106673-2130 ZEXEL 9 400 617 213 BOSCH INJECTION-PUMP ASSEMBLY 9400617213 1066732130 me157069


 

Information injection-pump assembly

BOSCH 9 400 617 213 9400617213
ZEXEL 106673-2130 1066732130
MITSUBISHI ME157069 me157069
106673-2130 INJECTION-PUMP ASSEMBLY
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Buy INJECTION-PUMP ASSEMBLY 106673-2130 zexel genuine, new aftermarket engine parts with delivery

Service parts 106673-2130 INJECTION-PUMP ASSEMBLY:

1. _
2. FUEL INJECTION PUMP 106060-5140
3. GOVERNOR 105408-0530
4. SUPPLY PUMP 105207-1210
5. AUTOM. ADVANCE MECHANIS 105636-1820
6. COUPLING PLATE 105662-0710
7. COUPLING PLATE
8. _
9. _
10. NOZZLE AND HOLDER ASSY 105100-6211
11. Nozzle and Holder ME059621
12. Open Pre:MPa(Kqf/cm2) 21.6{220}
13. NOZZLE-HOLDER 105030-5010
14. NOZZLE 105015-5330
15. NOZZLE SET

Include in #1:

106673-2130 as INJECTION-PUMP ASSEMBLY

Cross reference number

BOSCH 9 400 617 213 9400617213
ZEXEL 106673-2130 1066732130
MITSUBISHI ME157069 me157069


Zexel num
Bosch num
Firm num
Name
106673-2130 
9 400 617 213 
ME157069  MITSUBISHI
INJECTION-PUMP ASSEMBLY
6D22T K 14CA INJECTION PUMP ASSY PE6P,6PD PE

Calibration Data:

Adjustment conditions
Test oil
1404 Test oil
  ISO4113 or {SAEJ967d}
Test oil temperature degC   40 40 45
Nozzle and nozzle holder   105780-8140
Bosch type code   EF8511/9A
Nozzle   105780-0000
Bosch type code   DN12SD12T
Nozzle holder   105780-2080
Bosch type code   EF8511/9
Opening pressure MPa   17.2
Opening pressure kgf/cm2   175
Injection pipe
Outer diameter - inner diameter - length (mm)
mm   8-3-600
Overflow valve   131424-4620
Overflow valve opening pressure kPa   255 221 289
Overflow valve opening pressure kgf/cm2   2.6 2.25 2.95
Tester oil delivery pressure kPa   157 157 157
Tester oil delivery pressure kgf/cm2   1.6 1.6 1.6
Direction of rotation (viewed from drive side)
Right
  R
Injection timing adjustment
Direction of rotation (viewed from drive side)
Right
  R
Injection order   1-5-3-6- 2-4
Pre-stroke mm   4.8 4.75 4.85
Beginning of injection position
Governor side
  NO.1
Difference between angles 1
Cal 1-5
deg.   60 59.5 60.5
Difference between angles 2
Cal 1-3
deg.   120 119.5 120.5
Difference between angles 3
Cal 1-6
deg.   180 179.5 180.5
Difference between angles 4
Cyl.1-2
deg.   240 239.5 240.5
Difference between angles 5
Cal 1-4
deg.   300 299.5 300.5
Injection quantity adjustment
Adjusting point   A
Rack position   11.7
Pump speed r/min   700 700 700
Average injection quantity mm3/st.   132 129 135
Max. variation between cylinders %   0 -3 3
Basic   *
Fixing the lever   *
Injection quantity adjustment_02
Adjusting point   B
Rack position   4.8+-0.5
Pump speed r/min   500 500 500
Average injection quantity mm3/st.   8 5.4 10.6
Max. variation between cylinders %   0 -15 15
Fixing the rack   *
Injection quantity adjustment_03
Adjusting point   C
Rack position   13.9+-0. 5
Pump speed r/min   100 100 100
Average injection quantity mm3/st.   133 113 153
Fixing the lever   *
Rack limit   *
Injection quantity adjustment_04
Adjusting point   D
Rack position   6+-0.5
Pump speed r/min   275 275 275
Average injection quantity mm3/st.   10.8 8.2 13.4
Fixing the rack   *
Remarks
(check)
 
Timer adjustment
Pump speed r/min   950--
Advance angle deg.   0 0 0
Remarks
Start
 
Timer adjustment_02
Pump speed r/min   900
Advance angle deg.   0.5
Timer adjustment_03
Pump speed r/min   1100
Advance angle deg.   1 0.5 1.5
Remarks
Finish
 

Test data Ex:

Governor adjustment

Test data 106673-2130
N:Pump speed R:Rack position (mm) (1)Target notch: K (2)Tolerance for racks not indicated: +-0.05mm. (3)RACK LIMIT (4)Torque spring does not operate. (5)At delivery (6)Idle sub spring setting: L1.
----------
K=9 L1=6.2+-0.1mm
----------

Speed control lever angle

Test data 106673-2130
F:Full speed I:Idle (1)Stopper bolt setting (2)At shipping
----------

----------
a=30deg+-5deg b=(2deg) c=10deg+-5deg

Stop lever angle

Test data 106673-2130
N:Pump normal S:Stop the pump. (1)Normal
----------

----------
a=19deg+-5deg b=53deg+-5deg

Timing setting

Test data 106673-2130
(1)Pump vertical direction (2)Coupling's key groove position at No 1 cylinder's beginning of injection (3)- (4)-
----------

----------
a=(7deg)




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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