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 5 of 72.1.2 Continued AirworthinessInstructions for continued airworthiness are found in Garmin AT document number560-0986-00 Instructions for Continued Airworthiness.2.2 Related Data (Substantiating Data)The documents listed in Table 2, or later FAA approved revisions, contain informationrelated to this STC but are not required for follow-on installations.Table 2 - Substantiating DataDoc No. Rev Description424-2014-800 -- Apollo CNX80 Installation kitPD3104 B Apollo CNX80 System Certification PlanPD2248 D Apollo CNX80 STC System Accomplishment SummaryPD3105 -- Apollo CNX80 Plan Software Aspects of CertificationPD2215 -- Apollo CNX80 Plan for PLD Aspects for CertificationPD2249 A Apollo CNX80 System Safety AssessmentPD2212 A Apollo CNX80 Functional Hazard AssessmentPD2267 -- Process for the Acceptance for Aircraft on the CNX STC AMLPD2213 -- Apollo CNX80 Ground & Flight Test PlanPD3108 A Apollo CNX80 Environmental Test Report SummaryPD2106 A Flight Test Report for Motorola Oncore GPS and UPSAT WAAS GPSSensor2.3 Reference DocumentsThe following documents are used as reference for the installation.• FAA AC 43.13-1B, Acceptable Methods, Techniques, and Practices - AircraftInspection and Repair• FAA AC 43.13-2A, Acceptable Methods, Techniques, and Practices - AircraftAlterations• FAA AC 20-138A (final draft) dated 02/01/2003, Airworthiness approval of GlobalNavigation Satellite System (GNSS) Equipment