106067-7450 ZEXEL 9 410 614 361 BOSCH FUEL-INJECTION PUMP 9410614361 1060677450 me717267


 

Information fuel-injection pump

BOSCH 9 410 614 361 9410614361
ZEXEL 106067-7450 1060677450
MITSUBISHI ME717267 me717267
106067-7450 FUEL-INJECTION PUMP
Rating:
43
Buy FUEL-INJECTION PUMP 106067-7450 zexel genuine, new aftermarket engine parts with delivery

Scheme ###:

1. [1] 134050-6920 PUMP HOUSING
1/30. [3] 029040-6020 STUD
1/45. [1] 134311-0000 SPACER RING
1/50. [12] 134138-0000 STUD
7. [6] 134142-9620 PLUNGER-AND-BARREL ASSY
7/1. [6] 134131-1920 FLANGE BUSHING
7/2. [6] 134101-6620 PLUNGER-AND-BARREL ASSY P51
7/3. [6] 134110-4420 DELIVERY-VALVE ASSEMBLY P43
7/4. [6] 134116-2400 FITTING
7/5. [6] 139722-0400 O-RING
7/6. [6] 134117-1400 FILLER PIECE
7/7. [6] 134112-0600 COILED SPRING
7/8. [6] 134115-0100 GASKET
7/9. [6] 029302-0140 PLAIN WASHER
7/10. [6] 134135-0400 CAPSULE
7/11. [6] 029602-0010 LOCKING WASHER
7/13. [6] 139729-0400 O-RING
7/14. [6] 139715-0400 O-RING
7/15. [6] 139715-0400 O-RING
23/1. [0] 139400-0900 SHIM T0.500
23/1. [0] 139400-1000 SHIM T0.525
23/1. [0] 139400-1100 SHIM T0.550
23/1. [0] 139400-1200 SHIM T0.575
23/1. [0] 139400-1300 SHIM T0.600
23/1. [0] 139400-1400 SHIM T0.625
23/1. [0] 139400-1500 SHIM T0.650
23/1. [0] 139400-1600 SHIM T0.675
23/1. [0] 139400-1700 SHIM T0.700
23/1. [0] 139400-1800 SHIM T0.725
23/1. [0] 139400-1900 SHIM T0.750
23/1. [0] 139400-2000 SHIM T0.775
23/1. [0] 139400-2100 SHIM T0.800
23/1. [0] 139400-2200 SHIM T0.825
23/1. [0] 139400-2300 SHIM T0.850
23/1. [0] 139400-2400 SHIM T0.875
23/1. [0] 139400-2500 SHIM T0.900
23/1. [0] 139400-2600 SHIM T0.925
23/1. [0] 139400-2700 SHIM T0.950
23/1. [0] 139400-2800 SHIM T0.975
23/1. [0] 139400-2900 SHIM T1.000
23/1. [0] 139400-3000 SHIM T1.025
23/1. [0] 139400-3100 SHIM T1.050
23/1. [0] 139400-3200 SHIM T1.075
23/1. [0] 139400-3300 SHIM T1.100
23/1. [0] 139400-3400 SHIM T1.125
23/1. [0] 139400-3500 SHIM T1.150
23/1. [0] 139400-3600 SHIM T1.175
23/1. [0] 139400-3700 SHIM T1.200
23/1. [0] 139400-3800 SHIM T1.225
23/1. [0] 139400-3900 SHIM T1.250
23/1. [0] 139400-4000 SHIM T1.275
23/1. [0] 139400-4100 SHIM T1.300
23/1. [0] 139400-4200 SHIM T1.325
23/1. [0] 139400-4300 SHIM T1.350
23/1. [0] 139400-4400 SHIM T1.375
23/1. [0] 139400-4500 SHIM T1.400
23/1. [0] 139400-4600 SHIM T1.425
23/1. [0] 139400-4700 SHIM T1.450
23/1. [0] 139400-4800 SHIM T1.475
23/1. [0] 139400-4900 SHIM T1.500
23/1. [0] 139400-5000 SHIM T1.525
23/1. [0] 139400-5100 SHIM T1.550
23/1. [0] 139400-5200 SHIM T1.575
23/1. [0] 139400-5300 SHIM T1.600
23/1. [0] 139400-5400 SHIM T1.625
23/1. [0] 139400-5500 SHIM T1.650
23/1. [0] 139400-5600 SHIM T1.675
23/1. [0] 139400-5700 SHIM T1.700
23/1. [0] 139400-5800 SHIM T1.725
23/1. [0] 139400-5900 SHIM T1.750
23/1. [0] 139400-6000 SHIM T1.775
