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FLIGHT DESIGN CT - Chapter 75 - Cooling; 75-00.1 General; 75-00.2 Description

FLIGHT DESIGN CT
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Document Title Document No. Revision
Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS
AF 0480 0011 00 05-Aug-12 75-00-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
CHAPTER 75 – COOLING
Contents
75-00.1 General
75-00.2 Description
75-00.3 Maintenance Practices
75-00.3.1 Cooling Inspection
75-00.3.2 Cooling Hoses and Lines Replacement
75-00.1 General
This chapter provides description and information concerning maintenance of engine
cooling.
75-00.2 Description
The engine is provided with liquid cooling. The coupled water and oil radiators are installed
in front of the engine just behind the air-inlet. The fresh air flow through the radiators
enclosure and cool down coolant liquid and oil. An optional water thermostat can be
included to the system to further stabilize engine temperatures.
Fig. 75-00-1 Cooling system diagram without thermostat

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