C. Fuel Pressure Transducer Installation:
Find a convenient location on the rewall and mount the pressure
transducer with the clamp provided. Do not mount the pressure
transducer to an engine bae or directly on the engine with the
transducer supported by an adapter or tting. Vibration can cause
the adapter to break, resulting in loss of engine oil. The pressure
transducer is equipped with an 1/8" NPT male port. This port can be
adapted to any oil pressure line. Use only a exible hose and ttings
suitable for aircraft use. Route a exible oil pressure line from the
primary oil pressure pick-up point to the pressure transducer and
tighten all ttings. Do not use the case of the pressure transducer
to tighten the pressure ttings.
D. Gyro Vacuum Pressure Transducer Installation:
Mount the PT-05Di Pressure
Transducer on the inside
rewall or in the equipment
bay under the aircraft
instrument panel. Use the
holes in the bottom plate to
mount the PT-05Di. Only
two mounting holes are
required.
Connect the aircraft gyro vacuum line to the port tagged "Vac" on the PT-05Di. Leave the port tagged
"Press" open for non-pressurized aircraft. On pressurized aircraft connect the port tagged "Press" to the
gyro overboard pressure line. Be sure these lines are tight. The ports are 1/4" are union. Care should be
taken not to put excess pressure on the exible lines. Make sure the exible lines do not kink.
E. Airspeed Transducer Installation:
Mount the PT-05Di Pressure Transducer on the inside rewall or in the equipment bay under the aircraft
instrument panel. Use the holes in the bottom plate to mount the PT-05Di. Only two mounting holes are
required.
Connect the aircraft pitot (airspeed) line to the port tagged "Press" on the PT-05Di. Connect the aircraft
static pressure line to the port tagged "Vac" on the PT-05Di. Be sure these lines are tight. The ports are
1/4" are union. Care should be taken not to put excess pressure on the exible lines. Make sure the
exible lines do not kink. The Appendix at the back of the "Operating Instructions" manual provides
calibration instructions for Airspeed.
F. Altitude Transducer Installation:
Mount the PT-30Alt Altitude Transducer
on the inside rewall or in the equipment
bay under the aircraft instrument panel.
Use the holes in the bottom plate to mount
the PT-30Alt. Only two mounting holes are
required.
The PT-05Diff, Pressure
Transducer (0 to 6" Hg)
Open or Overboard
Pressure Line
Gyro Vacuum Line
Pressure
Vacuum
RED
BLK
GRN
WHT
To EDC
Press Input
(Top Connector)
RED
BLK
GRN
WHT
(TOP Connector)
EDC
Press Input
Aircraft Static
Line
.170" ID Flexible Tube
(Top Connector)
To EDC
Press Input
(RED)
(BLK)
(GRN)
(WHT)
Pressure Transducer
PT-30GA for 0-33 psi
PT-100GA for 0-110 psi
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