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 5 of 7
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