Page 1
Apollo CNX80 STC Master Data List
Garmin AT
2345 Turner Rd SE 27 October 2003
Salem, OR 97302 Part #: 560-0987-00 Rev E
Apollo CNX80
Master Data List
Part Number: 560-0987-00
Document Revision: E
27 October 2003
Garmin AT, Inc.
2345 Turner Rd SE
Salem, OR 97302 USA
Phone (503) 581-8101
FAX (503) 364-2138
APOLLO
Garmin AT
is a registered trademark of Garmin AT, Inc.
TM
is a trademark of Garmin Ltd. or its subsidiaries.
Printed in the USA
Copyright 2003 Garmin AT, Inc. All Rights Reserved
Page 1 of 7
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Apollo CNX80 STC Master Data List
Garmin AT
2345 Turner Rd SE 27 October 2003
Salem, OR 97302 Part #: 560-0987-00 Rev E
Revision Log
Rev Date Description EN By
-- 23-Apr-03 Original Release 7625 dfs
A 30-May-03 Revised document revisions in Table 1 and Table 2 to reflect updated
documents.
B 5-Jun-03 Changed revision status of AFM and added A33/A34 installation guides. 7659 dfs
C 19-Jun-03 Revised document revisions to reflect updated documents and added new
documents to Table 1 and Table 2.
D 27-Jun-03 Update document revisions (Table 1, Table 2) 7662 mak
E 27-Oct-03 Update documents for company name and v1.2 application software
(Table 1).
Title:
Prepared By:
Approved By:
Approved By:
Garmin AT, Inc.
Cage Code
0XCJ6
Apollo CNX80 STC Master Data List
Daniel Schmidt
Chris Schulte
Chris Schulte, CNX80 Project Manager (approval signature on file)
Marv A. Kumley
Marv Kumley, Sr. Systems Eng. (approval signature on file)
P. O. Box 13549
Salem, Oregon USA
Number:
Date:
Date:
Date:
560-0987-00
4/23/03
4/24/03
4/24/03
7654 dfs
7662 dfs
7729 mak
Copyright 2003 Garmin AT, Inc. All Rights Reserved
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Apollo CNX80 STC Master Data List
Garmin AT
2345 Turner Rd SE 27 October 2003
Salem, OR 97302 Part #: 560-0987-00 Rev E
Table of Contents
1 INTRODUCTION...............................................................................................................................................4
1.1 PURPOSE.............................................................................................................................................................4
1.2 SCOPE.................................................................................................................................................................4
1.3 STC INCLUDES APPROVED MODEL LIST.............................................................................................................4
2 DATA AND EQUIPMENT LIST REQUIRED FOR INSTALLATION.......................................................4
2.1 DATA REQUIRED FOR INSTALLATION .................................................................................................................4
2.1.1 Apollo CNX80 Installation Data ...............................................................................................................4
2.1.2 Continued Airworthiness...........................................................................................................................5
2.2 RELATED DATA (SUBSTANTIATING DATA)........................................................................................................5
2.3 REFERENCE DOCUMENTS ...................................................................................................................................5
2.4 EQUIPMENT LIST ................................................................................................................................................6
3 GENERAL INSTALLATION REQUIREMENTS..........................................................................................6
3.1 GENERAL............................................................................................................................................................6
3.2 MECHANICAL .....................................................................................................................................................6
3.3 HARDWARE ........................................................................................................................................................6
3.4 WIRING ..............................................................................................................................................................7
3.5 CIRCUIT PROTECTION.........................................................................................................................................7
3.6 ELECTRICAL LOAD ANALYSIS ............................................................................................................................7
4 SPECIAL INSTALLATION INSTRUCTIONS...............................................................................................7
5 ADDITIONAL SYSTEM NOTES .....................................................................................................................7
Copyright 2003 Garmin AT, Inc. All Rights Reserved
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Apollo CNX80 STC Master Data List
Garmin AT
2345 Turner Rd SE 27 October 2003
Salem, OR 97302 Part #: 560-0987-00 Rev E
1 Introduction
1.1 Purpose
The purpose of this document is to list the data required to support STC installation of the
Garmin AT Apollo CNX80 in accordance with STC requirements, and to list other data
associated with the STC which is not required for installation.
1.2 Scope
This document applies to the installation of the Apollo CNX80 when installed to the
Approved Model List as defined in the STC. This document includes general installation
requirements, special installation instructions, and it provides an index of STC data
including both data required for installation and data associated with the STC, but not
required for installation.
