Raytheon Beech Baron E55 - Page 642

Raytheon
nircraft
Company
BARON 55
AND
58
SHOP
MANUAL
Chart
11
MAXIMUM
CONTINUOUS
ELECTRICAL
UTILIZATION
(Standard
Equipment)
(Continued)
MODEL
58
(TH-680
thru
TH-972)
No.
Per
Amperes Amperes
Equipment
Part
No.
Airplane
Per
Unit
Total
Not
used
while in
flight.
Only
one
used at
a
time.
Chart
12
MAXIMUM
CONTINUOUS
ELECTRICAL
UTILIZATION
(Optional
Equipment)
MODEL
58
(TH-680
thru
TH-972)
No.
Per
Amperes
Amperes
Equipment
Part
No.
Airplane
Per
Unit
Total
Alcohol
Anti-ice
Indicator,
Quantity
50-384001-1
1
0.27
0.27
Alcohol
Anti-ice
Pump
476284
1 0.40
0.40
Alcohol
Anti-ice
Valve
AV-1B-1473
1’ 0.35 0.35
Anti-ice,
Prop
(2
Blades)
Kit 65-060
1 12.00
12.00
Anti-ice,
Prop (3
Blades)
Kit
65-065
1
18.00 18.00
Heater,
Pitot,
R.H.
50-384040
1
4.00
4.00
Indicator,
Engine
Hours
15000 Series
1
0.05 0.05
Indicator,
Flight
Hours
58-380043-1
1
0.01 0.01
Power
Supply,
Strobe
60-1750-3
1
3.50
3.50
5th
6th
Reading
Light
1495
2
0.30 0.60
Beacon,
Rotating,
Lower
40-01
00-3
1 3.10 3.10
Beacon,
Rotating, Upper
40-01
00-3
1
3.10 3.10
Instrument,
Post
Light
(Single)
327
30
0.04 1.20
Instrument,
Post
Light
(Dual)
327
48 0.04
1.92
Instrument,
Wedge
Light
(Single)
267
(2
ea)
16
0.05
0.80
Instrument,
Wedge
Light
(Dual)
267
(2
ea)
23
0.05 1.15
Valve
required
only
when
windshield
and
prop
alcohol anti-ice
are
installed
concurrently.
Page
44Dec
31/03
SECTION
13
E21