Garmin 0140000 AIRBORNE COMMUNICATIONS TRANSCEIVER User Manual coverrevS
Garmin International Inc AIRBORNE COMMUNICATIONS TRANSCEIVER coverrevS
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![Page 1-26 GIA 63/GIA 63W Installation Manual Revision S 190-00303-05 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: NOTE 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).](https://usermanual.wiki/Garmin/0140000/User-Guide-1366591-Page-35.png)
![GIA 63/GIA 63W Installation Manual Page 1-27 190-00303-05 Revision S The GNSS navigation system has [two ETSO-145 / TSO-C145a Class 3 approved Garmin GIA 63Ws, and ETSO-146 / TSO-C146a Class 3 approved Garmin GDU 1XXX Display Units]. The Garmin GNSS navigation system as installed in this aircraft complies with the equipment requirements for PRNAV and BRNAV operations in accordance with AC 90-96A and JAA TGL-10 Rev 1. This does not constitute an operational approval. Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) in accordance with AC 20-153 for database integrity, quality, and database management practices for the Navigation database. Pilots and operators can view the LOA status at www.garmin.com > Aviation Databases > Type 2 LOA Status. Navigation information is referenced to WGS-84 reference system. GARMIN GNSS (GPS/SBAS) NAVIGATION SYSTEM LIMITATIONS The pilot must confirm at system initialization that the Navigation database is current. Navigation database is expected to be current for the duration of the flight. If the AIRAC cycle will change during flight, the pilot must ensure the accuracy of navigation data, including suitability of navigation facilities used to define the routes and procedures for flight. If an amended chart affecting navigation data is published for the procedure, the database must not be used to conduct the procedure. GPS/SBAS based IFR enroute, oceanic, and terminal navigation is prohibited unless the pilot verifies and uses a valid, compatible, and current Navigation database or verifies each waypoint for accuracy by reference to current approved data. Discrepancies that invalidate a procedure must be reported to Garmin International. The affected procedure is prohibited from being flown using data from the Navigation database until a new Navigation database is installed in the aircraft and verified that the discrepancy has been corrected. Contact information to report Navigation database discrepancies can be found at www.garmin.com > Support > Contact Garmin Support > Aviation. Pilots and operators can view navigation data base alerts at www.garmin.com > In the Air > NavData Alerts. For flight planning purposes, in areas where SBAS coverage is not available, the pilot must check RAIM availability. Within the United States, RAIM availability can be determined using the Garmin WFDE Prediction program, [part number 006-A0154-01 (included in G1000 trainer software) version 3.00 or later approved version with GARMIN GA36 and GA37 antennas selected], or the FAA’s en route and terminal RAIM prediction website: www.raimprediction.net, or by contacting a Flight Service Station. Within Europe, RAIM availability can be determined using the Garmin WFDE Prediction program or Europe’s AUGER GPS RAIM Prediction Tool at http://augur.ecacnav.com/augur/app/home. For other areas, use the Garmin WFDE Prediction program. This requirement is not necessary if SBAS coverage is confirmed to be available along the entire route of flight. The route planning and WFDE prediction program may be downloaded from the Garmin website on the internet. For information on using the WFDE Prediction Program, refer to Garmin WAAS FDE Prediction Program, part number 190-00643-01, ‘WFDE Prediction Program Instructions’. For flight planning purposes, operations within the U.S. National Airspace System on RNP and RNAV procedures when SBAS signals are not available, the availability of GPS integrity RAIM shall be confirmed for the intended route of flight. In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended route of flight, the flight should be delayed, canceled, or re-routed on a track where RAIM requirements can be met. For flight planning purposes for operations within European B-RNAV and P-RNAV airspace, if more than one satellite is scheduled to be out of service, then the availability of GPS integrity RAIM shall be](https://usermanual.wiki/Garmin/0140000/User-Guide-1366591-Page-36.png)
