823547A 2 SEAL KIT Mercury
1031203UB, 1031203UD, 1031207ZF, 1031312DB, 1040213YL, 1041312UB, 10432037D, 1043203DD, 1043203VD, 1043213DD, 1043302DD, 1043411DD, 1043412DB, 1043412DD, 1050302DB, 1050302FB, 1050302FD, 1050312FB, 1050411DD, 1050412DB, 1050412DD, 1050412FB, 1050412F
SEAL
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$72.95
25-03-2023
-: -
Lower Unit Seal Kit is Compatible with Chrysler Force 40 50 Hp 1995-1999 OEM# 823547A2
High Performace Quality OEM Style Gaskets. || Gaskets and seals meet OEM standards or higher. || PWC Engine brings Higher Quality for an awesome price!
High Performace Quality OEM Style Gaskets. || Gaskets and seals meet OEM standards or higher. || PWC Engine brings Higher Quality for an awesome price!
$76.26
10-07-2023
0.05[0.02] Pounds
-: -
GEARCASE SEAL KIT | GLM Part Number: 87514; Mercury Part Number: 823547A2
GLM Part Number: 87514; Mercury Part Number: 823547A2
GLM Part Number: 87514; Mercury Part Number: 823547A2
Compatible models:
Mercury entire parts catalog list:
- X-LONG COMPONENTS » 823547A 2
- GEAR HOUSING(PROPELLER SHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- X-LONG COMPONENTS » 823547A 2
- GEAR HOUSING(PROPELLER SHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- X-LONG COMPONENTS » 823547A 2
- GEAR HOUSING(PROPELLER SHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- X-LONG COMPONENTS » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 2.00:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- X-LONG COMPONENTS » 823547A 2
- GEAR HOUSING(PROPELLER SHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(2.00:1 GEAR RATIO) » 823547A 2
- JET COMPONENTS » 823547A 2
- GEAR HOUSING (PROPELLER SHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING (DRIVE SHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- JET COMPONENTS » 823547A 2
- GEAR HOUSING (PROPELLER SHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING (DRIVE SHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- JET COMPONENTS » 823547A 2
- GEAR HOUSING(PROPELLER SHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(DRIVESHAFT)(1.83:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, DRIVESHAFT - 2.41:1 GEAR RATIO » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 2.41:1 GEAR RATIO » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 2.41:1 GEAR RATIO » 823547A 2
- GEAR HOUSING, DRIVESHAFT - 2.41:1 GEAR RATIO » 823547A 2
- GEAR HOUSING(PROP SHAFT-2:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING(DRIVESHAFT-2:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING(PROP SHAFT-2:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING(DRIVESHAFT-2:1 GEAR RATIO) » 823547A 2
- GEAR HOUSING, PROPELLER SHAFT - 1.83:1 GEARRATIO-NON BIGFOOT » 823547A 2
- GEAR HOUSING, DRIVESHAFT - 1.83:1 GEAR RATIO - NON BIGFOOT » 823547A 2
Information:
Illustration 1 g02469917
Air inlet and exhaust system
(1) Aftercooler core
(2) Air filter
(3) Clean Emissions Module (CEM)
(4) Back pressure valve
(5) Turbocharger
(6) Wastegate actuator
(7) Exhaust cooler (NRS)
(8) Exhaust gas valve (NRS)
(9) Wastegate regulator The components of the air inlet and exhaust system control the quality of air and the amount of air that is available for combustion. The air inlet and exhaust system consists of the following components:
Air cleaner
Exhaust cooler (NRS)
Exhaust gas valve (NRS)
Turbocharger
Aftercooler
Inlet manifold
Cylinder head, injectors, and glow plugs
Valves and valve system components
Piston and cylinder
Exhaust manifold
Clean Emissions Module (CEM)Air is drawn in through the air cleaner into the air inlet of the turbocharger by the turbocharger compressor wheel. The air is compressed to a pressure of about 150 kPa (22 psi) and heated to about 120° C (248° F) before the air is forced to the aftercooler. As the air flows through the aftercooler the temperature of the compressed air lowers to about 55° C (131° F). Cooling of the inlet air assists the combustion efficiency of the engine. Increased combustion efficiency helps achieve the following benefits:
