09450-00330 PUMP ASSY, INJECTI Denso Cross


 

Information pump assy, injecti

09450-00330 PUMP ASSY, INJECTI
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Buy PUMP ASSY, INJECTI 09450-00330 genuine, new aftermarket engine parts with delivery

Components :

001. PUMP ASSY, INJECTI 09450-00330

Scheme ###:

000. [01] 09450-00330 PUMP ASSY, INJECTI EZ01018
003. [01] 09011-00811 HOUSING SUB-ASSY,
005. [01] 09005-90040 NIPPLE, DELIVERY V EZ00965005
006. [01] 09024-50071 SCREW, HOLLOW EZ00965XX006
007. [02] 09005-80040 WASHER, NIPPLE EZ00965XX007
008. [01] 09013-60010 SPRING, DELIVERY V 85265-00021
009. [01] 09013-10091 HOLDER, DELIVERY V EZ00965XX009
010. [01] 09013-70010 GASKET, DELIVERY V 85265-00019
011. [01] 09014-00010 VALVE SUB-ASSY, IN 09014-00010
012. [01] 09015-00961 ELEMENT SUB-ASSY, EZ01184
013. [01] 09016-10220 SLEEVE, PLUNGER CO EZ0066313
014. [01] 09016-30010 SEAT, SPRING, UPR 09016-30010
015. [01] 09016-40140 SPRING, PUMP PLUNG EZ0096515
016. [01] 09016-50010 SEAT, SPRING, LWR 85265-00031
017. [01] 09021-60011 SLEEVE, GUIDE EZ0096517
018. [01] 09018-70010 RING, SNAP EZ00663018
019. [01] 09021-20150 RACK, CONTROL EZ0066319
020. [01] 94918-00310 SCREW, HOLLOW 85265-00078
021. [02] 09022-20011 WASHER, FUEL PIPE 85265-00048
021. [02] 09022-20070 WASHER, FUEL PIPE 85265-00079
023. [01] 09024-40010 SCREW, AIR BLEEDER 09024-40010
024. [01] 09024-30010 PACKING, AIR BLEED 09024-30010
025. [01] 94904-10650 BOLT, SLOTTED HEXA EZ0066325
026. [01] 09026-10021 POINTER EZ0066326
027. [1C] 09026-20010 WASHER, CONPENSATI EZ0066327
027. [1C] 09026-30010 WASHER, CONPENSATI EZ0066327
027. [1C] 09026-40010 WASHER, CONPENSATI EZ0066327
027. [1C] 09026-50010 WASHER, CONPENSATI EZ0066327

Include in #3:

09450-00330 as PUMP ASSY, INJECTI

Cross reference number



Part num Firm num Firm Name
09450-00330  EZ01018  PUMP ASSY, INJECTI
EZ01018    MITSUBISHI PUMP ASSY, INJECTI




Information:

Operation of ATAAC
Inlet air is pulled through the air cleaner, compressed and heated by the compressor wheel in the compressor side of the turbocharger to about 150°C (300°F). The heated air is then pushed through the air to air aftercooler core and moved to the air inlet manifold in the cylinder head at about 43°C (110°F).
Radiator Core (1) and Aftercooler Core (2).Cooling the inlet air increases combustion efficiency, which helps to lower fuel consumption and increase horsepower output. The aftercooler core (2) is a separate cooler core installed behind the standard radiator core (1). Ambient temperature is moved across both cores by the engine fan- this cools the turbocharged inlet air and the engine coolant.Lower inlet air temperature allows more air to enter the cylinder. More complete fuel combustion and reduced exhaust emissions are the results. Air-to-air aftercoolers can achieve charge air temperatures lower than water-to-air systems. The lower air temperatures provide improved efficiency.
To maintain an adequate water pump cavitation temperature for efficient water pump performance in an Air-to-Air Aftercooled engine: Caterpillar recommends that the coolant mix contain a minimum of 30 percent Caterpillar Antifreeze, or equivalent.
Air Inlet System
An air hose failure or a significant air inlet system leak will cause a large drop in boost pressure and power. The engine can be operated at this power level for a short period of time, however, sustained operation under this condition should be avoided.A slight reduction in power or response, or a small increase in exhaust temperature may indicate a small air leak in the charge air cooler core or piping.If air leaking is suspected, inspect the air inlet hoses, elbows and gaskets for cracks or damage. Replace the parts as needed. Check for loose clamps and tighten the clamps as needed.Radiator Restrictions
Caterpillar discourages the use of air flow restriction devices mounted in front of radiators with air-to-air aftercooled engines. Air flow restriction can cause higher exhaust temperatures, power loss, excessive fan usage, and a reduction in fuel economy.If an air flow restriction device must be used, the device should have a permanent opening directly in line with the fan hub. The device must have a minimum opening dimension of at least 770 cm2 (120 in2).A centered opening, directly in line with the fan hub, is specified to provide sensing when viscous fan drives are used and/or to prevent an interrupted air flow on the fan blades. Interrupted air flow on the fan blades could cause a fan failure.Caterpillar recommends that a package include an inlet manifold temperature device, such as a light indicator, buzzer, etc., set at 65°C (150°F) and/or installation of an inlet air temperature gauge. For the ATAAC (Air-To-Air Aftercooled) engines, air temperature in the inlet manifold should not exceed 65°C (150°F). Temperatures exceeding this limit can cause power loss and potential engine damage.This temperature provides engine protection for full restriction device closure. This temperature can also serve as a diagnostic tool for a malfunction of the charge air cooling system. It is not anticipated that

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