vision microsystems VM1000 - 1.3 OIL SYSTEM INSTALLATION; Oil Transducer Installation and Wiring

I2
SECTION
t INSTALI,ATION
1.3 OIL SYSTEM
INSTALLATION
I.3.1 OIL TEMPERATURE
TRANSDUCER
INST.
(P/N
3010021)
The transducer
is mounted
on the
engine
and
is designed
for
mounting
according
to MS28034-1.
Consult
your
engine manual
for
the
proper
installation
location.
A
gasket
is supplied
for
use
with the
temperature
transducer.
This
gasket
is designed
to be used only
once.
1.3.2 OIL
PRESSURE
TRANSDUCER
INST.
(P/N
3010018)
=
Do NOT:
MOUNT
TRANSDUCER
DIRECTLY
ON ENGINE.
:)
DO NOT:
mount
the transducer
where
fluids may
contact it
during
operation
or maintenance.
:)
DO NOT:
solder onto
terminal
lugs
of the transducer.
Mount the
transducer
in cabin
or engine
area
using
the
provided
'Adelt'
clamp
to a STATIONARY
location
then safety
wire it
to
the
clamp.
Connect
using
the
appropriate
aircraft
grade
hose and
fittings.
The
transducer
has a 1/8
NPT
externalthread
to accommodate
many
plumbing
options.
BE
CAREFUL
not
to dent
or
deform
the transducer
in any
way or
improper
operation
will result.
Do
not
block
the tiny
-\-./
vent
hole
centered
on the
back
of
the transducer
between
the
lerminals.
Use only
aircraft
grade
fittings
and
hoses.
Refer to
your
engine manual
for
the
proper
oil
pressure
connection
port
location.
"*"
CAUTION**"
Always
discharge
yourself
to
ground
before
wiring.
1.3.3
OIL SYSTEM
WIRING
DPU
TERM.
CABLE
COLOR
XDUCER
PIN
/ WIRE
.XDUCER
DESCR.
XDUCER
PART
NO.
J4-1
RED
RED
OIL
TEMP
301 0021
J4-2
BLK
BLK
3a
J3-1
WHT
PIN
1
OIL PRES
301
001
I
J3-2
GRN
PIN 3
t3
c
J3-3
RED
PIN
4
a3
$
J3-4
BLK
PIN
2
33
33
NOTE: Connect
cable
bare
shield
wire
to
cable
BLK
wire
at
DPU
and
snip
off shield
wire
excess
at
sensor
end.
s010002 REv
F
VMl0ll0 OWNERS
MANUAL