Instruction Manual

Instructions for Continued Airworthiness 190-00792-12 Rev 1
for the Garmin G500H Installation in Eurocopter AS350 Page 4 of 80
CHAPTER 1
Section 01-00-00 Introduction
These are accepted Instructions for Continued Airworthiness for modifications performed in
accordance with Eurocopter AS350 Garmin G500H Flight Display System Installation STC. All
references to the G500H in this document will refer to the Garmin G500H Flight Display System
Installation and other related components specified in these Instructions for Continued
Airworthiness (ICA). A STC permission letter and Instructions for Continued Airworthiness (ICA)
should be supplied to the owner/operator of the STC at the time of completion. Subsequent
accepted changes to the ICA will be distributed to owners and operators of the STC.
This, Instructions for Continued Airworthiness, is intended to supplement the Model AS350
rotorcraft maintenance manuals provided by Eurocopter. The information, procedures,
requirements, and limitations contained in this, Instructions for Continued Airworthiness, for
this type design change supersedes the information, procedures, requirements, and limitations
contained in the rotorcraft’s maintenance manual when the type design change is installed on
the Type Certificate Holder’s rotorcraft.
01-00-00