Quantcast Section IX. ELECTRICAL SYSTEM

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ameter, 7 x 19 aircraft-type, preformed cable.
Thread  through
holes  in  operating  shaft  until  both  ends  are
of  equal  length.
Thread ends through holes in pickup member. Twist ends in
loose,  single  knot  across  pickup  member  in  such  a  manner  that
both  ends  may  be  clamped  with  both  U-bolts.  Install  four
-inch  plain  washers  and  -inch  hex  nuts  on  two  U-bolts.
Install
spare
wheel
and
tire
carrier (b a b o v e ) .
Section IX. ELECTRICAL SYSTEM
71.
Electrical
Sockets,
and
Wiring
a.
General.
All  electrical  cables  for  the  lights  lead  from
sockets and/or receptacles mounted on the front cross mem-
ber of the chassis frame.
All cables for taillights, blackout
stoplights,
and
turn
indicator  lights  are  attached  to  the  left
chassis frame longitudinal beam.
Cables for side blackout and
side
eclarance
lights
lead
from
the  main  harness  to  their  re-
spective electrical connectors at the body frame side rails.  A l l
cables  are  secured  with  cushioned  clips  which  are  attached
with lockwasher and hex nuts to studs or bolts welded to
frame,  beams,  and  cross  members.  All  cables  are  identified
TAGO 1321B
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