![Page 1-28 GIA 63/GIA 63W Installation Manual Revision S 190-00303-05 confirmed for the intended flight (route and time). In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended flight, the flight should be delayed, canceled, or re-routed on a track where RAIM requirements can be met. For flight planning purposes, operations where the route requires Class II navigation the aircraft’s operator or pilot-in-command must use the Garmin WFDE Prediction program to demonstrate that there are no outages on the specified route that would prevent the Garmin GNSS navigation system to provide primary means of Class II navigation in oceanic and remote areas of operation that requires (RNP-10 or RNP-4) capability. If the Garmin WFDE Prediction program indicates fault exclusion (FDE) availability will exceed 34 minutes in accordance with FAA Order 8400.12A for RNP-10 requirements, or 25 minutes in accordance with FAA Order 8400.33 for RNP-4 requirements, then the operation must be rescheduled when FDE is available. Both Garmin GPS navigation receivers must be operating and providing GPS navigation guidance to their respective PFD for operations requiring RNP-4 performance. North Atlantic (NAT) Minimum Navigational Performance Specifications (MNPS) Airspace operations per AC 91-49 and AC 120-33 require both GPS/SBAS receivers to be operating and receiving usable signals except for routes requiring only one Long Range Navigation sensor. Each display computes an independent navigation solution based on the on-side GPS sensor. However, either display will automatically revert to the cross-side sensor if the on-side sensor fails or if the cross-side sensor is determined to be more accurate. [On G1000 installations a “BOTH ON GPS1” or “BOTH ON GPS2” message does not necessarily mean that one GPS has failed. Refer to the MFD AUX-GPS STATUS page to determine the state of the unused GPS]. Whenever possible, RNP and RNAV routes including Standard Instrument Departures (SIDs) and Obstacle Departure Procedures (ODPs), Standard Terminal Arrival (STAR), and enroute RNAV “Q” and RNAV “T” routes should be loaded into the flight plan from the database in their entirety, rather than loading route waypoints from the database into the flight plan individually. Selecting and inserting individual named fixes from the database is permitted, provided all fixes along the published route to be flown are inserted. Manual entry of waypoints using latitude/longitude or place/bearing is prohibited. “GPS”, “or GPS”, and “RNAV (GPS)” instrument approaches using the Garmin navigation systems are prohibited unless the pilot verifies and uses the current Navigation database. GPS based instrument approaches must be flown in accordance with an approved instrument approach procedure that is loaded from the Navigation database. Not all published Instrument Approach Procedures (IAP) are in the Navigation database. Pilots planning on flying an RNAV instrument approach must ensure that the Navigation database contains the planned RNAV Instrument Approach Procedure and that approach procedure must be loaded from the Navigation database into the FMS flight plan by its name. IFR non-precision approach approval using the GPS/SBAS sensor is limited to published approaches within the U.S. National Airspace System. Approaches to airports in other airspace are not approved unless authorized by the appropriate governing