Textron Cessna 182S - Page 191

CESSNA AIRCRAFT
COMPANY
MODEL 182/T182
WIRING DIAGRAM MANUAL
Table 207. Permanent Crimp Environmental Resistant Splices (continued)
WIRE END 1 SPLICE APPROVED WIRE END 2
* PART TO MIL.
NUMBER SPEC. PART
NUMBER
16 D436-38
YELLOW
16 D436-38
YELLOW
16 D436-38
YELLOW
24
D436-0110
RED
24
D436-0110
RED
24 D436-0110
RED
22 D436-52
BLUE
22 D436-52
BLUE
22 D436-52
BLUE
20 D436-53
YELLOW
20 D436-53
YELLOW
20 and 18 D436-53
YELLOW
18 D436-53
YELLOW
18
D436-53
YELLOW
M81824/1-3 2 1
M81824/1-3
M81824/1-3
1 16
1 14
24
24
22
22 and 20
20
22
20
18
20
18
18
*
Raychem Corp.
V06090
D.
Combinations of wire
splicing not shown in
Table 207, may be determined
by the following
procedure:
(1) Calculate
the Circular Mil Area (CMA) for each
end of the splice. Refer to Table 208.
20-10-06 Page 207
© Cessna Aircraft Company
Mar 1/2004
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