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CAUSE INJURY TO PEOPLE AND DAMAGE TO EQUIPMENT.
(14) Disconnect the inlet and return fuel hoses
from the injector fuel pump.
For aircraft fitted with a manifold valve fuel
return hose, remove the fuel return hose
from the manifold valve.
Put caps on the two fuel hoses. And put
caps on the two injector fuel pump
connections. This will stop contamination
going into the fuel system.
Put caps on the fuel hose and manifold
valve connector.
Power Plant
DA20-C1 AMM
Page 206
19 Dec 1997 71-00-00 Doc # DA201-C1
Rev. 0
Figure 4: Connections On The Left Of The Engine (2)
DA20-C1 AMM
Power Plant
Doc # DA201-C1
Rev. 11 71-00-00 Page 207
28 June 2005
Detail Steps/Work Items Key Items
WARNING: DO NOT GET OIL ON YOU. OIL CAN CAUSE SKIN DISEASE.
(15) Remove the P-clip that attaches the fuel
pump and cylinder drain pipes to the firewall.
(16) Remove the two worm drive clamps from the
flexible pipe between the oil cooler and the
aft baffle. Remove the flexible pipe.
(17) Disconnect the inlet and return oil pipes from
the oil cooler.
Put caps on the two oil hoses. And put
caps on the two oil cooler connections.
This will stop contamination going into the
oil system.
(18) Disconnect the vacuum hose from the
firewall connection:
Put a cap on the firewall adapter. And put
a cap on the vacuum feed hose. This will
stop contamination going into the vacuum
system.
(19) Item deleted.
(20) Remove the shield from the right side of the
aft baffle.
− Remove the manifold fuel pressure hose
clear of the aft baffle/engine.
(21) Remove the two worm drive clamps from the
flexible pipe between the muffler and the
cabin heat control valve.
− Remove the flexible pipe.
(22) Remove the engine exhaust system.
− Remove the eight nuts from the four
exhaust port flanges.
Discard the nuts.
Refer to Chapter 78-00.
(23) Remove the heat shield from the right side of
the engine.
− Remove the two screws and spring
washers from the two brackets at the
cylinder heads.
− Remove the heat shield with fuel pipes
and electrical cables attached.
− Move the heat shield clear of the engine.
Power Plant
DA20-C1 AMM
Page 208
24 Mar 1999 71-00-00 Doc # DA201-C1
Rev. 1
Figure 5: Connections On The Right Of The Engine
Rear Lifting Eye
Front Lifting Eye
Throttle Cable
Bracket
Throttle Cable
P-Clamp
Throttle Cable
Connection Generator
Control Cables
Generator
Power Cable
P-Clips Holding Fuel Pipes
And Electrical Cables
Spark-Plug Leads
Heat Shield
Heat Shield
Attaching Screws
Vacuum
Pipe
Starter Power Cable
DA20-C1 AMM
Power Plant
Doc # DA201-C1
Rev. 10 71-00-00 Page 209
23 Jun 2004
Detail Steps/Work Items Key Items
(24) Disconnect the throttle control cable from the
throttle and metering unit lever:
− Remove the nut.
− Remove the bolt.
− Remove the three washers.
− Move the control cable clear of the
engine.
(25) Remove the control cable from the bracket at
the top of the plenum assembly:
− Remove the adjusting nut from the front
of the control cable.
− Move the throttle control cable clear of
the bracket.
− Remove the rear adjusting nut from the
control cable.
(26) Move the throttle control cable clear of the
engine.
− Release the P-clamp holding the cable to
the engine mounting frame.
− Carefully pull the throttle control cable
through the rubber grommet at the aft
baffle.
(27) Disconnect the mixture control cable from
fuel mixture control lever:
− Loosen the stiff nut.
− Remove the control cable from the
mixture control lever.
(28) Disconnect the mixture control cable from
the front support bracket.
For aircraft with a standard fuel pump:
− Remove the adjusting nut from the front
of the control cable.
− Move the throttle control cable clear of
the bracket.
− Remove the rear adjusting nut from the
control cable.
For aircraft with an altitude compensating
fuel pump:
− Remove the nuts, washers and screws
that fasten the mixture cable keeper to
the bracket.
− Remove the mixture cable keeper.
− Remove the mixture control cable from
the front support bracket.
Power Plant
DA20-C1 AMM
Page 210
　
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本文鏈接地址：鉆石20系列AMM 2(71)