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(3) Carefully move the engine end of the harness
forward through the firewall.
Take care not to damage the
connectors. Adjust the harness position
so that all connections can be made
without stress.
AIRCRAFT
Engine Controls DA 40 Series
AMM
Detail Steps/Work Items Key Items/References
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Rev. 5
(4) Connect the engine wire harness and bonding
cables to these electrical sensors:
S Crankshaft 1.
S Crankshaft 2.
S Camshaft 1.
S Camshaft 2.
S Coolant temperature.
S Oil temperature.
S Oil pressure.
S Manifold air temperature.
S Fuel rail pressure regulator.
S Fuel rail pressure sensor.
S Propeller governor.
S Gear temperature.
S Waste gate valve solenoid.
S Fuel injectors.
S Glow plugs.
S Waste gate control valve.
At the front right crank case.
At the front left crank case.
On inlet valve cover between cyl. 3 & 4.
On inlet valve cover between cyl. 1 & 2.
At the thermostat valve.
At the bottom of the oil case.
At the rear side of the oil filter housing.
On the intercooler outlet pipe.
At the rear end of the fuel rail.
At the front side of the fuel rail.
At the right side of the reduction gear.
At top left of front bearing reduction gear.
At the lower crankshaft cover.
At each fuel injector.
At the lower crankshaft cover.
At the lower crankshaft cover.
(5) Connect the harness at these terminal blocks:
S Glow.
S ECU Bus.
S Instruments and Annunciator Panel.
Behind the instrument panel.
(6) Connect the 2 electrical connectors to the ECU. Refer to Figure 3. Under the left pilot's
seat. Make sure that the bayonet
lockings are engaged.
AIRCRAFT
DA 40 Series
AMM
Engine Controls
Detail Steps/Work Items Key Items/References
Doc # 6.02.01
Rev. 5 76-01-00 Page 213
20 Sep 2007
(7) Install the cable-ties and clamps that attach the
cable harness to the engine and structure.
Refer to the notes that you made during
removal for the type and location of
each attachment.
(8) Install the shields for the feed-through at the
firewall.
Seal with PR 812 or equivalent.
(9) Install the coolant radiator. Refer to Section 75-01.
(10) Install the power lever. Refer to Paragraph 2.C.
(11) Install the instrument panel cover. Refer to Section 25-10.
(12) Install the left pilot’s seat. Refer to Section 25-10.
(13) Connect the airplane main battery. Refer to Section 24-34
(14) Install the engine cowlings. Refer to Section 71-11.
(15) Do an engine run-up. Refer to Section 71-01.
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Engine Controls DA 40 Series
AMM
Page 214
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AIRCRAFT
DA 40 Series
AMM
Engine Indicating
Doc # 6.02.01
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20 Sep 2007
CHAPTER 77
ENGINE INDICATING
AIRCRAFT
Engine Indicating DA 40 Series
AMM
Page 2
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AIRCRAFT
DA 40 Series
AMM
Engine Indicating
Doc # 6.02.01
Rev. 5 77-CONTENTS Page 1
20 Sep 2007
TABLE OF CONTENTS
CHAPTER 77
ENGINE INDICATING
Section 77-00
Engine Indicating - Lycoming Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Section 77-01
Engine Instrumentation - TAE 125 Diesel Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description and Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Section 77-40
Integrated Engine Indication - Lycoming Engine
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2. Description/Operation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
Trouble-Shooting
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 101
Maintenance Practices
1. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 201
2. Remove/Install the Indicator Panel . . . . . . . . . . . . . . . . . . . . . . . . 201
3. Replace an Engine Indicator Gauge Sensor/Transducer . . . . . . . 202
AIRCRAFT
Engine Indicating DA 40 Series
AMM
Page 2
20 Sep 2007 77-CONTENTS Doc # 6.02.01
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Section 77-41
Engine Integrated Instrument System - TAE 125 Diesel Engine
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钻石40系列AMM 3(83)
