Instruction Manual

Instructions for Continued Airworthiness 190-01190-11 Rev. 1
for G500H in Robinson R44 Series Rotorcraft Page 3 of 20
1. INTRODUCTION
1.1 Purpose
This document is designed for use by the installing agency of the Garmin G500H PFD/MFD System as
Instructions for Continued Airworthiness in response to Title 14 CFR Part 27.1529 and Part 27 Appendix
A. This ICA includes information required by the operator to adequately maintain the Garmin G500H
system installed under STC TBD.
1.2 Scope
This document identifies the Instruction for Continued Airworthiness for the modification of the rotorcraft
for installation of the Garmin G500H PFD/MFD System installed under STC TBD.
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 G500H system 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) ADC: Air Data Computer
3) AEG: Aircraft Evaluation Group
4) AHRS: Attitude Heading Reference System
5) CFR: Code of Federal Regulations
6) FAA: Federal Aviation Administration
7) ICA: Instructions for Continued Airworthiness
8) MFD: Multi-Function Display
9) PFD: Primary Flight Display
10) PMI: Principal Maintenance Inspector
11) STC: Supplemental Type Certificate