Raytheon Beech Baron E55 - Page 657

Raytheon
Aircraft
Company
BARON
55
AND
58
SHOP MANUAL
Chart
20
AVIONIC
EOUIPMENT
ELECTRICAL
UTILIZATION
(Continued)
MODEL
58
(TH-973
thru
TH-1395,
except
TH-1389)
MODEL
855
(TE-1143
and
After)
MODEL
855
(TC-2181
and
After)
Amperes
Equipment
Part Number
Per
Unit
DG-360
0.50
Autopilot
Trim
Only
1.00
Autopilot
Yaw
Axis
1.90
Inverter
PC-IL~B
6.35
Inverter
PC-1SB
13.10
Inverter
PC-50
2.75
Encoding
Altimeter
Series
519
0.54
Encoding
Altimeter
Series
570
0.32
Code
Translator
KA-43
0.10
Code Translator
KA-58
0.03
Audio
Ampl.
KA-134
1.30
Audio
Ampl.
KAA-445
2.10
Compass System
KCS-55A
1.73
ADF Receiver
KDF-805
0.75
DME
KDM-705A
3.00
Autopilot
KFC-200
(WNaw)
11.05’
W/KCS-55A
Comp.
Sys
(W/O
Yawl
9.03
Glideslope
Receiver
KGM-681
0.24
Marker
Beacon/Glideslope
Receiver
KGM-691
0.35
VOR/LOC
Converter
Indicator
KI-203
0.10
VOR/LOC
Converter
KI-204
0.10
VOR/ILS
Indicator
KI-206
0.10
VOR/LOC
Converter
Indicator
KI-208
0.15
VOR/I1S
Converter
Indicator
KI-209
0.15
Marker
Beacon/Glideslope
Receiver/Audio
KMA-20
1.40
Amplifier
DME
KN-65A
2.40
VOR/LOC
Converter
KN-72
0.05
RNAV
Computer
KN-74
0.35
E21
SECTION
13
Dec
31/03Page
59