85-Maintenance Procedures
85-50-00 Reciprocating Engine – Liquid Cooling
1. Coolant Temperature Sensor
A. Remove the Coolant Temperature Sensor
Refer to the applicable Aircraft
Maintenance Manual.
Disconnect the electrical connector “CTS,
CTS_GPC”.
Remove the coolant temperature sensor from
the intake air manifold.
B. Install the Coolant Temperature Sensor
Refer to Section 85-30-00 Paragraph 1 for the exploded view of the intake
air system.
Tighten the coolant temperature sensor.
Torque 15 Nm.
Refer to Fig. 85 - 90.
Connect the electrical connector “CTS,
CTS_GPC”.
Fill and bleed the coolant system.
Refer to the applicable Aircraft
Maintenance Manual.
Refer to Section 71-00-01.
Examine the coolant system for leakage.