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GA RI\ 111\ Ltd. or its subsidiaries
c
1
0
Garmin International
1200 E. 151''
Street. Olathe. KS
66062
LS
1
\
AIRPLANE FLIGHT l\1A>iUAL SLPPLEMENT
or
SlPPLEl\IE:\TAL AIRPLA'\E FLICill"l l\!Al\UAL
for a Garmin
400\\
Series '.\avigation System
Section 2.
LIMITATIO~S
2. l
Pilot's G 11ide
The GARl\111\
400\\
Series
()uide.
part
number
and
revision listed
below (or later applicable revisions). must be immediately available for the
crew whenever
is predicated
on
the use of the
400Vv
Series
unit.
• 400\V
Series Pilot's (iuide
&
Reference Pi?\
190-00356-00
Rev E
• 400\V 500\V
Series Optional Displays P
1
l\ 190-00356-30
Rev F
• 400\V 500\V
Series Display Interfaces P
1
l\ 190-00356-31
Rev B
This AFl\l supplement does
not
grant
for
IFR
operations to aircraft
limited to VFR
Additional aircraft systems may be required for
IFR operational approval. S) stems limited
to
VFR shall be placarded in
close proximity to the
400\V
Series unit
"GPS LIMITED TO VFR lSE ONLY'.
2.2
System Software:
The s;stem
must
utilize the \lain
and
GPS soil ware versions listed below
(or
later
FA:\
approved versions). The soflware versions are displayed
on
the
self-test
atkr turn-on for approximately 5 seconds or they
X
page~.
Subsequent software versions may support different functions. Check the
400\\'
Series Pilot's Guide
for
further information.
T II l
\
is
f
ale
- , .nnrovec , o
tware
Solhvare Item
!\lain SW Version
GPS S\V Version
190-00356-03
Rev.
B
Page 6 of 16
· ers1011s
Approved Software Version
for later F LI approred rersions
for
this SI(
·1
SW version
As displaved on unit
3.30
3.30
~
')
.)._
., I
.)._
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