SUPPLEMENT SG-3
INTRODUCTION
INTRODUCTION
This document supplements P2002-JF Aircraft Maintenance Manual [doc. No.
2002/30] on those aspects relevant to the installation of the Integrated Flight
Deck System (IFDS) Garmin G500.
These airplane embodies the Design Change MOD2002-041 “Garmin G500 Instal-
lation”.
In the event of discrepancies or conflicts with the basic Aircraft Maintenance
Manual, this Supplement takes precedence.
Herein are reported the ATA Chapters impacted by the design change mentioned
above.
When the G500 suite is installed a 40A External Alternator must be installed to
provide the necessary amount of current to the LRUs. When this design change
is applied, a dedicated breaker panel is installed on the cockpit LH side:
Moreover the installation of GNS 430W or other equivalent external NAV/GPS
source is necessary in order to provide G500 suite with GPS and NAV infor-
mation to be displayed on GDU 620.
ABBREVIATIONS
Attitude and Heading Reference System
Aircraft Maintenance Manual
Post Installation Checkout Procedure