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(9) Release the tension on the hoist.
(10) Disconnect the hoist. Remove the sling from
the engine.
(11) Install the heat shield bracket to the engine.
− Install the two spring washers and two
screws.
− Tighten the screws.
WARNING: DO NOT GET FUEL ON YOU. FUEL CAN CAUSE SKIN DISEASE.
DO NOT ALLOW FIRE NEAR FUEL. FIRE BURNS AND CAN
CAUSE INJURY TO PEOPLE AND DAMAGE TO EQUIPMENT.
(12) Attach the fuel feed hose to the fuel pump
inlet.
− Tighten the fuel pipe connector.
Torque to 30.5 Nm (270 in lbs)
(13) Attach the fuel return hose to the fuel pump
outlet.
− Tighten the fuel pipe connector.
Torque to 15.2 Nm (135 in lbs)
(14) For aircraft fitted with a manifold valve fuel
return hose, attach the fuel return hose to
the manifold valve return port.
− Tighten the fuel pipe connector.
Torque to 15.2 Nm (135 in lbs)
Power Plant
DA20-C1 AMM
Page 214
19 Dec 1997 71-00-00 Doc # DA201-C1
Rev. 0
Detail Steps/Work Items Key Items
(15) Install the shield to the right side of the aft
baffle.
(16) Install the engine exhaust system. Refer to Chapter 78
(17) Attach the vacuum hose to the firewall
connector. Install the worm drive clamp:
− Tighten the worm drive clamp.
(18) Attach the engine ground cable to the bottom
of the blanking plate on the engine
accessory housing.
− Tighten the bolt.
Refer to the TCM Maintenance Manual for
the torque value.
(19) Install the tachometer drive shaft.
− Put the flexible drive shaft into the
engine accessory case at the attachment
point.
− Install the knurled nut to the accessory
case housing.
WARNING: DO NOT GET OIL ON YOU. OIL CAN CAUSE SKIN DISEASE.
(20) Connect the inlet and outlet oil hoses to the
oil cooler. Tighten the two connections.
Torque to 40.67 Nm (360 in lbs)
(21) Install the flexible pipe between the oil cooler
and the aft baffle. Install the worm drive
clamps to the oil cooler and to the aft baffle.
Tighten the clamps.
Note: If the generator has been removed, refer to Chapter 24-20 for the installation
procedure.
Note: If the engine baffles have been removed, refer to Chapter 75 for the
installation procedure.
DA20-C1 AMM
Power Plant
Doc # DA201-C1
Rev. 0 71-00-00 Page 215
19 Dec 1997
Detail Steps/Work Items Key Items
(22) Attach the engine electrical cables to these
components:
− The oil temperature sensor.
− The oil pressure sensor.
− The cylinder head temperature (CHT)
sensor.
− The events (hours meter) switch.
− The fuel pressure sensor.
− The exhaust gas temperature (EGT)
sensor.
− The starter motor. (One cable).
− The generator (Two cables).
− Attach the electrical cable P clips.
(23) Install the P-clip that attaches the fuel pump
and cylinder drain pipes to the firewall.
(24) Cut the locking wire from the oil sump drain
plug:
− Remove the oil sump drain plug.
− Drain the preservation oil from the oil
sump into a correct oil container.
(25) Install the oil sump drain plug.
− Tighten the oil sump drain plug.
− Lock the plug with wire.
Torque 21.4-23.7 Nm (190-210 in lbs)
CAUTION: USE ONLY THE CORRECT ENGINE OILS. REFER TO THE
TELEDYNE CONTINENTAL MAINTENANCE MANUAL FOR THE
CORRECT ENGINE OIL SPECIFICATIONS. IF YOU DO NOT USE
THE CORRECT ENGINE OIL, THE ENGINE CAN BE DAMAGED.
(26) Fill the engine oil system with the correct
specification engine oil.
Refer to the Teledyne Continental
Maintenance Manual for the correct oil
specification and quantity.
(27) Install the flexible pipe between the muffler
and the cabin heat control valve.
− Install the worm drive clamp to the
muffler.
− Tighten the clamp.
Power Plant
DA20-C1 AMM
Page 216
23 Jun 2004 71-00-00 Doc # DA201-C1
Rev.10
Detail Steps/Work Items Key Items
(28) Put the mixture control cable in position
through the rubber grommet at the aft baffle.
(29) Install the mixture control cable into the
support bracket at the front of the engine.
For aircraft with a standard fuel pump:
− Install the rear adjusting nut to the
control cable.
− Put the control cable in position through
the bracket.
− Install the forward adjusting nut to the
control cable.
For aircraft with an altitude compensating
fuel pump:
− Insert the end of the mixture control
　
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