ENGINE AIRSTARTS (CONT)
23.
Battery Charging Bus Current Limiter Check:
Failure to successfully complete
the
following
current
limiter checks indicates a malfunction.
In
this event, re-
fer
to
CURRENT UMITER FAILURE/ILLUMINATION
OF
CUR UM (CUR
UMITER)
UGHf
IN
FUGHT
procedure, this section.
-Aircraft 35-067 thru 35-147 and aircraft 36-018 thru 36-035
except aircraft incorporating
AMK
80-17
or
AAK
81-1:
a.
MAIN
BUS
TIE
Circuit Breaker (copilot's panel) -
Pull.
b.
One
START -GEN Switch -
OFF.
Check ammeter reading
on
opposite generator, apprOximately doubles, then switch back
to
GEN.
c. OppoSite START -GEN Switch -
OFF.
Check ammeter read-
ing
on
opposite generator, approximately doubles, then switch
back to GEN.
d.
MAIN
BUS TIE Circuit Breaker - Reset.
-Aircraft 35-148 thru 35-389 except 35-370
and
aircraft 36-036
thru 36-047 except aircraft incorporating AMK 80-17
or
AAK
81-1:
a. TEST Selector Switch - Rotate to L CUR UM.
b.
TEST Button - Depress. Green current limiter light
will
illumi-
nate and remain
on
while button
is
held. L
GEN
light
will
illumi-
nate and right generator voltage may
be
reduced
approximately 2 vdc.
c.
'TEST"Selector Switch - Rotate to R CUR UM.
d. TEST Button - Depress. Green current limiter light
will
illumi-
nate and remain
on
while button
is
held. R
GEN
light
will
illu-
minate and left generator voltage may
be
reduced
approximately 2 vdc.
- Aircraft 35-067 thru 35-389 except 35-370
and
36-018 thru 36-
047 incorporating
AMK
80-17
or
AAK
81-1:
a. L CUR UMITER
and
R CUR UMITER Lights - Check
extinguished.
- Aircraft 35-370, 35-390
and
subsequent
and
aircraft 36-048
and subsequent:
a. . CUR
UM
Light - Check extinguished.
FAA APPROVED 4-30-76
REISSUED
2-25-81, CHANGE 10
3·19
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