authority. The navigation equipment required to join and fly an instrument approach procedure is indicated by the title of the procedure and notes on the IAP chart. Use of the Garmin GPS/SBAS receivers to provide navigation guidance during the final approach segment of an ILS, LOC, LOC-BC, LDA, SDF, MLS or any other type of approach not approved for “or GPS” navigation is prohibited. When using the Garmin VOR/LOC/GS receivers to fly the final approach segment, VOR/LOC/GS navigation data must be selected and presented on the CDI of the pilot flying.](https://usermanual.wiki/Garmin/0140000/User-Guide-1366591-Page-37.png)
![Page 2-2 GIA 63/GIA 63W Installation Manual Revision S 190-00303-05 2.1.3 Additional Equipment Required The following installation accessories are required but not provided: COM Antenna: Shall meet TSO-C37(), C38(), and C-169()*. Broad band, 50 Ω, vertically polarized with coaxial cable GPS Antenna: GIA 63 (Non-WAAS) shall meet TSO-C129a. TSO-C144 antennas can also meet TSO-C129a requirements for the GIA 63 (Refer to Section 2.1.3.1). GIA 63W (WAAS) shall meet TSO-C144 and additional system requirements specified by TSO-C145a. Refer to Section 2.1.3.2 for approved antennas VOR/LOC Antenna: Shall meet TSO-C40() and C36(). Broad band, 50 Ω, horizontally polarized with coaxial cable Glideslope Antenna: Shall meet TSO-C34(). Broad band, 50 Ω, horizontally polarized with coaxial cable or low-loss splitter used with the VOR/LOC antenna Headphones: 500 Ω nominal impedance Microphone: Low impedance, carbon or dynamic, with transistorized pre-amp Hardware: #6-32 x 100°Flathead SS Screw [(MS24693, AN507R or other approved fastener) (4 ea.)] for horizontal mounting of the standalone rack. Hardware: #8-32 Panhead Machine Screw [(MS35206, AN526 or other approved fastener) (4 ea.)] for vertical mounting of the standalone rack. * GIA 63W only 2.1.3.1 Required Antennas for the GIA 63 Antennas used with the GIA 63 (non-WAAS) must meet the antenna specifications shown in Section 2.6. In addition, TSO-C144 antennas can also meet TSO-C129a requirements for the GIA 63 (non-WAAS) if their additional gain (which is about 16dB at 1.5 GHz for antennas produced by Garmin) is offset by added attenuation in-line with the GIA 63 (non-WAAS). If an in-line attenuator is used, it must pass DC current (40 mA max at 4.6 VDC) which is provided from the GPS receiver to the antenna pre-amplifier.](https://usermanual.wiki/Garmin/0140000/User-Guide-1366591-Page-43.png)
![GIA 63/GIA 63W Installation Manual Page 2-3 190-00303-05 Revision S 2.1.3.2 Required WAAS Antennas for the GIA 63W The following is a list of TSO-C144 antennas that allow the GIA 63W with GPS software version 3.00 or later to meet TSO-C145a requirements without requiring the operational limitations specified in Section 1.6.5 of this manual: Model Mount Style Conn Type SATCOM Compatible [3] Mfr Antenna Part Number Garmin Order Number Additional Requirements Aero Antenna AT575-93GW-TNCF-000-RG-27-NM GA 35 GPS WAAS Antenna [6] Screw Mount, Teardrop Footprint [2] TNC Yes Garmin 013-00235-00 013-00235-00 Aero Antenna AT575-326GW-TNCF-000-RG-27-NM GA 36 GPS WAAS Antenna [6] Screw Mount, ARINC 743 Footprint TNC Yes Garmin 013-00244-00 013-00244-00 Aero Antenna AT2300-126GW-TNCF-000-RG-27-NM GA 37 FIS/WAAS Antenna [6] Screw Mount, ARINC 743 Footprint TNC Yes Garmin 013-00245-00 013-00245-00 Comant 2580-200 WAAS and COM Antenna [6] [8] CI 2580-200 Comant 2580-410 FIS/WAAS /COM Antenna [6] [8] Screw Mount, Teardrop Footprint [2] BNC TNC [5] Yes Comant CI 2580-410 N/A Comant 428-200 WAAS Antenna [6] [8] CI 428-200 Comant 428-410 FIS/WAAS Antenna [6] [8] Screw Mount, ARINC 743 Footprint TNC Yes Comant CI 428-410 N/A Comant 2728-200 WAAS and COM Antenna [6] [8] CI 2728-200 Comant 2728-410 FIS/WAAS /COM Antenna [6] [8] Screw Mount, Teardrop Footprint [7] BNC TNC [5] Yes Comant CI 2728-410 N/A None](https://usermanual.wiki/Garmin/0140000/User-Guide-1366591-Page-44.png)