23/1. [0] 139400-6100 SHIM T1.800
23/1. [0] 139400-6200 SHIM T1.825
23/1. [0] 139400-6200 SHIM T1.825
23/1. [0] 139400-6300 SHIM T1.850
23/1. [0] 139400-6400 SHIM T1.875
23/1. [0] 139400-6500 SHIM T1.900
23/1. [0] 139400-6600 SHIM T1.925
23/1. [0] 139400-6700 SHIM T1.950
23/1. [0] 139400-6800 SHIM T1.975
24. [12] 134132-0300 PLAIN WASHER
26. [12] 013021-0040 UNION NUT M10P1.5H8
30. [2] 134001-0000 BUSHING
30. [2] 134001-0000 BUSHING
32. [1] 134256-5000 CONTROL RACK
33. [1] 024030-2030 BEARING PIN
34. [1] 134222-0000 BUSHING
41. [6] 134241-0021 CONTROL SLEEVE
43. [6] 134216-0000 SLOTTED WASHER
44. [6] 134215-0400 COMPRESSION SPRING
45. [6] 134217-0500 SLOTTED WASHER
47. [6] 134200-0020 TAPPET
47/2. [6] 134204-0000 ROLLER
47/3. [6] 134205-0000 BUSHING
47/4. [6] 134203-0000 BEARING PIN
47/5. [6] 131206-0500 SLIDER
59. [1] 016650-2230 BEARING PLATE 4T-32205(NSK)
64/1. [0] 134303-0000 SHIM D59.8&43T1.2
64/1. [0] 134303-0100 SHIM D59.8&43T1.5
64/1. [0] 134303-0200 SHIM D59.8&43T1.8
64/1. [0] 134303-0300 SHIM D59.8&43T2.0
64/1. [0] 134303-0400 SHIM D59.8&43T0.6
67. [4] 029010-6810 BLEEDER SCREW
71. [1] 134371-2800 CAMSHAFT
74. [1] 134306-0100 BEARING SHELL
75. [2] 020106-2040 BLEEDER SCREW
79. [1] 016650-2230 BEARING PLATE 4T-32205(NSK)
80. [1] 134316-1700 COVER
81. [1] 139625-0000 PACKING RING
82/1. [0] 134314-0000 SHIM T0.1
82/1. [0] 134314-0100 SHIM T0.12
82/1. [0] 134314-0200 SHIM T0.14
82/1. [0] 134314-0300 SHIM T0.16
82/1. [0] 134314-0400 SHIM T0.18
82/1. [0] 134314-0500 SHIM T0.3
82/1. [0] 134314-0600 SHIM T0.5
83. [1] 029635-5010 O-RING
84. [1] 134563-0900 SLIDING PIECE
85. [1] 134043-0800 COVER
86. [1] 134042-1400 GASKET
87. [12] 012206-1640 FLAT-HEAD SCREW
88. [1] 134045-0100 CAPSULE
89. [1] 026524-2940 GASKET
93. [3] 139206-0400 UNION NUT
95. [1] 131041-0800 GASKET
96. [6] 134047-0000 CAPSULE
98. [1] 029470-5010 WOODRUFF KEY
111. [1] 134416-0100 COVER
112. [2] 014530-6540 TAB WASHER
113. [2] 021306-3010 FLAT-HEAD SCREW
118. [1] 134496-0600 POINTER
119. [2] 020006-1240 BLEEDER SCREW
147. [1] 029731-0180 EYE BOLT
148. [2] 026510-1340 GASKET
157. [1] 029731-4680 EYE BOLT
158. [2] 029341-4130 GASKET
167. [1] 131424-4620 OVER FLOW VALVE
168. [2] 029341-4130 GASKET

Include in #1:

106671-7121 as FUEL INJECTION PUMP

Cross reference number

Zexel num
Bosch num
Firm num
Name
106067-7450 
9 410 614 361 
NP-PE6P120/721RS3000NP155 
ME717267  MITSUBISHI
FUEL-INJECTION PUMP
Q




Information:

Air-to-air aftercooling (ATAAC) systems are simple, reliable, and easy to maintain. Generally, ATAAC benefits one or two of the following areas: * Improved fuel consumption* Lower emissions* Increased power In some cases all three may be improved.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

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