GARMIN Ltd.
or
its
subsidiaries
do
Garmin
Internationa)
1200
E.
151“
Street,
Olathe,
KS
66062
USA
AIRPLANE FLIGHT
MANUAL SUPPLEMENT
or
SUPPLEMENTAL
AIRPLANE FLIGHT MANUAL
for
a Garmin 400W Series Navigation System
Section
2. LIMITATIONS
2.1
Pilot's Guide
The
GARMIN
400W Scries 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 Scries 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
System Software:
The
system
must
utilize the
Main and
GPS
software
versions listed
below
(or
later
FAA approved
versions). The
software versions
arc
displayed
on
the
self-test
page immediately
after tum-on
for approximately
5
seconds
or
they
can
be accessed
in
the
AUX
pages.
Subsequent software versions may
support
different functions. Cheek
the
400W Series
Pilot’s
Guide
for further information.
Table
I
-
Approved
Software Versions
Software
Item
Approved
Software
Version
(or
later
FAA
approved
versions
for
this
STC
)
SW version
As
displayed
on
unit
Main SW Version
3.30
3.30
GPS SW Version
3.2
3.2
190-00356-03
Rev.
B
Page 6
of
16
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