Raytheon Beech Baron E55 - Page 835

P"
I
i
L37A20
L51B20
I
-L
L37820
L103AZON
I
C-20
L44A2DSj~i
L52A20---t
B-20
L30A20
r
ICI
L102A20
~C
L38A20
eB-20EI
L54A20
aoj
2
f
ENGINE
INSTRUMENT
E-20
L30B20
L51A20
CONSOLE
AND
AVIONICS
L49A20N
rj
~L39A20
Ef
In
L103B20N
DIMMING
L’102B20
I
ELECTROLUMINESCENT
L50A20R!1
L52A20
L31A20
T
t
r-
L43A20
__~
L43A20
DIMM1NG
Pt
s,
L44B20
i
L58A20
OPTIONAL
ENGINE
L39B20
TO
L48A20N
i
L53h20N
I
i
L102C20
LIGHTS
INSTRUMENT
WEDGE
FUEL
L39E20
L32A20NRED
C-20
I
L43BZO
L43C20
SELECTTAB
ELEVATOR
L39C20
s
INDICATOR
8-20FLIGHT
L102D20*f
FLAP
L39D20
POSITION
r
BLACK
EI
i
INSTRUMENT
AILERON
L33820
DIMMING
TAB
LH
RH
E20
INDICATOR
L102E20
ENGINE
ENGINE
;Z’
GAGE
GAGE
RED
L56A20
L90A20
L
TO
L64,20N
A
BLACK
TO
TO
OPTIONAL
CABIN
RADIO
/A\
FLIGHT
LIGHTS
LIGHTS
INSTRUMENT
WIRE
FURNISHED
WITH
LIGHT
(REF.
WHEEL CLOCK~
I
L102FZO
POST
LIGHTS
L39E20
CONNECTED TO BUS NO.
2
WHEN
L57820
-1--, I
’./A’´• GEAR
THESE LIGHTS
ARE
LANDING
OPTIONAL
FLIGHT
INSTRUMENT
VISUAL
POST LIGHTS
ARE
INSTALLED
A’
I I I
I
I I
L102GZO
WHEN OPTIONAL
ENGINE
INSTRUMENT
POST
LIGHTS
ARE
INSTALLED
THESE
LIGHTS
ARE CONNECTED
AI
’TE838 AND AFTER
TO BUS NO.
1
A\
i’
TH´•141
AND
AFTER
2
Circuit
Branker
i_
OMNI
OMNI
"TE´•826
AND
AFTER
l.aul
Bil
TH´•83
AND AFTER
3
Llph~
Dlnlnllng
Tranlt,lo,
I
"’TH 1
FIND
BFTEA
TO
4
Ahcorln~
Lti7U7(1
(;I~RESI(IFCT)
OPTIONAL
5
Connccio F
LWOD
LIGHTS
FLIGHT
6E
Isctrolun´•llns´•icenI
panel.
Left Swltc)lc?e
INS~RUMENf
7
W~DCE
E 1YO1
Uldll
LIGHTS
9
Rsii~lo,
Instrument
Lights
TE-938,
TE-943
thru
TE-1063
TH-385
thru
fH-647
srcept
TH-598
14-138