Information governor
BOSCH
9 420 610 652
9420610652
ZEXEL
105923-1252
1059231252

Rating:
Scheme ###:
1. | [1] | 159360-0520 | GOVERNOR HOUSING |
4. | [1] | 159362-5520 | PLATE |
5. | [10] | 139006-6100 | BLEEDER SCREW |
5. | [10] | 139006-6100 | BLEEDER SCREW |
7. | [1] | 139709-0100 | O-RING |
8. | [1] | 159364-0120 | LEVER SHAFT |
9. | [1] | 159362-5620 | CONTROL LEVER |
10. | [1] | 016010-0740 | LOCKING WASHER |
11/1. | [0] | 029311-0220 | SHIM D18&10.3T0.2 |
11/1. | [0] | 029311-0230 | SHIM D18&10.3T0.5 |
11/1. | [0] | 029311-0430 | SHIM D18&10.3T0.30 |
11/1. | [0] | 029311-0440 | SHIM D18&10.3T0.40 |
11/1. | [0] | 029311-0450 | SHIM D18&10.3T0.25 |
11/1. | [0] | 029311-0460 | SHIM D18&10.3T0.35 |
11/1. | [0] | 139410-3300 | SHIM D18&10.3T0.6 |
11/1. | [0] | 139410-3400 | SHIM D18&10.3T0.8 |
11/1. | [0] | 139410-3500 | SHIM D18&10.3T0.9 |
12. | [1] | 159368-7800 | COILED SPRING |
13. | [1] | 159362-1500 | CONTROL LEVER |
15. | [1] | 013020-8040 | UNION NUT M8P1.25H7 |
16. | [1] | 159364-5000 | CAPSULE |
17. | [1] | 159362-0520 | CONTROL LEVER |
18. | [1] | 159215-0600 | COILED SPRING |
20. | [1] | 159364-3800 | LEVER SHAFT |
21. | [2] | 020104-1240 | BLEEDER SCREW |
22. | [1] | 159362-0600 | CONTROL LEVER |
23. | [2] | 139608-0600 | PACKING RING |
23. | [2] | 139608-0600 | PACKING RING |
24. | [1] | 159362-0700 | PLAIN WASHER |
24B/1. | [0] | 139408-1000 | SHIM D16&8T0.5 |
24B/1. | [0] | 139408-1300 | SHIM D16&8T0.2 |
24C. | [1] | 159362-0700 | PLAIN WASHER |
24D. | [1] | 139308-2100 | PLAIN WASHER |
25. | [1] | 159238-4200 | LOCKING WASHER |
25B. | [1] | 159238-4200 | LOCKING WASHER |
26. | [1] | 159390-6100 | CONTROL LEVER |
27. | [1] | 159368-9600 | COILED SPRING |
28. | [1] | 159364-6000 | BUSHING |
29. | [1] | 014110-8440 | LOCKING WASHER |
30. | [1] | 013020-8040 | UNION NUT M8P1.25H7 |
31. | [1] | 155644-1301 | BLEEDER SCREW |
31B. | [1] | 153505-0800 | FLAT-HEAD SCREW |
32. | [2] | 013030-6040 | UNION NUT M6P1H3.6 |
32. | [2] | 013030-6040 | UNION NUT M6P1H3.6 |
35. | [1] | 159361-0020 | GOVERNOR COVER |
43. | [1] | 159364-0700 | LEVER SHAFT |
44. | [1] | 159364-0800 | BEARING PIN |
45. | [2] | 016010-0640 | LOCKING WASHER |
46. | [1] | 159363-5720 | TENSIONING LEVER |
46/1. | [1] | 159363-5620 | TENSIONING LEVER |
46/2. | [1] | 159362-8221 | GUIDE LEVER |
46/3. | [1] | 159364-4201 | BEARING PIN |
46/4. | [1] | 159368-6201 | COILED SPRING |
46/5. | [1] | 016010-0540 | LOCKING WASHER |
46/6. | [1] | 016010-0440 | LOCKING WASHER |
46/7. | [1] | 159364-4121 | RACK |
46/8. | [1] | 159364-4300 | UNION NUT |
46/9. | [1] | 159364-4400 | FLAT-HEAD SCREW |
46/10. | [1] | 159368-6900 | COILED SPRING |
