Raytheon Beech Baron E55 - Page 650

Raytheon
Aircraft
Company
BARON
55
AND
58
SHOP MANUAL
Chart 16
MAXIMUM
CONTINUOUS
ELECTRICAL UTILIZATION
(Standard
Equipment)
(Continued)
MODEL
58
(TH-973
thru
TH-1395,
except
TH-1389)
MODEL 855
(TE-1143
and
After)
MODEL
855
(TC-2181
end
After)
No.
Per
Amperes
Amperes
Equipment
Part No.
Airplane
Per
Unit
Total
Compass
Light
327
1 0.04
0.04
Elevator
Tab
Light
1819
1
0.04 0.04
Engine
Instruments
Light
327
4
0.04
0.16
Flap
Position
Indicator
Light
58-324065-5
1
0.03
0.03
Glareshield Flood
313 12 0.17
2.04
Map
Light
1495
1
0.30
0.30
OAT
Light
327
1 0.04 0.04
Rheostat
Light
327
1 0.04
0.04
Switch
Panel
Light
327
7’"
0.04
0.28
Tail
Light
A2064-678
1 0.80 0.80
Wing
Tip
Nav.
Light
A7512-24
2 0.93
1.86
Unit
operates
in
gear
down
position only.
Used
only
on
Model
95-855
Used
only
on
Models
58
and
E55.
Omit
two
potentiometers
on
Model 95-855.
Optional
on
Model
95-855
used when
optional
alternators
are
installed.
Both units
are
not
operated
simultaneously.
Dec
31/03Page
52
SECTION
13
821