GDL 90 UAT System Helicopter STC Master Data List

Transcription

1 GDL 90 UAT System Helicopter STC Master Data List Part Number: Document Revision: D 20 September 2007, Inc Turner Rd SE USA Phone (503) FAX (503) TM is a trademark of Garmin Ltd. or its subsidiaries. Printed in the USA Copyright 2005 to 2007, Inc. All Rights Reserved Page 1 of 7

2 Revision Log Rev Date Description EN By A 07-Dec-2005 Original Release, MS Word mak B 02-Feb-2006 Update RFMS to -01 Rev A, and STC Accomplishment Summary to Rev B; add GSL 71 Helicopter Install Supplement document (Table 1, Table 2) mak C 26-Apr-2006 Update for v2.1 GDL 90, GA 56W/56A/57 GPS antennas, EC 130 on AML, and ICA acceptance, RFMS (Table 1, Table 2, Table 3). D 20-Sep-2007 Update for V2.2, GA GPS antennas, structural skin GPS antenna installations, latest manuals & ICA (Table 1, Table 2, Table 3, ) mak 8451 mak Title: Prepared By: Approved By:, Inc. Cage Code 0XCJ6 GDL 90 UAT System Helicopter STC Master Data List Marvin A. Kumley Thomas L Mosher Tom Mosher, GDL 90 Project Manager 2345 Turner Road SE, Salem, Oregon USA Number: Date: 7 December 2005 Date: 22 Dec 2005 Copyright 2005 to 2007, Inc. All Rights Reserved Page 2 of 7

3 Table of Contents 1 INTRODUCTION PURPOSE SCOPE STC INCLUDES APPROVED MODEL LIST DATA AND EQUIPMENT LIST REQUIRED FOR INSTALLATION DATA REQUIRED FOR INSTALLATION GDL 90 UAT SYSTEM INSTALLATION DATA CONTINUED AIRWORTHINESS RELATED DATA (SUBSTANTIATING DATA) REFERENCE DOCUMENTS EQUIPMENT LIST GENERAL INSTALLATION REQUIREMENTS GENERAL MECHANICAL HARDWARE WIRING CIRCUIT PROTECTION ELECTRICAL LOAD ANALYSIS SPECIAL INSTALLATION INSTRUCTIONS ADDITIONAL SYSTEM NOTES...7 Copyright 2005 to 2007, Inc. All Rights Reserved Page 3 of 7

4 1 Introduction 1.1 Purpose The purpose of this document is to list the data required to support STC installation of the Garmin GDL 90 UAT System in accordance with STC SR01863LA 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 GDL 90 UAT System 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. 2 Data and Equipment List Required for Installation 2.1 Data Required for Installation GDL 90 UAT System Installation Data The 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 Or Or Doc No. Rev Description D GDL 90 UAT Heli Master Data List (this document) C GDL 90 UAT Heli Instructions for Continued Airworthiness C GDL 90 UAT Installation Manual C A-41 UAT Antenna Information B A-40 UAT Antenna Information D A-33 GPS Antenna Installation Manual F A-34 & GA 35 GPS Antenna Installation Manual D GA 56W Antenna Installation Instructions B GA 55A, 56A, 57 Antenna Installation Instructions F GA Antenna Series Installation Instructions A GA 36 GA 36 GA 37 Antenna Installation Instructions C GDL 90 UAT Helicopter Installation Manual Supplement B GSL 71 UAT Control Panel Helicopter Install Supplement C GSL 71 Rotorcraft Flight Manual Supplement B GSL 71 Pilot s Guide Manual Copyright 2005 to 2007, Inc. All Rights Reserved Page 4 of 7

5 Doc No. Rev Description D GSL 71 Installation Manual Continued Airworthiness Instructions for continued airworthiness are found in document number 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 GSL 71 UAT Control Panel Installation kit GDL 90 UAT Installation kit PD3538 C GDL 90 UAT Acceptance Analysis for Aircraft on the AML PD3601 C GDL 90 UAT System Safety Assessment PD3608 D GDL 90 UAT Helicopter STC System Accomplishment Summary PD3609 B GDL 90 UAT Helicopter Ground & Flight Test Plan PD3614 B GDL 90 UAT Process for the Acceptance of Aircraft on the AML PD6008 B Capstone AS-350 Helicopter STC PSCP 2.3 Reference Documents The following documents are used as reference for the installation. FAA AC B, Acceptable Methods, Techniques, and Practices - Aircraft Inspection and Repair FAA AC A, Acceptable Methods, Techniques, and Practices - Aircraft Alterations FAA AC A, Airworthiness approval of Global Navigation Satellite System (GNSS) Equipment 2.4 Equipment List All equipment must have the Part Numbers and Software Versions contained in Table 3 (or later FAA approved revisions or versions). Copyright 2005 to 2007, Inc. All Rights Reserved Page 5 of 7

6 Table 3 - System Equipment List OR OR Description Model No. Mfg. P/N Mfg. Comment Data Link Sensor GDL SW Ver. 2.0, 2.1, or 2.2 UAT Control Panel GSL Optional, SW Ver. 1.0 Micro APM SW Ver. 1.0 UAT Antenna A AT AeroAntenna Optional antenna UAT Antenna A Standard antenna CI Comant GPS Antenna A Optional antenna AT AeroAntenna GPS Antenna A Optional teardrop AT AeroAntenna footprint GPS Antenna GA Garmin Standard teardrop footprint GPS Antenna GA Garmin Optional arinc footprint GPS Antenna GA Garmin Optional GPS + XM GPS Antenna GA 56W Garmin Optional teardrop antenna GPS Antenna GA 56A Garmin Optional arinc footprint GPS Antenna GA Garmin Optional GPS + XM Equipment listed as equivalent in the STC documents is equivalent with respect to functionality of the GDL 90 UAT system 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 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 Copyright 2005 to 2007, Inc. All Rights Reserved Page 6 of 7

7 recommended practices and procedures found in AC A, Chapter 2, Radio Installations, and Chapter 3, Antenna Installations; AC B, Chapter 11, Electrical Systems, Section 3, 4 and 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 B, Chapter 5, Aircraft Hardware. 3.4 Wiring All wire used in the installation shall be of appropriate standard aircraft quality grade and size as described in AC B, Chapter 11, Sections Circuit Protection All circuits shall be protected in accordance with AC B, 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 B, Chapter 11 Section 3. The document P/N GDL 90 UAT Installation Manual provides specifications on the GDL 90 UAT power requirements. The document P/N GSL 71 Installation Manual provides specifications on the GSL 71 power requirements. 4 Special Installation Instructions None 5 Additional System Notes No other system notes. Copyright 2005 to 2007, Inc. All Rights Reserved Page 7 of 7