0344200 EVINRUDE PROPELLER SHAFT ASSY.


0344200 PROPELLER SHAFT ASSY. EVINRUDE BE5FRBECC, BE5FRBEUS, BE6DRECR, BE8RCLT, E5DRECR, E5R4EEM, E5R4EEM, E5R4SIE, E5R4SIE, E5R4SSB, E5R4SSB, E6R4EEM, E6R4SIE, E6R4SSB, E8DREEA, E8DRSSM, E8RECR, E8WREES, E8WRLSIR, E8WRLSSC, HE6FRECA, HE6FREUR PROPELLER
0344200 PROPELLER SHAFT ASSY. EVINRUDE
Rating:
98

Buy PROPELLER SHAFT ASSY. 0344200 EVINRUDE genuine, new aftermarket parts with delivery
Number on catalog scheme: 9
 

BRP EVINRUDE entire parts catalog list:

BE5FRBECC, BE5FRBLECC, HE5FRECA, HE5FRLECA 1998
BE5FRBEUS, BE5FRBLEUS, HE5FREUR, HE5FRLEUR 1997
BE6DRECR, BE6DRLECR, E6RECR, E6RLECR 1998
BE8RCLT, BE8RCT 1998
E5DRECR, E5DRLECR 1998
E5R4EEM, E5RB4EER, E5RBL4EER, E5RL4EEM, E6R4EEM, E6RL4EEM 1999
E5R4EEM, E5RB4EER, E5RBL4EER, E5RL4EEM 1999
E5R4SIE, E5RL4SIE, E6R4SIE, E6RL4SIE 2001
E5R4SIE, E5RL4SIE 2001
E5R4SSB, E5RL4SSB, E6R4SSB, E6RL4SSB 2000
E5R4SSB, E5RL4SSB 2000
E6R4EEM, E6RL4EEM 1999
E6R4SIE, E6RL4SIE 2001
E6R4SSB, E6RL4SSB 2000
E8DREEA 1999
E8DRSSM 2000
E8RECR, E8RLECR, E8SRLECA 1998
E8WREES, E8WRLEES 1999
E8WRLSIR, E8WRSIR 2001
E8WRLSSC, E8WRSSC 2000
HE6FRECA, HE6FRLECA 1998
HE6FREUR, HE6FRLEUR 1997

Information:

