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(2)  Remove the pressure cap from the coolant tank: S Turn the cap counter-clockwise a small distance to release the pressure. S When the pressure has fully released, turn the cap fully counter-clockwise. 
(3)  Drain the coolant: S Remove the drain plug from the left side of the coolant radiator near the bottom. S Open the drain plug on the engine RH lower side above the turbo-charger. S Close the coolant drain plug above the turbo-charger. S Install the drain plug to the coolant radiator.  Use a suitable container to catch the coolant. You need not remove this drain plug. Use a suitable duct to guide the coolant into the container. Use a new copper gasket. 
(4)  Visually check the coolant for oil.  No oil allowed in coolant. 

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DA 40 Series

Detail Steps/Work Items  Key Items/References 
CAUTION: USE ONLY THE CORRECT COOLANT. REFER TO CHAPTER 2 OF THE AIRPLANE FLIGHT MANUAL FOR THE CORRECT COOLANT SPECIFICATIONS. IF YOU DO NOT USE THE CORRECT COOLANT, THE ENGINE CAN BE DAMAGED. 
(5)  Fill the cooling system: S Open the bleed points on the cabin heat pipes. S Add coolant to the coolant tank. S When coolant comes from the bleed points without air bubbles, close the bleed points. S Install the cap to the coolant tank.  Allow time for the coolant to move through the system. 
(6)  Do a ground run-up: S Let the coolant temperature rise up to the point where the coolant flows from the thermostat valve through the main circuit. S After shut-down, check for leaks.  To circulate and remove air. Repair any leaks. 
(7)  Let the engine cool down. 
WARNING: DO NOT REMOVE THE PRESSURE CAP FROM THE COOLANT TANK IF THE ENGINE IS HOT. THE PRESSURE IN THE SYSTEM CAN FORCE HOT COOLANT TO COME OUT AND BURN YOU. 
(8)  Remove the pressure cap from the coolant tank: S Turn the cap counter-clockwise a small distance to release the pressure. S When the pressure has fully released, turn the cap fully counter-clockwise. 
(9)  Check coolant level. Repeat items (5) to (8) until the system is completely de-aerated and full. 
(10)  Install the cap to the coolant tank. 
(11)  Install the engine cowlings.  Refer to Section 71-11. 

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AMM

7. Brake System
The brake fluid reservoirs are located on the brake master cylinders on the co-pilot’s side. You get access in the cockpit below the instrument panel.
WARNING:  DO NOT GET BRAKE FLUID ON YOUR SKIN OR IN YOUR MOUTH. BRAKE FLUID CAN CAUSE DISEASE. 
CAUTION:  REMOVE SPILLED BRAKE FLUID IMMEDIATELY. BRAKE FLUID CAN CAUSE DAMAGE TO PAINT AND OTHER MATERIALS. 

A. Fill the Brake System Reservoirs
Detail Steps/Work Items  Key Items/References 
(1)  Clean the top of the brake fluid reservoir and filler cap. 
(2)  Remove the filler cap. 
(3)  Fill the reservoir to the correct level.  Use only MIL-H-5606A hydraulic fluid. 12 to 25 mm (0.5 to 1 in.) below the top of the filler hole. 
(4)  Install the filler cap. 

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8. Tires
The DA 40 has these tires: Main tires: 6.00 x 6, 6PR, 120 mph, TSO C62; pressure 2.5 bar (36 psi). Nose tire: 5.00 x 5, 6PR, 120 mph, TSO C62; pressure 2.0 bar (29 psi).
A. Examine the Tires and Measure the Pressure
　
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