46/11. | [1] | 159368-7000 | COILED SPRING |
46/13. | [1] | 016010-0540 | LOCKING WASHER |
46/14. | [1] | 159364-1900 | FLAT-HEAD SCREW |
46/15. | [1] | 159364-1800 | UNION NUT |
46/16. | [1] | 159368-9500 | COILED SPRING |
47. | [2] | 016110-1020 | LOCKING WASHER |
48. | [2] | 159237-0200 | CAPSULE |
51. | [9] | 020106-3840 | BLEEDER SCREW |
65. | [1] | 154611-4220 | RACK SENSOR ASSY |
65/1. | [1] | 479775-1420 | RACK SENSOR |
65/2. | [1] | 154614-4800 | JOINT CONNECTION |
65/3. | [1] | 154614-3100 | BLOCK |
65/4. | [1] | 010234-1040 | HEX-SOCKET-HEAD CAP SCREW |
65/5. | [1] | 014110-4440 | LOCKING WASHER |
65/6. | [1] | 026524-3040 | GASKET |
65/7A. | [0] | 029310-6220 | SHIM D11.5&6.5T0.10 |
65/7B. | [0] | 029310-6230 | SHIM D11.5&6.5T0.20 |
65/7C. | [0] | 029310-6240 | SHIM D11.5&6.5T0.25 |
65/7D. | [0] | 029310-6260 | SHIM D11.5&6.4T1.00 |
65/7E. | [0] | 029310-6270 | SHIM D11.5&6.4T1.20 |
65/7F. | [0] | 029310-6280 | SHIM D11.5&6.4T1.50 |
65/8. | [1] | 154614-1900 | UNION NUT |
65/9. | [1] | 154614-3300 | BEARING PIN |
97. | [1] | 159364-2000 | CAPSULE |
100. | [1] | 154100-9220 | FLYWEIGHT ASSEMBLY |
101. | [1] | 025803-1310 | WOODRUFF KEY |
102. | [1] | 029321-2020 | LOCKING WASHER |
103. | [1] | 029231-2030 | UNION NUT |
110. | [1] | 154123-2320 | SLIDING PIECE |
111/1. | [0] | 029311-0010 | SHIM D14&10.1T0.2 |
111/1. | [0] | 029311-0180 | SHIM D14&10.1T0.3 |
111/1. | [0] | 029311-0190 | SHIM D14&10.1T0.40 |
111/1. | [0] | 029311-0210 | SHIM D14&10.1T1 |
111/1. | [0] | 139410-0000 | SHIM D14.0&10.1T0.5 |
111/1. | [0] | 139410-0100 | SHIM D14.0&10.1T1.5 |
111/1. | [0] | 139410-3000 | SHIM D14&10.1T2.0 |
111/1. | [0] | 139410-3100 | SHIM D14&10.1T3.0 |
111/1. | [0] | 139410-3200 | SHIM D14&10.1T4.0 |
112. | [1] | 159364-2100 | TERMINAL STUD |
130. | [1] | 159367-0600 | GOVERNOR SPRING |
131. | [1] | 159367-6300 | GOVERNOR SPRING |
132. | [1] | 159368-6500 | COILED SPRING |
133. | [1] | 159368-2720 | SPRING PACK |
133/1. | [1] | 159364-2200 | GUIDE SLEEVE |
133/2. | [1] | 159368-0000 | COILED SPRING |
133/3. | [1] | 159368-0800 | COILED SPRING |
133/4/1. | [0] | 029311-0010 | SHIM D14&10.1T0.2 |
133/4/1. | [0] | 029311-0180 | SHIM D14&10.1T0.3 |
133/4/1. | [0] | 029311-0190 | SHIM D14&10.1T0.40 |
133/4/1. | [0] | 029311-0210 | SHIM D14&10.1T1 |
133/4/1. | [0] | 139410-0000 | SHIM D14.0&10.1T0.5 |
133/4/1. | [0] | 139410-0100 | SHIM D14.0&10.1T1.5 |
133/4/1. | [0] | 139410-3000 | SHIM D14&10.1T2.0 |
133/4/1. | [0] | 139410-3100 | SHIM D14&10.1T3.0 |
133/4/1. | [0] | 139410-3200 | SHIM D14&10.1T4.0 |
135. | [1] | 159364-2300 | FLAT-HEAD SCREW |
137. | [1] | 159364-2000 | CAPSULE |
140. | [1] | 159364-2500 | LEVER SHAFT |
