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20 Sep 2007
5. Fill and Bleed the Cooling System
Detail Steps/Work Items Key Items/References
(1) 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.
(2) 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.
(3) 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.
(4) 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.
(5) Check coolant level. Repeat items (1) to (4) until
the system is completely de-aerated and full.
(6) Install the cap to the coolant tank.
(7) Install engine cowlings. Refer to Section 71-11.
AIRCRAFT
Cooling DA 40 Series
AMM
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DA 40 Series
AMM
Engine Controls
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CHAPTER 76
ENGINE CONTROLS
AIRCRAFT
Engine Controls DA 40 Series
AMM
Page 2
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DA 40 Series
AMM
Engine Controls
Doc # 6.02.01
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TABLE OF CONTENTS
CHAPTER 76
ENGINE CONTROLS
Section 76-00
Engine Controls - Lycoming Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description and Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
Trouble-Shooting
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Install the Throttle Bowden Cable . . . . . . . . . . . . . . . . . . 201
3. Remove/Install the Mixture Bowden Cable . . . . . . . . . . . . . . . . . . 207
4. Throttle/Mixture Control Range of Movement Test . . . . . . . . . . . . 213
Section 76-01
Engine Controls - TAE 125 Diesel Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description and Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Trouble-Shooting
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101
AIRCRAFT
Engine Controls DA 40 Series
AMM
Page 2
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Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Install the Power Lever . . . . . . . . . . . . . . . . . . . . . . . . . . 201
3. Remove/Install the ECU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 205
4. Remove/Install the Engine Control System Harness . . . . . . . . . . 207
AIRCRAFT
DA 40 Series
AMM
Engine Controls
Doc # 6.02.01
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20 Sep 2007
CHAPTER 76
ENGINE CONTROLS
Section 76-00
Engine Controls - Lycoming Engine
1. General
This Section tells you about the DA 40 engine controls for airplanes with the Lycoming engine
installed. Bowden cables transmit the control inputs to the engine. For data on the propeller control
system refer to Section 61-20.
Figure 1 shows the engine control assembly.
This Chapter gives you data on the linkages cables and levers. It does not include data on the fuel
control units themselves. For data on the engine fuel-control unit refer to the Lycoming Maintenance
Manual. For data on the alternate air unit refer to Section 71-60.
The DA 40 has these engine controls:
) Throttle control lever.
) Mixture control lever.
AIRCRAFT
Engine Controls DA 40 Series
AMM
Page 2
20 Sep 2007 76-00-00 Doc # 6.02.01
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Throttle Bowden
Cable
Mixture Bowden
Cable
Throttle Friction Adjuster
　
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