Raytheon Beech Baron E55 - Page 651

Raytheon
AiKraft
Company
BARON
55
AND
58
SHOP
MANUAL
Chart
17
MAXIMUM
CONTINUOUS ELECTRICAL
UTILIZATION
(Optional Equipment)
MODEL
58
(TH-973
thru
TH-1395,
except
TH-1389)
MODEL E55
(TE-1143
and
After)
MODEL
855
(TC-2181
and
After)
No.Per
Amperes
Amperes
Equipment
Part No.
Airplane
Per Unit
Total
Air
Conditioning
Actuator,
Condenser
Door 96-380021-23
1*
0.77
0.77
Blower
Motors
1523200-4
2
4.07
8.14
Compressor
Clutch
102-389006-1
1
1.70
1.70
Condenser
Blower
58-380081
1
20.00
20.00
Relay,
Condenser
Blower 6041
H200
1
0.35
0.35
Alcohol Anti-ice
System
Indicator,
Quan.
50-384001 1
0.01
0.01
Pump
476284
1
0.60
0.60
Valve,
Windshield
AV-1 B-l
473 1’**
0.29 0.29
Clock,
Digital
CT-24 1
0.20 0.20
Electrothermal
Prop
De-ice
Ammeter
58-380086
1
0.01 0.01
Heater,
Prop
(2
Blade)
Kit
65- 080
1
12.00 12.00
Heater,
Prop
(3
Blade)
Kit
65-085
1
18.00
18.00
Timer
3E1
1
50-3 1
0.29
0.29
Engine
Hour
Meter
58-380042
1
0.01 0.01
Flight
Hour
Meter
58-380043
1
0.01 0.01
Heater,
Pitot
R.H.
50-384040
1
4.60
4.60
Power
Supply,
Strobe
60-1750-3
1
5.00
5.00
Prop.
Synchronizer
Governor
System
213699
1
1.00 1.00
Lighting
5th
6th
Reading
303
2
0.30 0.60
Control
Wheel Clock
327
1 0.04 0.04
Engine
Hour
327
1
0.04
0.04
Flight
Hour
327
1
0.04 0.04
Instrument,
Post
(Single)
327
34
0.04 1.36
Instrument,
Post
(Dual)
327
40
0.04
1.60
E21
SECTION
13
Dec
31/03Page
53