Rotax 915 i A series Maintenance Manual page 436

Step Procedure
1 Follow the aircraft manufacturer's instruc-
tions for assembly.
2 Plug the respective wiring harness con-
nector into the pressure control sensor.
3 Lock connector with tab.
Figure 18.43
Pressure control
1
valve
AMBIENT AIR PRESSURE/
TEMPERATURE SENSOR (AAPTS) —
INSTALLATION
Procedure
Step
1
Follow the aircraft manufacturer's instruc-
tions for assembly.
2 Plug the respective wiring harness con-
nector into the corresponding pressure or
temperature sensor. See
00 section Wiring harness (main
76–70–00
Page 28
August 01 2018
BRP-Rotax
MAINTENANCE MANUAL HEAVY
Chapter 76-50-
strand).
CYLINDER HEAD TEMPERATURE
SENSOR (CTS) — INSTALLATION
Step Procedure
1 Clean the thread of the cylinder head
temperature sensor.
2 Apply LOCTITE 243 to the thread of CTS
and use an 19 mm socket wrench part
no. 876130 (or a similar tool) to tighten it.
Tightening torque 15 Nm (133 in. lb.).
3 Plug the respective wiring harness con-
nector into the corresponding tempera-
ture sensor. See
section Wiring harness (main
Figure 18.44
Cylinder head tem-
perature sensor
1
(CTS)
MANIFOLD TEMPERATURE SENSOR
(MATS) — INSTALLATION
Step Procedure
1 Clean the thread of the manifold tempera-
ture sensor.
2 Fasten the temperature sensor with the
connector bracket and sealing ring using
an 19 mm socket wrench part no. 876130
(or similar tool). Tightening torque 15 Nm
(133 in. lb.).
Chapter 76-50-00
strand).
Effectivity: 915 i A Series
Edition 0/Rev. 0