GARMIN Ltd. or its subsidiaries
c/o Garmin International
1200 E. 151
st
Street, Olathe, KS 66062 USA
AIRPLANE FLIGHT MANUAL SUPPLEMENT
or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL
for a Garmin 400W Series Navigation System
190-00356-03 Rev. B
Page 6 of 16
Section 2.
LIMITATIONS
2.1
Pilot’s Guide
The GARMIN 400W Series Pilot’s Guide, part number and revision listed
below (or later applicable revisions), must be immediately available for the
flight crew whenever navigation is predicated on the use of the 400W Series
unit.
y
400W Series Pilot’s Guide & Reference P/N 190-00356-00 Rev E
y
400W/500W Series Optional Displays P/N 190-00356-30 Rev F
y
400W/500W Series Display Interfaces P/N 190-00356-31 Rev B
This AFM supplement does not grant approval for IFR operations to aircraft
limited to VFR operations. Additional aircraft systems may be required for
IFR operational approval. Systems limited to VFR shall be placarded in
close proximity to the 400W Series unit
“
GPS LIMITED TO VFR USE ONLY
”.
2.2
System Software:
The system must utilize the Main and GPS software versions listed below (or
later FAA approved versions). 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 - Approved Software Versions
Approved Software Version
(or later FAA approved versions for this STC)
Software Item
SW version
As displayed on unit
Main SW Version
3.30
3.30
GPS SW Version
3.2
3.2
