity changes to
non-approach mode navigation.
5. Garmin was granted a deviation from TSO-C129a to eliminate the requirement in (a)(3)(xi)1.b.ii to
“alert the pilot of the need to manually insert the barometric pressure”.
6. Garmin was granted a deviation from TSO-C129a to eliminate the requirement in (a)(3)(xv)4.b to
provide a “means to manually identify a satellite that is expected to be unavailable at the destination
(for scheduled maintenance as identified in FAA Notice to Airmen) shall be provided” for the RAIM
prediction process.
7. Garmin was granted a deviation from TSO-C129a to change the requirement in (a)(6)(iii) from
“The navigation data contains all 1’s or 0’s” to “All data bits in subframe 1, 2, or 3 are 0’s”.
8. Garmin was granted a deviation from TSO-C129a to change the requirement in paragraph
(a)(7)(ii) to match the WAAS TSO-C145a and DO-229 requirements for Power input testing.
ETSO-C129a 1. Garmin was granted a deviation from ED-72A 3.2.2.1.f (list item 3) and 3.2.2.4.j.4 to eliminate the
annunciation for pending CDI scale change 3.0 nm from the FAF.
2. Garmin was granted a deviation from ED-72A 3.2.2.4.j.3 to extend automatic CDI sensitivity
changes for approach mode navigation to non-approach mode navigation as well.
3. Garmin was granted a deviation from ED-72A 3.2.2.1.f (list item 4) and 3.2.2.3.e.4 and 3.2.2.4.j.2
to eliminate the requirement to alert the pilot of the need to manually insert the barometric pressure.
4. Garmin was granted a deviation from ED-72A 3.2.2.3.d.2 to eliminate the requirement to provide a
means to manually identify a satellite that is expected to be unavailable at the destination (for
scheduled maintenance as identified in FAA Notice to Airmen) for the RAIM prediction process.
5. Garmin was granted a deviation from ED-72A 3.1.4.1.c to change the requirement from
“the navigation data contains all 1’s or 0’s” to “all data bits in subframe 1,2, or 3 are 0’s”.
6. Garmin was granted a deviation from ED-72A 4.16.2 to eliminate the requirement for valid position
within 10 seconds of power interrupt for abnormal operating conditions power input tests. For
abnormal operating conditions power input tests, satellite acquisition time of 5 minutes applies.
TSO-C151b 1. Garmin was granted a deviation from TSO-C151b 4.a. to mark the unit with the serial number
instead of the date of manufacture.
Table 1-12. GIA 63 TSO/ETSO Deviations
TSO/ETSO Deviation