Instruction Manual

G500H Flight Display System 190-01150-21 Rev. 2
Instructions for Continued Airworthiness Bell 407 Page 4 of 19
2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
2.1 Introduction
Content, Scope, Purpose and Arrangement: This document identifies the Instructions for
Continued Airworthiness for the modification of the
rotorcraft by installation of the Garmin G500H
PFD/MFD System.
Applicability: Applies to Bell models 407 rotorcraft altered by
installation of the Garmin G500H PFD/MFD
System.
Definition of Abbreviations: See Section 1.5
Precautions: None
Units of measurement: None
Referenced publications: Garmin 190-01150-06 Rev. 3 “G500H Rotorcraft
STC Installation Manual” or later FAA Approved
Revisions
Garmin 190-01150-44 Rev. 3 “GENERAL
ARRANGEMENT, G500H SYSTEM, BELL 407
ROTORCRAFT” or later FAA Approved Revisions
Additional Maintenance Data: Garmin 190-01150-45 Rev. 3 “INSTALLATION,
G500H SYSTEM, BELL 407 ROTORCRAFT” or
later FAA Approved Revisions
Garmin 005-W0222-00 Rev. 3 “G500H MAIN
WIRE HARNESS ASSEMBLY” or later FAA
Approved Revisions
Garmin 005-W0222-01 Rev. 1 “G500H NAV
1 HARNESS ASSEMBLY” or later FAA
Approved Revisions
Garmin 005-W0222-02 Rev. 1 “G500H GPS
2 HARNESS ASSEMBLY” or later FAA
Approved Revisions
Garmin 005-W0222-03 Rev. 1 “G500H NAV
2 HARNESS ASSEMBLY” or later FAA
Approved Revisions
Garmin 005-W0222-04 Rev. 1 “G500H WX
DATALINK HARNESS ASSEMBLY” or later
FAA Approved Revisions
Garmin 005-W0222-05 Rev. 1 “G500H
IRIDIUM DATALINK HARNESS ASSEMBLY”