Textron Cessna 182S - Page 189

CESSNA AIRCRAFT COMPANY
MODEL 182/T182
WIRING
DIAGRAM
MANUAL
B. Tools used with permanent crimp environmental resistant splices.
NOTE: The following tools (or equivalent) are required.
(1)
Heat gun part number CV5700 and reflector
part number MG7 are available through
Raychem
Corp. V06090.
(2) For crimp tool information refer to Table 206.
Table 206. Permanent Crimp Environmental Resistant Splice Installation Tools
M81824/1-1, M81824/1-2, D436-36, D436-37, D436-52, D436-110
CRIMP TOOL DIE MANUFACTURER
M22520/5-01
M22520/10-01
AD1377
M81824/1-3, D436-38, D436-53
CRIMP TOOL
M22520/5-103
M22520/10-104
none
DIE
Commercially Available
Commercially
Available
Raychem Corp. V06090
MANUFACTURER
M22520/5-01
M22520/10-01
AD1377
M22520/5-102
M22520/10-103
none
Commercially Available
Commercially Available
Raychem Corp. V06090
C. Installation of permanent crimp environmental resistant splices.
(1) MIL-S-81824 Type Splices.
(a) Slide the insulating/sealing sleeve onto the wire(s) that will be located at one end of the
sleeve.
(b)
Strip 0.312
to 0.343
of insulation
from the wires.
(c) Insert
the wires into
crimp barrel
and crimp with
crimp tool.
(d) Slide the insulating/sealing sleeve to center the crimp barrel between the sealing rings.
(e) Using a heat gun, shrink the insulating/sealing sleeve over the crimp barrel and wires.
Continue to heat the ends
of the sealing sleeve until the meltable
inserts flow from the
ends of the sleeve.
(2) 3-Wire Guide Type Splices Sealing Insert.
(a) Slide the insulating/sealing sleeve onto the wires that will be located on the 3-wire guide
end of splice, maximum of 2 wires in each hole in wire guide.
(b) Repeat Steps
6.C.1 (b) through (e) for
MIL-S-81824 type splices.
Table 207. Permanent Crimp Environmental Resistant Splices
WIRE END 1
SPLICE
* PART
NUMBER
WIRE SIZE
24
22
APPROVED
TO MIL.
SPEC. PART
NUMBER
SINGLE WIRE SPLICING
D436-36
RED
D436-36
RED
M81824/1-1
M81824/1-1
WIRE END 2
NUMBER
OF WIRES
1
1
WIRE SIZE
24
22
20-10-06
© Cessna Aircraft Company
NUMBER
OF WIRES
1
1
Page 205
Mar 1/2004