145. | [1] | 159233-5700 | UNION NUT |
149. | [1] | 159237-5400 | CAPSULE |
150. | [1] | 159364-2600 | SLOTTED WASHER |
151. | [1] | 159364-2700 | SLOTTED WASHER |
155. | [1] | 159363-2421 | STRAP |
156. | [1] | 010235-1020 | HEX-SOCKET-HEAD CAP SCREW |
160. | [1] | 159362-2020 | LEVER GROUP |
160/1. | [1] | 159364-3220 | LEVER SHAFT |
160/2. | [1] | 159362-1020 | CONTROL LEVER |
160/3. | [1] | 159362-2000 | CONTROL LEVER |
160/4. | [2] | 159362-1300 | SHIM |
160/4. | [2] | 159362-1300 | SHIM |
160/5. | [2] | 016010-0840 | LOCKING WASHER |
160/5. | [2] | 016010-0840 | LOCKING WASHER |
160/6. | [1] | 159368-6600 | COILED SPRING |
162. | [1] | 139411-0600 | SHIM |
163. | [1] | 159238-3000 | LOCKING WASHER |
164. | [1] | 139610-0800 | PACKING RING |
168. | [1] | 159380-0300 | CONTROL LEVER |
169. | [1] | 013020-8040 | UNION NUT M8P1.25H7 |
170. | [1] | 159381-0620 | CONTROL LEVER |
172. | [2] | 020106-1240 | BLEEDER SCREW M6P1.0L12 |
173. | [1] | 154013-1700 | BLEEDER SCREW |
173B. | [1] | 154013-1800 | BLEEDER SCREW |
173C. | [1] | 154013-1900 | BLEEDER SCREW |
174. | [1] | 154013-2000 | BLEEDER SCREW |
175. | [1] | 154013-2100 | FLAT-HEAD SCREW |
176. | [1] | 154011-4000 | UNION NUT |
177. | [1] | 154011-4100 | UNION NUT |
178. | [1] | 013131-0040 | UNION NUT M10P1.25H6 |
220. | [1] | 159368-8420 | HEADLESS SCREW |
221. | [1] | 154011-4300 | UNION NUT |
222. | [2] | 026512-1540 | GASKET D15.4&12.2T1.50 |
223. | [1] | 154159-2100 | CAP NUT |
224. | [1] | 139006-0800 | BLEEDER SCREW |
225. | [2] | 029310-8050 | SHIM D13.5&8T0.5 |
226. | [1] | 159368-9101 | COILED SPRING |
227. | [1] | 159362-6720 | CONTROL LEVER |
236. | [1] | 154390-4200 | GASKET |
237. | [1] | 154390-2500 | GASKET |
248. | [1] | 159397-1720 | BRACKET |
250. | [1] | 159396-6020 | BRACKET |
251. | [2] | 154339-0600 | COILED SPRING |
252. | [3] | 020106-1640 | BLEEDER SCREW M6P1.0L14 |
252B. | [1] | 154370-9400 | PLAIN WASHER |
254. | [1] | 010110-2040 | BLEEDER SCREW M10P1.25L20 |
257. | [2] | 154156-1800 | TUBE |
270. | [1] | 159362-4620 | GUIDE PLATE |
271. | [2] | 020106-1640 | BLEEDER SCREW M6P1.0L14 |
300. | [1] | 159372-9700 | CAM PLATE |
301. | [1] | 016010-0840 | LOCKING WASHER |
303. | [1] | 016010-0540 | LOCKING WASHER |
311. | [2] | 159237-5400 | CAPSULE |
340. | [1] | 159396-0120 | BRACKET |
340B. | [1] | 159396-0200 | PLATE |
341. | [1] | 020106-1240 | BLEEDER SCREW M6P1.0L12 |
341B. | [1] | 020106-1840 | BLEEDER SCREW M6P1L18 |
Include in #1:
108622-3343
as GOVERNOR
Cross reference number
Zexel num
Bosch num
Firm num
Name
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
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