TM 55-1730-229-12
TO 35C2-3-473-1
NOTE
(2) Ensure that DC POWER switch is
set to OFF.
While 83-360D still has the
capacity of providing 50 amps
NOTE
DC output from the battery
Battery power cannot be uses
charger in combination with
if DC POWER switch is set to
AC, this operation is not
ON.
recommended. Using normal DC
output procedures, the TRU can
(3) Set BATTERY OUTPUT switch to
deliver 5-7 times the DC with
ON.
no danger of overloading and
burning out the battery
Slave
charger. For the 83-360D, DC
start may be accomplished by two
power output is obtained in
methods:
(1) from a dc generator
the same way, whether in
supplying 220 to 32 vdc, 800 amp
combination with AC power
minimum; or (2) from an external 24
(lb.) or with no AC power
vdc battery.
(1c). Settings in 1c of the
table are used.
b. Combined Output Operation.
NOTE
following steps.
DC generator used to start
AGPU in this procedure may
(1) Select desire output from
be another AGPU, or any gen-
column 1.
erator set capable of sup-
supplying between 22 to 32
(2) Make load connections by
vdc, 800 amp minimum current.
performing applicable steps refer-
enced in column 4.
electrical (slave) cable
that
will
mate
with
CAUTION
AGPU
slave
receptacle.
When applying power under
(1) On AGPU to be started, perform
combined output operation,
steps in Prestart Procedure, para-
observe the sequence specified
in applicable aircraft TM.
(4) Apply power to aircraft by
CAUTION
performing applicable steps refer-
Ensure that BATTERY OUTPUT
referenced in column 4.
switch on AGPU remains in
(5) Remove power from aircraft
OFF position at all times
by
performing
applicable
steps
when starting from a
DC
referenced in column 5.
DC generator.
c. To obtain DC power (50 amps
maximum)
while
operating
in
AC
mode, perform the following steps
DC power switch is set to off.
(3) Connect slave cable from DC
generator to slave receptacle on
(1) Set CURRENT LIMIT SELECTOR
switch to AC 10KW, 20KW, or 30KW
AGPU.
position.