Instruction Manual

Instructions for Continued Airworthiness 190-01190-11 Rev. 1
for G500H in Robinson R44 Series Rotorcraft Page 4 of 20
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 Robinson R44 series 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 190-01190-06 Rev. 2 “G500H
INSTALLATION MANUAL FOR ROBINSON R44
SERIES ROTOCRAFT” or later revision
Garmin 190-01150-02, Rev. C “G500H PILOT
GUIDE” or later revision
Additional Maintenance Data:
Garmin 005-W0227-00 Rev. 1 “G500H Robinson
R44 MAIN WIRE HARNESS ASSY DWG (REQ’D)”
or later revision
Garmin 005-W0227-01 Rev. 1 “G500H
ROBINSON R44 NAV1 HARNESS ASSY DWG
(OPTL)” or later revision
Garmin 005-W0227-02 Rev. 1 “G500H
ROBINSON R44 GPS2 HARNESS ASSY DWG
(OPTL)” or later revision
Garmin 005-W0227-03 Rev. 1 “G500H
ROBINSON R44 NAV2 HARNESS ASSY DWG
(OPTL)” or later revision
Garmin 005-W0227-04 Rev. 1 “G500H
ROBINSON R44 WX DATALINK HARNESS ASSY
DWG (OPTL)” or later revision
Garmin 005-W0227-05 Rev. 1 “G500H
ROBINSON R44 IRIDIUM DATALINK HARNESS
ASSY DWG (OPTL)” or later revision
Garmin 005-W0227-06 Rev. 1 “G500H
ROBINSON R44 VIDEO HARNESS ASSY DWG
(OPTL)” or later revision