Lower fuel consumption
Increased power output
Reduced NOx emission
Reduced particulate emissionFrom the aftercooler, the air flows to the exhaust gas valve (NRS). A mixture of air and exhaust gas is then forced into the inlet manifold. Air flow from the inlet manifold to the cylinders is controlled by inlet valves. There are two inlet valves and two exhaust valves for each cylinder. The inlet valves open when the piston moves down on the intake stroke. When the inlet valves open, cooled compressed air from the inlet port is forced into the cylinder. The complete cycle consists of four strokes:
Inlet
Compression
Power
ExhaustOn the compression stroke, the piston moves back up the cylinder and the inlet valves close. The cool compressed air is compressed further. This additional compression generates more heat.Note: If the cold starting system is operating, the glow plugs will also heat the air in the cylinder.Just before the piston reaches the top center (TC) position, the ECM operates the electronic unit injector. Fuel is injected into the cylinder. The air/fuel mixture ignites. The ignition of the gases initiates the power stroke. Both the inlet and the exhaust valves are closed and the expanding gases force the piston downward toward the bottom center (BC) position.From the BC position, the piston moves upward. This initiates the exhaust stroke. The exhaust valves open. The exhaust gases are forced through the open exhaust valves into the exhaust manifold.
Illustration 2 g03706055
Typical example
The NOx Reduction System (NRS) operates with the transfer of the hot exhaust gas from the exhaust manifold to the exhaust cooler (7). The hot exhaust gas is cooled in the exhaust cooler. The now cooled exhaust gas passes through the assembly of exhaust gas valve.The reed valves that are located in the exhaust gas valve (NRS) has one main function. The one main function is to prevent the reverse flow of charge air from the inlet side of the engine to the exhaust side of the engine.As the electronically controlled valve (8) starts to open the flow of cooled exhaust gas from the exhaust cooler (7) mixes with the air flow from the charge air aftercooler. The mixing of the cooled exhaust gas and the air flow from the charge air aftercooler reduces the oxygen content of the gas mixture. This results in a lower combustion temperature, so decreases the production of NOx.As the demand for more cooled exhaust gas increases the electronically controlled valve opens further. The further opening of the valve increases the flow of cooled exhaust gas from the exhaust cooler. As the demand for cooled exhaust gas decreases, the electronically controlled valve closes. This decreases the flow of cooled exhaust gas from the exhaust cooler.Exhaust gases from the exhaust manifold enter the inlet of the turbocharger in order to turn the turbocharger turbine wheel. The turbine wheel is connected to a shaft that rotates. The exhaust gases pass from the turbocharger through the following components: exhaust outlet, back pressure valve, Clean Emissions Module and exhaust pipe.Turbocharger
Illustration 3 g00302786
Typical example of a cross section of a turbocharger
(1) Air intake
(2) Compressor housing
(3) Compressor wheel
(4) Bearing
(5) Oil inlet port
(6) Bearing
(7) Turbine housing
(8) Turbine wheel
(9) Exhaust outlet
(10) Oil outlet port
(11) Exhaust inlet The turbocharger is mounted on the outlet of the exhaust manifold. The exhaust gas from the exhaust manifold enters the exhaust inlet (11) and passes through the turbine housing (7) of the turbocharger. Energy from the exhaust gas causes the turbine wheel (8) to rotate. The turbine wheel is connected by a shaft to the compressor wheel (3).As the turbine wheel rotates, the compressor wheel is rotated. The rotation of the compressor wheel causes the intake air to be pressurized through the compressor housing (2) of the turbocharger.
