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The following information may be published in the approved AFM, AFMS, and/or POH provided the
system is installed in accordance with AC 20-138A and is comprised of two TSO-C145a Class 3
approved Garmin GIA 63Ws, two/three TSO-C146a Class 3 approved Garmin GDU 1XXX Display
Units, Garmin GA36 and GA37 antennas, and GPS software version 3.2 or later approved version:
Text contained in brackets "[ ]" is meant to serve as an example and will need to be
modified in order to reflect the actual installation.
GARMIN GNSS (GPS/SBAS) NAVIGATION SYSTEM EQUIPMENT APPROVALS
The Garmin GNSS navigation system installed in this aircraft is a GPS system with a Satellite Based
Augmentation System (SBAS) comprised of [two TSO-C145a Class 3 approved Garmin GIA 63Ws,
TSO-C146a Class 3 approved Garmin GDU 1XXX Display Units, Garmin GA36 and GA37 antennas,
and GPS software version 3.2 or later approved version]. The Garmin GNSS navigation system 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 AC
20-138A and is approved for navigation using GPS and SBAS (within the coverage of a Satellite Based
Augmentation System complying with ICAO Annex 10) for IFR en route, terminal area, and
non-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 for
approach 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 equipment
requirements of AC 90-105 and meets the equipment performance and functional requirements to conduct
RNP 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 equipment
requirements 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 are
authorized to fly RNAV 2 and RNAV 1 procedures. 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 has been found to comply with the
requirements 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 GNSS
navigation system can be used without reliance on other long-range navigation systems. This does not
constitute an operational approval.
The Garmin GNSS navigation system as installed in this aircraft has been found to comply with the
navigation 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 navigation
system can be used without reliance on other long-range navigation systems. Additional equipment may
be required to obtain operational approval to utilize RNP-4 performance. This does not constitute an
operational 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 operations
in accordance with JAA Administrative & Guidance Material Section One: General Part 3: Temporary
Guidance Leaflets, Leaflet No 10 (JAA TGL-10 Rev 1).
Page 1-26
Revision S
NOTE
GIA 63/GIA 63W Installation Manual
190-00303-05
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