曝光台 注意防骗
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fuel-pump and move the hose clear of the
engine.
(41) Remove the cable ties that attach the fuel flow
divider drain to the engine mount and the ignition
harness.
Note the location of the ties!
(42) Disconnect the engine breather hose from the
accessory housing at the top of the engine.
Put caps on the breather hose and the
engine connection.
WARNING: DO NOT GET OIL ON YOU. OIL CAN CAUSE SKIN DISEASE.
(43) Disconnect the oil pipe at the top of the
accessory-housing.
Use a suitable container to catch the oil.
Put caps on the oil pipe and the
accessory-housing connection.
(44) Disconnect the oil pipe at the front of the oil
cooler.
Use a suitable container to catch the oil.
Put caps on the oil pipe and the oil
cooler.
(45) Disconnect the oil pipe for the oil pressure sensor
at the engine crank-case.
Remove spilt oil.
(46) Remove the cylinder-head temperature-probe
from the bottom of the cylinder head:
S Disconnect the electrical cables at the in-line
connectors.
S Remove the probe from its holder.
S Remove the cable-ties/P-clamps which hold
the cables for the cylinder-head temperature
probe in position.
Do this item for each cylinder-head
temperature-probe.
Note the location of the cable-ties/Pclamps.
AIRCRAFT
DA 40 Series
AMM
Power Plant
Detail Steps/Work Items Key Items/References
Doc # 6.02.01
Rev. 5 71-00-00 Page 211
20 Sep 2007
(47) Disconnect the electrical cables from these
components:
S The generator (5 cables).
S The starter motor (1 cable).
S Fuel pressure sensors (2 cables).
S Oil temperature sensor.
S Fuel flow sensor.
S RPM sensor.
Remove the P-clamps and cable-ties from the
right-hand side of the engine. Move the cables
clear of
At the in-line connector.
Note the locations of the P-clamps and
the cable-ties!
(48) Disconnect the manifold pressure pipe from the
No. 4 cylinder inlet manifold. Release the Pclamp
from the rear of the No. 4 cylinder head.
(49) Disconnect the earth cable from the engine:
S Remove the bolt and washer which attaches
the cable eye-end to the engine.
WARNING: DO NOT GO UNDER THE ENGINE WHILE IT IS HELD BY THE
ENGINE HOIST. IF THE HOIST FAILS, THE ENGINE CAN FALL AND
CAUSE INJURY TO PERSONS.
(50) Attach the engine hoist to the engine. At the top of the engine. At the lifting
shackles.
Note: The hoist must hold the weight of the engine. The weight of the engine is 150 kg
(330 lb). If the propeller and spinner are fitted the total weight is 172 kg (378 lb).
(51) Adjust the hoist to “take the weight” of the engine.
AIRCRAFT
Power Plant DA 40 Series
AMM
Page 212
20 Sep 2007 71-00-00 Doc # 6.02.01
Rev. 5
Bolt
Bolt
Cylindrical
Shock-Mount
Cylindrical
Shock-Mount
Spacer
Spacer
Engine Mount
Engine Mount
Conical
Shock-Mount
Conical
Shock-Mount
Engine
Engine
Washer
Washer
Self-Locking Nut
Self-Locking Nut
TOP SHOCK-MOUNT ASSEMBLY
BOTTOM SHOCK-MOUNT ASSEMBLY
Figure 5: Engine Shock Mounts
AIRCRAFT
DA 40 Series
AMM
Power Plant
Doc # 6.02.01
Rev. 5 71-00-00 Page 213
20 Sep 2007
Detail Steps/Work Items Key Items/References
(52) Remove the engine-mounting-bolts:
S Remove the nuts from the lower engine
mounting bolts.
S Pull the mounting bolts rearwards and clear
of the engine mount and remove the rear
shock mount rubber.
S Remove the nuts from the upper engine
mounting bolts.
S Pull the mounting bolts rearwards and clear
of the engine mount and remove the rear
shock mount rubber.
S Move the engine clear of the airplane.
S Lower the engine into the engine stand.
Remove the front shock mount rubber.
Make sure that when you move the
engine clear of the airplane that you do
not catch the engine on any of the
equipment around the engine mount.
(53) If necessary:
S Remove the oil pipe from the accessory
housing.
S Remove the fuel pipe from the inlet to the
engine driven fuel pump.
Note the orientation.
Put caps on the open connections.
Note the orientation.
AIRCRAFT
Power Plant DA 40 Series
AMM
Page 214
20 Sep 2007 71-00-00 Doc # 6.02.01
Rev. 5
3. Install the Engine (without the Engine Mount)
Note: If you install a new engine, you must do the engine break-in procedure after
installation. Refer to Paragraph 11.
A. Equipment
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钻石40系列AMM 3(17)
