Garmin 80 Data List
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Apollo CNX80 STC Master Data ListGarmin AT2345 Turner Rd SE 27 October 2003Salem, OR 97302 Part #: 560-0987-00 Rev E Copyright 2003 Garmin AT, Inc. All Rights ReservedPage 6 of 72.4 Equipment ListAll equipment must have the Part Numbers and Software Versions contained in thefollowing table (or later FAA approved revisions or versions).Table 3 - System Equipment ListDescription Model No. Mfg. P/N Mfg. CommentWAAS/GPS/Nav/Com CNX80 430-6100-800-001 Garmin AT SW Ver. 1.1 or 1.2GPS Antenna A-33 590-1104AT-575-9Garmin ATAeroAntennaStandard antennaGPS Antenna A-34 590-1112AT-575-93Garmin ATAeroAntennaOptional “teardrop”footprintEquipment listed as equivalent in this document is equivalent with respect to functionalityof the Apollo CNX80 activated via this STC. It is the responsibility of those installing theequivalent equipment to verify that it is also acceptable for all other interfaces, devices, orintegration considerations, and that it is equivalent for any and all other airworthinessconsiderations.3 General Installation Requirements3.1 GeneralThe installation must be done in accordance with all applicable FARs. The installationshall conform to the data listed in Section 2.1 Data Required for Installation, withexception of special instructions as defined in Section 4 Special Installation Instructions,which shall have precedence over the dated listed in Section 2.1.3.2 MechanicalMechanical installation, wiring, cable bundling and routing, and connections to existingaircraft systems must conform to those specific instructions or requirements found in theSTC data. Those aspects of the STC where specific installation instructions orrequirements are not provided in the STC data, the installer shall conform to therecommended practices and procedures found in AC 43.13-2A, Chapter 2, RadioInstallations, and Chapter 3, Antenna Installations; AC 43.13-1B, Chapter 11, ElectricalSystems, Section 3, 4 and 7.3.3 HardwareHardware not supplied with the equipment, or otherwise specified in the appropriateinstallation manuals or other STC data (ie screws, nuts, tie wraps…. etc) shall be fromstandard aircraft hardware as described by AC 43.13-1B, Chapter 5, Aircraft Hardware. |
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