Important safety and product information (60 pages)
Summary of Contents for Garmin 80
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Apollo CNX80 STC Master Data List Garmin AT 2345 Turner Rd SE Salem, OR 97302 APOLLO Garmin AT Copyright 2003 Garmin AT, Inc. All Rights Reserved Apollo CNX80 Master Data List Part Number: 560-0987-00 Document Revision: E 27 October 2003 Garmin AT, Inc.
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Chris Schulte, CNX80 Project Manager (approval signature on file) Approved By: Marv A. Kumley Marv Kumley, Sr. Systems Eng. (approval signature on file) Copyright 2003 Garmin AT, Inc. All Rights Reserved Part #: 560-0987-00 Rev E Revision Log Cage Code...
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...7 IRING ...7 IRCUIT ROTECTION LECTRICAL NALYSIS SPECIAL INSTALLATION INSTRUCTIONS ...7 ADDITIONAL SYSTEM NOTES ...7 Copyright 2003 Garmin AT, Inc. All Rights Reserved Table of Contents ...4 ODEL ...4 )...5 ...7 27 October 2003 Part #: 560-0987-00 Rev E...
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.
2345 Turner Rd SE Salem, OR 97302 2.1.2 Continued Airworthiness Instructions for continued airworthiness are found in Garmin AT document number 560-0986-00 Instructions for Continued Airworthiness. 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.
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 Part #: 560-0987-00 Rev E Mfg.
CNX80 power requirements. 4 Special Installation Instructions None 5 Additional System Notes No other system notes. Copyright 2003 Garmin AT, Inc. All Rights Reserved 27 October 2003 Part #: 560-0987-00 Rev E Page 7 of 7...