Garmin GNS 530AW 사용 설명서 - 페이지 4
{카테고리_이름} Garmin GNS 530AW에 대한 사용 설명서을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin GNS 530AW 23 페이지. For continued airworthiness bell 206b
Garmin GNS 530AW에 대해서도 마찬가지입니다: 파일럿 매뉴얼 부록 (24 페이지), 파일럿 매뉴얼 부록 (50 페이지), 파일럿 매뉴얼 부록 (24 페이지), 보충 설명서 (12 페이지), 빠른 참조 (23 페이지), 빠른 참조 (25 페이지)
1. INTRODUCTION
1.1 Purpose
This document is designed for use by the installing agency of the Garmin Model 500W series
GPS/WAAS Nav/Com as Instructions for Continued Airworthiness in response to Title 14 CFR Part
27.1529, Part 27 Appendix A. This ICA includes information required by the operator to adequately
maintain the Garmin 500W unit and additional equipment installed under STC SR02080SE.
1.2 Scope
This document identifies the Instruction for Continued Airworthiness for the Bell 206B series rotorcraft
modified by the installation of the Garmin Models 500W series GPS/WAAS Nav/Com unit and additional
equipment under STC SR02080SE.
1.3 Document Control
This document shall be released, archived, and controlled in accordance with the Garmin document
control system. When this document is revised, refer to Section 2.15 for information on how to gain FAA
acceptance or approval and how to notify customers of changes.
1.4 Permission to Use Certain Documents
Permission is granted to any corporation or person applying for approval of a Garmin Model 500W series
to use and reference appropriate STC documents to accomplish the Instructions for Continued
Airworthiness and show compliance with STC engineering data. This permission does not construe
suitability of the documents. It is the responsibility of the applicant to determine the suitability of the
documents for the ICA.
1.5 Definitions
The following terminology is used within this document:
1) ACO: Aircraft Certification Office
2) AEG: Aircraft Evaluation Group
3) CFR: Code of Federal Regulations
4) FAA: Federal Aviation Administration
5) ICA: Instructions for Continued Airworthiness
6) PMI: Principle Maintenance Inspector
7) STC: Supplemental Type Certificate
500W Series
Instructions for Continued Airworthiness Bell 206B
190-01226-03 Rev. 5
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