![Page 2-4 GIA 63/GIA 63W Installation Manual Revision S 190-00303-05 The following is a list of known TSO-C144 antennas that allow the GIA 63W with any version of GPS software version to meet TSO-C145a requirements with the operational limitations specified in Section 1.6.5 of this manual: Model Mount Style Conn Type SATCOM Compatible [3] Mfr Antenna Part Number Garmin Order Number Additional Requirements Aero Antenna AT575-93W-TNCF-000-05-26-NM A-34 GPS WAAS Antenna Screw Mount, Teardrop Footprint [2] TNC Yes Garmin AT 590-1112 013-00113-00 GA56A GPS WAAS Antenna Screw Mount, ARINC 743 Footprint BNC No Garmin 011-01154-00 010-10599-00 GA56W GPS WAAS Antenna Stud Mount, Teardrop Footprint [1] BNC No Garmin 011-01111-00 010-10561-01 GA57 GPS WAAS and FIS Antenna Screw Mount, ARINC 743 Footprint BNC TNC [4] No Garmin 011-01032-00 010-10604-00 The operational limitation described in Section 1.6.5 requires use of 006-A0154-01 as the Prediction Program in conjunction with these antennas. [1] Same footprint and mounting hole pattern as GA 56. [2] Same mounting hole pattern as the GA 56, but has a physically larger footprint. [3] SATCOM compatibility requirements are as specified by RTCA/DO-229C Section 2.5.6.1, Section 2.5.8.2, Appendix C.2.1, and Appendix C.2.2. [4] The WAAS GPS antenna connector is a BNC type. The XM antenna connector is a TNC type. [5] The WAAS GPS antenna connector (and XM antenna connector where applicable) is TNC type. The VHF COM antenna connector is BNC type. [6] Not approved for use with the GIA 63 (non-WAAS) since max DC current specification exceeds 40 mA. [7] Larger footprint and mounting hole pattern than GA 56, GA 35 or CI 2580. [8] It is the installer’s responsibility to ensure the antenna complies with Antenna Minimum Performance Specification for Garmin’s GPS/WAAS Receiver System Antenna (004-00287-00) by communicating the requirement to the supplier and obtaining a certificate of compliance to 004-00287-00 from the supplier. An antenna that complies only with TSO-C144 requirements is not adequate for this installation. Other TSO-C144 antennas may meet the installation requirements of the GIA 63W. Contact Garmin to ensure compatibility and applicable operation limitations before beginning the installation.](https://usermanual.wiki/Garmin/0140000/User-Guide-1366591-Page-45.png)
![APPENDIX B OUTLINE & INSTALLATION DRAWINGS GIA 63/GIA 63W Installation Manual Page B-1 (Page B-2 blank) 190-00303-05 Revision S 1.8 462.9 744.7 12014X NOTE 3.480 12.19TYP9.58TYP.37794.673.727TYP.44 11.1TYPMODULAR INSTALLATION14X NOTE 312.19TYP175.26TYP6.90011.1TYP.44.4803.76 95.414X NOTE 3P606P601P603COMAIRGPS P605P602NAVG/SP604MOUNTING HOLE FOR #6 FLAT HEAD 100 CSK SCREW (42 PLCS).3.NOTES: UNLESS OTHERWISE SPECIFIEDDIMENSIONS: INCHES[mm]1. DIMENSIONS SHOWN ARE FOR REFERENCE ONLY.2.10.00 253.9160.06.30184.47.26210.58.29 223.18.78 232.99.174X6X.20 5.0 Figure B-1. GIA 63(W) Modular Installation Outline Drawing](https://usermanual.wiki/Garmin/0140000/User-Guide-1366591-Page-98.png)
![APPENDIX B OUTLINE & INSTALLATION DRAWINGS GIA 63/GIA 63W Installation Manual Page B-5 (Page B-6 blank) 190-00303-05 Revision S 3.50 88.94.42 112.31.98 50.3 4X NOTE 3 2X 1.625 41.282X 4.500 114.302X 5.25 133.42X .56 14.2NOTES: UNLESS OTHERWISE SPECIFIEDDIMENSIONS: INCHES[mm]1. DIMENSIONS SHOWN ARE FOR REFERENCE ONLY.2. MOUNTING HOLE FOR #6 FLAT HEAD 100 CSK SCREW (8 PLCS).3. MOUNTING HOLE FOR #8 PAN HEAD SCREW (4 PLCS).4.STANDALONE INSTALLATION4X NOTE 42X .56 14.32X 2.75 69.852X 1.60 40.62X 4.458 113.23GPSAIRCOMP603P601P604 P606G/SNAVP602P6054X NOTE 32X 6.91 175.53X 6.42 163.12X 5.250 133.352X .56 14.26X 10.06 255.42X 8.84 224.62X 1.13 28.62X 4.500 114.304X 9.23 234.38.35 212.0.14 3.52X 3.88 98.5 Figure B-3. GIA 63(W) Standalone Installation Outline Drawing](https://usermanual.wiki/Garmin/0140000/User-Guide-1366591-Page-100.png)
