Garmin GIA 63 Installation Manual
Also see for GIA 63: Installation manualInstallation manualInstallation manual
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Page 1-24 GIA 63 Installation ManualRevision T 190-00303-05The following information may be published in the approved AFM, AFMS, and/or POH provided thesystem is installed in accordance with AC 20-138A and is comprised of two TSO-C145a Class 3approved Garmin GIA 63W or GIA 63H units, two/three TSO-C146a Class 3 approved GarminGDU 1XXX Display Units, Garmin GA36 and GA37 antennas, and GPS software version 3.2 or laterapproved version:NOTEText contained in brackets “[ ]” is meant to serve as an example and will need to bemodified in order to reflect the actual installation.GARMIN GNSS (GPS/SBAS) NAVIGATION SYSTEM EQUIPMENT APPROVALSThe Garmin GNSS navigation system installed in this aircraft is a GPS system with a Satellite BasedAugmentation System (SBAS) comprised of [two TSO-C145a Class 3 approved Garmin GIA 63W orGIA 63H units, TSO-C146a Class 3 approved Garmin GDU 1XXX Display Units, Garmin GA 36 andGA 37 antennas, and GPS software version 3.2 or later approved version]. The Garmin GNSS navigationsystem in this aircraft is installed in accordance with AC 20-138A.The Garmin GNSS navigation system as installed in this aircraft complies with the requirements of AC20-138A and is approved for navigation using GPS and SBAS (within the coverage of a Satellite BasedAugmentation System complying with ICAO Annex 10) for IFR en route, terminal area, andnon-precision approach operations (including those approaches titled “GPS”, “or GPS”, and “RNAV(GPS)” approaches). The Garmin GNSS navigation system installed in this aircraft is approved forapproach procedures with vertical guidance including “LPV” and “LNAV/VNAV”, within the U.S.National Airspace System.The Garmin GNSS navigation system as installed in this aircraft complies with the equipmentrequirements of AC 90-105 and meets the equipment performance and functional requirements to conductRNP terminal departure and arrival procedures and RNP approach procedures without RF (radius to fix)legs. Part 91 subpart K, 121, 125, 129, and 135 operators require operational approval from the FAA.The Garmin GNSS navigation system as installed in this aircraft complies with the equipmentrequirements of AC 90-100A for RNAV 2 and RNAV 1 operations. In accordance with AC 90-100A,Part 91 operators (except subpart K) following the aircraft and training guidance in AC 90-100A areauthorized to fly RNAV 2 and RNAV 1 procedures. Part 91 subpart K, 121, 125, 129, and 135 operatorsrequire operational approval from the FAA.The Garmin GNSS navigation system as installed in this aircraft has been found to comply with therequirements for primary means of Class II navigation in oceanic and remote navigation (RNP-10)without time limitations in accordance with AC 20-138A and FAA Order 8400.12A. The Garmin GNSSnavigation system can be used without reliance on other long-range navigation systems. This does notconstitute an operational approval.The Garmin GNSS navigation system as installed in this aircraft has been found to comply with thenavigation requirements for primary means of Class II navigation in oceanic and remote navigation(RNP-4) in accordance with AC 20-138A and FAA Order 8400.33. The Garmin GNSS navigationsystem can be used without reliance on other long-range navigation systems. Additional equipment maybe required to obtain operational approval to utilize RNP-4 performance. This does not constitute anoperational approval.The Garmin GNSS navigation system as installed in this aircraft complies with the accuracy, integrity,and continuity of function, and contains the minimum system functions required for PRNAV operationsin accordance with JAA Administrative & Guidance Material Section One: General Part 3: TemporaryGuidance Leaflets, Leaflet No 10 (JAA TGL-10 Rev 1).DRAFT Rev T 11/12/2010 |
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