Garmin 400W Series Ergänzendes Flughandbuch - Seite 6

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GARMIN Ltd. or its subsidiaries

1200 E. 151

AIRPLANE FLIGHT MANUAL SUPPLEMENT

or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL

for a Garmin 400W Series Navigation System

Section 2. LIMITATIONS

2.1

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.

400W Series Pilot's Guide & Reference P/N 190-00356-00 Rev E

400W/500W Series Optional Displays P/N 190-00356-30 Rev F

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

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

Software Item

Main SW Version

GPS SW Version

190-00356-03 Rev. B

Page 6 of 16

c/o Garmin International

Street, Olathe, KS 66062 USA

Approved Software Version

(or later FAA approved versions for this STC)

SW version

3.30

3.2

As displayed on unit

3.30

3.2