1.3 STC includes Approved Model List
The STC includes an approved model list that should be consulted for applicability to each
installation. If the installation is covered under the STC, then the approved AFM can be
directly used for that installation. The installer should complete page 1 of the AFM (add
make/model, registration number and serial number) and include it with the aircraft’s
existing flight manual.
2 Data and Equipment List Required for Installation
2.1 Data Required for Installation
2.1.1 Apollo CNX80 Installation Data
All documents listed in Table 1 are required for installation purposes and must be of the
version listed or later FAA approved revisions.
Table 1 - STC Data
Doc No. Rev Description
560-0987-00 E Apollo CNX80 Master Data List (this document)
560-0985-00 E Apollo CNX80 AFM Supplement
560-0986-00 D Apollo CNX80 Instructions for Continued Airworthiness
560-0982-00 E Apollo CNX80 Installation Manual
560-0984-00 C Apollo CNX80 Pilot’s Guide
560-0949-01 B A33 GPS Antenna Installation Guide
560-5047-00 B A34 GPS Antenna Installation Guide
Copyright 2003 Garmin AT, Inc. All Rights Reserved
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Apollo CNX80 STC Master Data List
Garmin AT
2345 Turner Rd SE 27 October 2003
Salem, OR 97302 Part #: 560-0987-00 Rev E
2.1.2 Continued Airworthiness
Instructions for continued airworthiness are found in Garmin AT document number
560-0986-00 Instructions for Continued Airworthiness.
2.2 Related Data (Substantiating Data)
The documents listed in Table 2, or later FAA approved revisions, contain information
related to this STC but are not required for follow-on installations.
Table 2 - Substantiating Data
Doc No. Rev Description
424-2014-800 -- Apollo CNX80 Installation kit
PD3104 B Apollo CNX80 System Certification Plan
PD2248 D Apollo CNX80 STC System Accomplishment Summary
PD3105 -- Apollo CNX80 Plan Software Aspects of Certification
PD2215 -- Apollo CNX80 Plan for PLD Aspects for Certification
PD2249 A Apollo CNX80 System Safety Assessment
PD2212 A Apollo CNX80 Functional Hazard Assessment
PD2267 -- Process for the Acceptance for Aircraft on the CNX STC AML
PD2213 -- Apollo CNX80 Ground & Flight Test Plan
PD3108 A Apollo CNX80 Environmental Test Report Summary
PD2106 A Flight Test Report for Motorola Oncore GPS and UPSAT WAAS GPS
Sensor
2.3 Reference Documents
The following documents are used as reference for the installation.
• FAA AC 43.13-1B, Acceptable Methods, Techniques, and Practices - Aircraft
Inspection and Repair
• FAA AC 43.13-2A, Acceptable Methods, Techniques, and Practices - Aircraft
Alterations
• FAA AC 20-138A (final draft) dated 02/01/2003, Airworthiness approval of Global
Navigation Satellite System (GNSS) Equipment
Copyright 2003 Garmin AT, Inc. All Rights Reserved
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Apollo CNX80 STC Master Data List
Garmin AT
2345 Turner Rd SE 27 October 2003
Salem, OR 97302 Part #: 560-0987-00 Rev E
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
GPS Antenna A-34 590-1112
AT-575-93
Garmin AT
AeroAntenna
Garmin AT
AeroAntenna
Standard antenna
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.
Copyright 2003 Garmin AT, Inc. All Rights Reserved
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Apollo CNX80 STC Master Data List
Garmin AT
2345 Turner Rd SE 27 October 2003
Salem, OR 97302 Part #: 560-0987-00 Rev E
3.4 Wiring
All wire used in the installation shall be of appropriate standard aircraft quality grade and
size as described in AC 43.13-1B, Chapter 11, Sections 5-20.
3.5 Circuit Protection
All circuits shall be protected in accordance with AC 43.13-1B, Chapter 11, Section 4,
Circuit Protection Devices.
3.6 Electrical Load Analysis
An electrical load analysis shall be performed on each aircraft, as described in AC 43.131B, Chapter 11 Section 3. The document P/N 560-0982-00 CNX80 Installation Manual
provides specifications on the CNX80 power requirements.
4 Special Installation Instructions
None
5 Additional System Notes
No other system notes.
Copyright 2003 Garmin AT, Inc. All Rights Reserved
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