Garmin GPS 400W Installation Manual page 76

C H A N N E L O U T P U T S
S e l e c t i o n
O f f
A v i a t i o n
A v t n n o a l t
C r o s s f i l l
G D L 6 9
H W E G P W S
R y a n T C A D
W X - 5 0 0
5 . 3 . 3 M A I N S Y S T E M C O N F I G
S e l e c t t h e M A I N S Y S T E M C O N F I G P a g e ( s e e F i g u r e 5 - 3 ) .
T h i s p a g e a l l o w s y o u t o c o n f i g u r e t h e F u e l , T e r r a i n , a n d
D i s c r e t e s o p t i o n s .
F u e l
F u e l C O N F I G U R E
S e l e c t i n t h e
S e l e c t i o n
A V g a s
J e t A
J e t B
P a g e 5 - 6
R e v . A
D e s c r i p t i o n
No unit(s) connected to output of this channel
Serial position, altitude, velocity, and navigation data to the following
units:
A r g u s 3 0 0 0 , 5 0 0 0 , o r 7 0 0 0 M o v i n g M a p
E l e c t r o n i c s I n t e r n a t i o n a l F P - 5 L F u e l F l o w C o m p u t e r ( n o n - T S O ' d )
G a r m i n M X 2 0 ( V 5 . 6 o r l a t e r ) , G M X 2 0 0
G a r m i n G P S M A P 1 9 5 , G P S M A P 2 9 5 o r G P S I I I P i l o t
G a r m i n G P S M A P 1 9 6 , G P S M A P 2 9 6 , a n d G P S M A P 3 9 6
G a r m i n G T X 3 2 7 T r a n s p o n d e r
J P I n s t r u m e n t s E D M - 7 0 0 o r E D M - 7 6 0 E n g i n e M o n i t o r
S h a d i n 9 1 2 0 4 X M D i g i t a l F u e l M a n a g e m e n t S y s t e m
S h a d i n 9 1 0 5 3 X M D i g i t a l F u e l M a n a g e m e n t S y s t e m
S h a d i n 9 6 2 8 X X - X F u e l / A i r D a t a C o m p u t e r
S t o r m s c o p e S e r i e s I I ( w i t h N A V A I D ) M o v i n g M a p
Serial position, velocity, and navigation data to the following units:
G a r m i n M X 2 0 ( V 5 . 5 o r e a r l i e r )
H o r i z o n D D M P
I N S I G H T T A S 1 0 0 0 A i r D a t a C o m p u t e r
Serial transfer of flight plans and user waypoints between two
400W/500W Series units
Serial communication to a Garmin GDL 69/69A.
Serial communication to a Bendix/King (Honeywell) KGP 560 EGPWS.
Serial communication with a Ryan TCAD 9900B Series system.
Serial communication to an L3 Communications WX-500 Stormscope.
f i e l d t o s e l e c t t h e F U E L T Y P E (
D e s c r i p t i o n
The aircraft is using Aviation gas (5.8 lbs./gal.)
The aircraft is using Jet A or Jet A-1 fuel (6.7 lbs./gal.)
The aircraft is using Jet B (JP-4) fuel (6.5 lbs./gal.)
F i g u r e 5 - 3 . M A I N S Y S T E M C O N F I G P a g e
A V G a s , J e t A , o r J e t B )
4 0 0 W S e r i e s I n s t a l l a t i o n M a n u a l
1 9 0 - 0 0 3 5 6 - 0 2