Rotax 915 i A series Maintenance Manual page 418

Step Procedure
1 Push in the tab on the top of the connec-
tor and at the same time pull the connec-
tor out of the connection socket.
2 Follow the aircraft manufacturer's instruc-
tions for disassembly.
Figure 18.8
Pressure/temperature
1
sensor
PRESSURE CONTROL VALVE (PCV) –
REMOVAL
Installation position: Aircraft frame
Step Procedure
1 Lift the latch, press and pull out the
connector.
2
Follow the aircraft manufacturer's instruc-
tions for disassembly.
3 For removal of the hoses, see Chapter
73-10-00 section
hoses - removal.
76–70–00
Page 10
August 01 2018
BRP-Rotax
MAINTENANCE MANUAL HEAVY
2
Connection socket
Pressure control valve
Figure 18.9
Pressure control
1
valve (PCV)
MANIFOLD TEMPERATURE SENSOR
(MATS_1+MATS_2) — REMOVAL
Installation position: Airbox.
Step Procedure
1
Cut open the cable ties.
2 Unplug the relevant connector of the wir-
ing harness from the corresponding mani-
fold temperature sensor (MATS).
See Chapter
ness (main strand).
76-50-00 section Wiring har-
Effectivity: 915 i A Series
Edition 0/Rev. 0