Visual Inspection
Inspect the following parts at each oil change:
Air lines
Hoses
Gasket joints
Pressurized air can cause personal injury. When pressurized air is used for cleaning, wear a protective face shield, protective clothing, and protective shoes.
Ensure that the constant torque hose clamps are tightened to the correct torque. Refer to Specifications, SENR3130, "Torque Specifications" in order to locate the proper torque. Check the welded joints for cracks. Ensure that the brackets are tightened in the correct positions. Ensure that the brackets are in good condition. Use compressed air to clean any debris or any dust from the aftercooler core assembly. Inspect the fins in the aftercooler core for the following conditions:
Damage
Debris
CorrosionUse a stainless steel brush to remove any corrosion.Note: When parts of the air-to-air aftercooler system are repaired or replaced, a leak test is recommended.Inlet Manifold Pressure
Normal inlet manifold pressure with high exhaust temperature can be caused by blockage of the fins of the aftercooler core. Clean the fins of the aftercooler core. Refer to "Visual Inspection" under this topic for the cleaning procedure.Low inlet manifold pressure and high exhaust manifold temperature can be caused by any of the following conditions:Plugged air cleaner - Clean the air cleaner or replace the air cleaner, as required. Refer to the Operation and Maintenance Manual, "Engine Air Cleaner Element - Clean/Replace".Blockage in the air lines - Blockage in the air lines between the air cleaner and the turbocharger must be removed.Aftercooler core leakage - Aftercooler core leakage should be pressure tested. Refer to "Aftercooler Core Leakage" under this topic for the testing procedure.Inlet manifold leak - An inlet manifold leak can be caused by the following conditions: loose fittings and plugs, missing fittings and plugs, damaged fittings and plugs and leaking inlet manifold gasket.Aftercooler Core Leakage
Illustration 1 g01134323
FT-1984 Aftercooler Testing Group
(1) Regulator and valve assembly
(2) Nipple
(3) Relief valve
(4) Tee
(5) Coupler
(6) Aftercooler
(7) Dust plug
(8) Dust plug
(9) Chain A low power problem in the engine can be the result of aftercooler leakage. Aftercooler system leakage can result in the following problems:
Low power
Low boost pressure
Black smoke
High exhaust temperature
Remove all air leaks from the system to prevent engine damage. In some operating conditions, the engine can pull a manifold vacuum for short periods of time. A leak in the aftercooler or air lines can let dirt and other foreign material into the engine and cause rapid wear and/or damage to engine parts.
A large leak of the aftercooler core can often be found by making a visual inspection. To check for smaller leaks, use the following procedure:
Disconnect the air pipes from the inlet and outlet side of the aftercooler core.
Dust plug chains must be installed to the aftercooler core or to the radiator brackets to prevent possible injury while you are testing. Do not stand in front of the dust plugs while you are testing.
Install couplers (5) on each side of the aftercooler core. Also, install dust plugs (7) and (8). These items are included with the FT-1984 Aftercooler Testing Group.Note: Installation of additional hose clamps on the hump hoses is recommended in order to prevent the hoses from bulging while the aftercooler core is being pressurized.
Do not use more than 240 kPa (35 psi) of air pressure or damage to the aftercooler core can be the result.
Install the regulator and valve assembly (1) on the outlet side of the aftercooler core assembly. Also, attach the air supply.
Open the air valve and pressurize the aftercooler to 205 kPa (30 psi). Shut off the air supply.
Inspect all connection points for air leakage.
The pressure in the aftercooler system should not drop more than 35 kPa (5 psi) in 15 seconds.
If the pressure drop is more than the specified amount, use a solution of soap and water to check all areas for leakage. Look for air bubbles that will identify possible leaks. Replace the aftercooler core, or repair the aftercooler core, as needed.
To help prevent personal injury when the tooling is removed, relieve all pressure in the system slowly by using an air regulator and a valve assembly.
After the testing, remove the FT-1984 Aftercooler Testing Group. Reconnect the air pipes on both sides of the aftercooler core assembly. Air System Restriction
Pressure measurements should be taken at the inlet manifold and the turbocharger outlet.Use the differential pressure gauge of the 1U-5470 Engine Pressure Group. Use the following procedure in order to measure the restriction of the aftercooler:
Connect the vacuum port of the differential pressure gauge to a port on the inlet manifold.
Connect the pressure port of the differential pressure gauge to a port on the turbocharger outlet.
Record the value. The air lines and the cooler core must be inspected for internal restriction when both of the following conditions are met:
Air flow is at a maximum level.
Total air pressure drop of the charged system exceeds 13.5 kPa (4 in Hg) for engines with a 14.6 L (890 cu in) displacement.
Total air pressure drop of the charged system exceeds 15.2 kPa (4.5 in Hg) for engines with a 15.8 L (964 cu in) displacement.If a restriction is discovered, proceed with the following tasks, as required:
Clean
Repair
ReplacementTurbocharger Failure


Parts propeller EVINRUDE:

0391096
 
0391096 PROPELLER
BE4RDHEDS, BE5DREDS, BE5DREUC, BE5FRBECC, BE5FRBEUS, BE6DRECR, BE6DREDS, BE6DREUC, BE8RCB, BE8RCH, BE8RCLT, BE8REDS, E4RDHCCS, E4RDHCDE, E4RDHCEC, E4RDHCUD, E4RDHEIA, E4RDHENM, E4RDHEOD, E4RDHERE, E4RDHESR, E4RDHETB, E5DRECR, E5R4EEM, E5R4EEM, E5R4SI
0390237
PROPELLER
0390237 PROPELLER
BE5DREDS, BE5DREUC, BE5FRBECC, BE5FRBEUS, BE6DRECR, BE6DREDS, BE6DREUC, BE8RCB, BE8RCH, BE8RCLT, BE8REDS, E5DRECR, E5R4EEM, E5R4EEM, E5R4SIE, E5R4SIE, E5R4SSB, E5R4SSB, E5RCIC, E5RCSS, E5RHCNR, E5RHCTA, E6R4EEM, E6R4SIE, E6R4SSB, E6RCCS, E6RCDE, E6RC
0392183
 
0392183 PROPELLER, (srl model only)
BE5DREDS, BE5DREUC, BE5FRBECC, BE5FRBEUS, BE6DRECR, BE6DREDS, BE6DREUC, BE8RCB, BE8RCH, BE8RCLT, BE8REDS, E5DRECR, E5R4EEM, E5R4EEM, E5R4SIE, E5R4SIE, E5R4SSB, E5R4SSB, E5RHCNR, E5RHCTA, E6R4EEM, E6R4SIE, E6R4SSB, E6RCCS, E6RCDE, E6RCEC, E6RCOB, E6RC
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