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Textron Cessna 182S - Page 192

Textron Cessna 182S
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CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING DIAGRAM
MANUAL
EXAMPLE:
Splicing
three
AWG
22
wires
to
one
AWG
16
wire:
Wire
End
1
CMA
=
3
X
754
=
2262
Wire
End
2
CMA
=
2426
Table
208.
CMA
(Circular
Mill Area)
Of
Common
Conductors
WIRE
24
22 20
18
16
14
12
SIZE
(AWG)
STRANDS
19
19
19
19
19
19
37
CMA
475
754
1216
1900
2426
3831
(2)
Determine,
from
Table
209,
which
splice
part
numbers
will
accommodate
the
CMA
and
the
number
of
wires
of
End
1.
Note
that
a
maximum
of
two
wires
can
be
sealed
in
any
one
hole
in
a
sealing
insert.
(In
the
chart,
refer
to
the
MAXIMUM
NUMBERS
OF WIRES,
END
1
and
END
2
columns,
and
CMA
RANGE
OF BARREL,
MINIMUM
and
MAXIMUM
columns)
Example:
Three
AWG
22
wires
2262
CMA
Possible
splices
include
Part
Numbers
D436-52
and
D436-53
(3)
Determine
which
part
numbers will
accommodate the
CMA
and
the
number
of wires
of
End
2.
Example:
One
AWG
16
wire
2426
CMA
Possible
splices
include
Part
Numbers
D436-52
and
D436-53
(4)
Select
the
part
number
for
the
smallest
splice that
will
accommodate
both
ends.
Example:
D436-52
for
three
AWG
22
to
one
AWG
16.
Table
209.
CMA
(Circular
Mill
Area)
Limits
of
Splices
CMA
RANGE
OF
BARREL
COLOR
MINIMUM
MAXIMUM
END
1
304
779
1900
304
779
1900
1510
2680
6755
1510
2680
6755
2
2
2
6*
6*
6*
*
Maximum
number
of
2
wires
per
hole
in
a 3
wire
guide sealing
insert.
7.
Environment
Resistant
Splices
for Shielded
Cable
A.
Refer
to
Table
210
for
splice
information.
20-10-06
©
Cessna
Aircraft
Company
5874
SPLICE
MAXIMUM
NUMBER
OF
WIRES
PART
NUMBER
D436-36
D436-37
D436-38
D436-0110
D436-52
D436-53
RED
BLUE
YELLOW
RED
BLUE
YELLOW
END
2
2
2
2
2
2
2
Page
208
Mar 1/2004

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