Apollo CNX80 STC Master Data List
Garmin AT
2345 Turner Rd SE
27 October 2003
Salem, OR 97302
Part #: 560-0987-00 Rev E
Copyright 2003 Garmin AT, Inc. All Rights Reserved
Page 6 of 7
2.4
Equipment List
All equipment must have the Part Numbers and Software Versions contained in the
following table (or later FAA approved revisions or versions).
Table 3 - System Equipment List
Description
Model No.
Mfg. P/N
Mfg.
Comment
WAAS/GPS/Nav/Com CNX80
430-6100-800-001
Garmin AT
SW Ver. 1.1 or 1.2
GPS Antenna
A-33
590-1104
AT-575-9
Garmin AT
AeroAntenna
Standard antenna
GPS Antenna
A-34
590-1112
AT-575-93
Garmin AT
AeroAntenna
Optional “teardrop”
footprint
Equipment listed as equivalent in this document is equivalent with respect to functionality
of the Apollo CNX80 activated via this STC. It is the responsibility of those installing the
equivalent equipment to verify that it is also acceptable for all other interfaces, devices, or
integration considerations, and that it is equivalent for any and all other airworthiness
considerations.
3
General Installation Requirements
3.1
General
The installation must be done in accordance with all applicable FARs. The installation
shall conform to the data listed in Section 2.1 Data Required for Installation, with
exception 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
Mechanical
Mechanical installation, wiring, cable bundling and routing, and connections to existing
aircraft systems must conform to those specific instructions or requirements found in the
STC data. Those aspects of the STC where specific installation instructions or
requirements are not provided in the STC data, the installer shall conform to the
recommended practices and procedures found in AC 43.13-2A, Chapter 2, Radio
Installations, and Chapter 3, Antenna Installations; AC 43.13-1B, Chapter 11, Electrical
Systems, Section 3, 4 and 7.
3.3
Hardware
Hardware not supplied with the equipment, or otherwise specified in the appropriate
installation manuals or other STC data (ie screws, nuts, tie wraps…. etc) shall be from
standard aircraft hardware as described by AC 43.13-1B, Chapter 5, Aircraft Hardware.
