GIA 64 Installation/User Guide OEMs should obtain the most recent copy of the Installation Guide or Manual documents prior to equipment, configuration, installation and/or use.
Contents 1. Overview .............................................................................................................................................. 3 2. Physical Characteristics .................................................................................................................... 3 3. 2.1. Dimensions .................................................................................................................................. 3 2.2. Weight ...........................
1. Overview The GIA 64 series of line replaceable units (LRU) are a family of integrated avionics units (IAU) for use with a Garmin Integrated Flight Deck (GIFD). The GIA 64 provides the following functionality: • Interface capability to other GIFD system components using Ethernet (HSDB), RS-232, RS-485, RS-422, ARINC 429, and other interfaces. • Interface capability to third party equipment using RS-232, RS-485, RS-422, ARINC 429, and other interfaces.
General IO Interface Ethernet (HSDB) RS-232 RS-485/422 ARINC 429 (RX) ARINC 429 (TX) ARINC 429 (TX) / ARINC 717 (TX) CAN GPS PPS Output GPS ARINC 743 (TX) ARINC 708 (RX) Configurable Discrete Inputs Active High Discrete Inputs Active High Autopilot Disconnect Input Discrete Outputs Annunicators Superflags Analog Flight Director (Pitch/Roll) Inputs General Purpose DC Input General Purpose DC Output Analog Lateral CDI Outputs Analog Vertical CDI Outputs Configurable AC ARINC 407 (X/Y/Z) Inputs / DC SIN/COS In
3.1. General IO Considerations Implementation of available IO should take system and aircraft requirements in to account when using IO to interface to additional LRUs within the system. Connection and use of available configurable interfaces vary between model variants and system integration requirements. System and aircraft requirements should be considered prior to configuring any GIA 64 provided interfaces . 3.2.1. Ethernet The GIA 64 has a total of 3 Ethernet interfaces.
4.2. Cabling and Wiring Consideration Cabling and wiring must be installed in accordance with AC 43.13-1B CHG 1 Chapter 11, Sections 8 through 13. The following issues must be addressed: • Do not expose cabling and wiring to chafing • Avoid sharp bends in cabling and wiring harnesses • Make sure ample space is provided for cabling and wiring harnesses and connectors to allow connection and disconnection.
4.6.1. COM Antenna Location The GIA 64 COM antennas must be mounted as far as is practical from any protruding aircraft features such as engines or propellers.
GDL GTS GDL GSD GSD GDU GDU GDU GDU GTC GTC GIA GTC GTC GIA GSD GSD GWX 8. Unit Authorization 8.1. Transmitter Grant of Equipment Authorization CAUTION The operation of unapproved cellular telephones or other unapproved cellular devices aboard aircraft while airborne is prohibited by FCC rules.
Unapproved cellular telephones that are on, even in a monitoring state, can disrupt GPS performance. NOTE The FCC authorization for the COM Extended Range Option is for equipment certification purposes only; it does NOT constitute an authorization to operate the COM transmitter in the frequency range from 137.000 to 151.975 MHz in the United States (as described in 47 CFR 87.147(f)). Additional agency authorizations are required to operate the COM transmitter in these frequency bands.
