Airplane Flight Manual Supplement

GARMIN Ltd. or its subsidiaries
c/o Garmin International
1200 E. 151" Street, Olathe, KS 66062 USA
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
GARMIN 400W SERIES GPS-WAAS NAVIGATION SYSTEM
Bell 206B
Section I. LIMITATIONS
1.1 Pilot's Guide
The GARMIN 400W Series Pilot's Guide, part number and revision listed below (or later
revisions), must be immediately available for the flight crew whenever navigation is
predicated on the use of the 400W Series unit.
400W Series Pilot's Guide & Ref
PIN 190-00356-00 Rev G
400W/500W Series Optional Displays PIN 190-00356-30 Rev H
This model helicopter when equipped with the G400W is limited to VFR ONLY
operations in accordance with 14 Code of Federal Regulations Part 91 and Part 135. The
placard listed below shall be located in close proximity to the 400W Series unit.
"APPROVED FOR DAYINIGIIT VFR".
1.2 System Software:
The system must utilize the Main and GPS software versions listed below (or later FAA
approved versions for this STC). The software versions are displayed on the self-test
page immediately after turn.on for approximately 5 seconds or they can be accessed in
the AUX pages.
Subsequent software versions may support different functions. Check the 400W Series
Pilot's Guide for further information.
Table 1 - Almroved Software Versions
Approved Software Version
Software Item
(or lacer FAA annroved versions (or chis STCJ
SW version
As disnlaved on unit
Main SW Version
4.01
4.01
GPS SW Version
3.2
3.2
FAA APPROVED
SEP 27 2010
DATE:
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190-01226-06 Rev. I
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