Illustration 4 g03706081
Typical example
(12) Wastegate actuator
(13) Actuating lever
(14) Line (boost pressure)
Illustration 5 g02151895
Typical example
(15) Wastegate regulator When the load on the engine increases, more fuel is injected into the cylinders. The combustion of this additional fuel produces more exhaust gases. The additional exhaust gases cause the turbine and the compressor wheels of the turbocharger to turn faster. As the compressor wheel turns faster, air is compressed to a higher pressure and more air is forced into the cylinders. The increased flow of air into the cylinders allows the fuel to be burnt with greater efficiency. This produces more power.A wastegate is installed on the turbine housing of the turbocharger. The wastegate is a valve that allows exhaust gas to bypass the turbine wheel of the turbocharger. The operation of the wastegate is dependent on the pressurized air (boost pressure) from the turbocharger compressor. The boost pressure acts on a diaphragm that is spring loaded in the wastegate actuator which varies the amount of exhaust gas that flows into the turbine.The wastegate regulator (15) is controlled by the engine Electronic Control Module (ECM). The ECM uses inputs from a number of engine sensors to determine the optimum boost pressure. This will achieve the best exhaust emissions and fuel consumption at any given engine operating condition. The ECM
Parts seal Mercury:
43023 2
43023 2 SEAL
1075217DD, 1075217FD, 1075217PD, 1075217VD, 10752L7DF, 10752L7FF, 1075317DB, 1075317FB, 1075412DB, 1075412DD, 1075412DN, 1075412FB, 1075412FY, 1075D73FY, 1075D73HY, 1090412DB, 1090412DC, 1090412DD, 1090412DN, 1090412DY, 1090412FF, 1090412FY, 1090422D
878431
825238002
825238002 SEAL
1A40302FD, 1A40311FZ, 1A41412ZB, 1A41452EZ, 1A41452FU, 1A51411HZ, 1A51412HZ, 1A51452EZ, 1A60412HZ, 1A60452EZ, 1A60452HZ, 1B25203ZB, 1E60452HB, 1F30203ZB, 1F40203FD, 1F40213FZ
42941001
42941001 SEAL, Water Tube
1031312DB, 1043203DD, 1043213DD, 1043302DD, 1043411DD, 1043412DB, 1043412DD, 1050302DB, 1050302FB, 1050302FD, 1050312FB, 1050411DD, 1050412DB, 1050412DD, 1050412FB, 1050412FD, 1055207DB, 1115412DB, 1A30302ZB, 1A40302FD, 1A40311FZ, 1A41412ZB, 1A41452E
822424001
822424001 SEAL, Throttle Cable
1031312DB, 1043203DD, 1043213DD, 1043302DD, 1043411DD, 1043412DB, 1043412DD, 1050302DB, 1050302FB, 1050302FD, 1050312FB, 1050411DD, 1050412DB, 1050412DD, 1050412FB, 1050412FD
823572001
823572001 SEAL, Warning Horn
1031312DB, 1043203DD, 1043213DD, 1043302DD, 1043411DD, 1043412DB, 1043412DD, 1050302DB, 1050302FB, 1050302FD, 1050312FB, 1050411DD, 1050412DB, 1050412DD, 1050412FB, 1050412FD
822395001
822395001 SEAL, Exhaust Tube
1031312DB, 1043203DD, 1043213DD, 1043302DD, 1043411DD, 1043412DB, 1043412DD, 1050302DB, 1050302FB, 1050302FD, 1050312FB, 1050411DD, 1050412DB, 1050412DD, 1050412FB, 1050412FD
828495001
828495001 SEAL, Idle Relief
1043203DD, 1043213DD, 1043302DD, 1043411DD, 1043412DB, 1043412DD, 1050302DB, 1050302FB, 1050302FD, 1050312FB, 1050411DD, 1050412DB, 1050412DD, 1050412FB, 1050412FD