BFGoodrich PS-823 - Page 50

BFGoodrich
Avionics
Systems,
Inc.
Component
Maintenance
Manual
P/N
10
1-1075-(
)
Corrective
Test
Procedure Normal
Indication
Active
2.13
Cont.
Indicator
Test
Point
3Ø
1Ø
F to C
112.5±17.5Vac
NA
C to
E
115
±5.0Vac
117±7.0Vac
FtoE
I15±lI.0Vac
NA
The
flag should not
appear
during
the
run
cycle.
For
PS-823C,
D,
G,
H
The Indicator shall
accelerate
to
fullspeed
in
less
than
6.0 minutes.
After
synchronization
speed
is
attained
the
voltage betweenpins
shall
be as
follows:
Pin (Jl) Voltage
I
to
3
115.0V
±11.0Vac
3 to
7
115.0V
±5.0Vac
1
to 7
115.0V
±11.0Vac
The flag
should
not
appear
during
the
run
cycle.
e.
Place
the
ON-OFF-CHARGE
switch
OFF,
and
disconnect
the indicator.
Performance Test with
JT-5
Test Set
Figure 115
(Cont.)
msmijtp202TestFaultIsodiskl59
24-20-03
Page
130
Revision A June 30, 1999