Instruction Manual

Instructions for Continued Airworthiness 190-01527-15 Rev 1
for the Garmin G500H Installation in Eurocopter EC130 Page 4 of 82
CHAPTER 1
Section 01-00-00 Introduction
These are accepted Instructions for Continued Airworthiness for modifications performed in
accordance with Eurocopter EC130 B4 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 EC130 B4
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