871128 Propeller Volvo.Penta
430; 430A; 430B, 500; 500A; 501A, 740A; BB740A, AD30A; AQAD30A; MD30A, AQ120B; AQ125A; AQ140A, AQ145A; BB145A, AQ225D; AQ225E; AQ225F, AQ260A; AQ260B; BB260A, BB231A; BB261A, KAD42A; KAMD42A; HS1A, MB10A, MD11; MD11C; MD11D, MD1B; MD2B; AQD2B, MD21B;
Propeller
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Compatible models:
430; 430A; 430B
500; 500A; 501A
740A; BB740A
AD30A; AQAD30A; MD30A
AQ120B; AQ125A; AQ140A
AQ145A; BB145A
AQ225D; AQ225E; AQ225F
AQ260A; AQ260B; BB260A
BB231A; BB261A
KAD42A; KAMD42A; HS1A
MB10A
MD11; MD11C; MD11D
MD1B; MD2B; AQD2B
MD21B; AQD21B
MD31A; TMD31A; TMD31B
MD31A; TMD31B; TAMD31B
MD40A; TMD40A; TMD40B
MD5A; MD5B; MD5C
MD6; MD6A; MD6B
TMD41A; TMD41B; D41A
TMD41B; D41B; TAMD41B
Volvo.Penta
Volvo Penta entire parts catalog list:
- Propeller, Bronze Zinc Anode: A » 871128
740A; BB740A
AD30A; AQAD30A; MD30A; TAMD30A; TMD30A; AD30; AQAD30; MD30; TAMD30; TMD30
AQ120B; AQ125A; AQ140A; BB140A
AQ145A; BB145A
AQ225D; AQ225E; AQ225F; BB225A; BB225AV; BB225B; BB225C; 275; 280B; 290A; 290DP; MS3B; MS3C; MS4A
AQ260A; AQ260B; BB260A; BB260AV; BB260B; BB260C
BB231A; BB261A
KAD42A; KAMD42A; HS1A; MS5B
MB10A
MD11; MD11C; MD11D; MD17; MD17C; MD17D
MD1B; MD2B; AQD2B; MD3B
MD21B; AQD21B
MD31A; TMD31A; TMD31B; TAMD31A; TAMD31B; AD31; AQAD31A; AD31B; 290A; DP-A; DP-B; DP-A1; DP-B1; SP-A; SP-A1
MD31A; TMD31B; TAMD31B; AD31B
MD40A; TMD40A; TMD40B; TMD40C; AQD40A; TAMD40A; TAMD40B; AD40B; AQAD40A; AQAD40B
MD5A; MD5B; MD5C
MD6; MD6A; MD6B; MD7; MD7A; MD7B
TMD41A; TMD41B; D41A; D41B; TAMD41A; TAMD41B; AQAD41A; AD41A; AD41B; 290A; DP-A; DP-B; DP-A1; DP-B1; SP-A; SP-A1; AD41BJ; AD41; AD41P-B; D41; TAMD41
TMD41B; D41B; TAMD41B; AD41B; AD41BJ
Information:
Illustration 1 g00554753
Left side view (1) Fuel priming pump. (2) Fuel transfer pump. (3) Fuel filter. (4) Electronic Control Module (ECM).
Illustration 2 g00470983
Right side view (typical example) (5) Exhaust manifold. (6) Turbocharger. (7) Temperature regulator housing. (8) Water pump. (9) Oil filter. (10) Oil cooler. (11) Oil level gauge.
Illustration 3 g00470984
Top view (typical example) (1) Fuel priming pump. (5) Exhaust manifold. (6) Turbocharger. (11) Oil level gauge. (12) Flywheel housing.
Illustration 4 g00470986
Front view (typical example) (13) Front timing gear housing. (14) Vibration damper.
Illustration 5 g00471007
Rear view (typical example) (15) Flywheel housing. (16) Flywheel.General Information
The engines are electronically controlled mechanically actuated unit injector diesel engines. The 3406E is an in-line six cylinder engine with a bore of 137 mm (5.4 inch) and with a stroke of 165 mm (6.5 inch). The 3406E engine has a total displacement of 14.6 L (893 in3). The engine is configured for turbocharged air-to-air aftercooling with electronic unit injection.The 3456 is an in-line six cylinder engine with a bore of 140 mm (5.5 inch) and with a stroke of 171 mm (6.7 inch). The 3456 engine has a total displacement of 15.8 L (964.18 in3). The engine is configured for turbocharged air-to-air aftercooling with electronic unit injection.The electronic control system was designed to provide electronic governing, automatic fuel ratio control, torque rise shaping, injection timing control, and system diagnostics. The additional benefits of the electronic system are listed: Idle Shutdown Timer and Data Link. The additional benefits provide the following features: additional engine economy and serviceability.The Electronic unit injector system eliminates many of the mechanical components of an in-line pump system. This system also provides increased control of the timing control and of the fuel air ratio control. The timing advance is achieved by the precise control of the fuel injector timing. The engine rpm is controlled by adjusting the duration of the injection. A special pulse wheel provides information to the electronic control module for the detection of the cylinder position and of the engine rpm.The engine has built-in diagnostics in order to ensure that all of the components are operating properly. In the event of a system component failure, the operator will be alerted to the condition by the "Check Engine" light. A Caterpillar service tool can be used to read the numerical code of the faulty component or of the condition. Intermittent faults are logged and the information is stored in the memory.Starting the Engine
The Electronic Control Module (ECM) will automatically provide the correct amount of fuel that is necessary to start the engine. The throttle should not be held while the engine is being cranked. At temperatures below 0°C (32°F), starting fluid may need to be sprayed into the air cleaner inlet. If the engine fails to start in 30 seconds, the starter switch should be released. The starter motor should be allowed to cool for two minutes before being used again.
Excessive ether (starting fluid) can cause piston and ring damage. Use ether for cold weather starting purposes only.
Cold Mode Operation
The engine control system performs a cold start strategy for the correct warm-up time after a cold engine start. The temperature for a cold engine start is less than 18°C (64°F). This cold start strategy is called cold mode. After being activated, this cold mode will remain active until the coolant temperature rises above 18°C (64°F) or until the engine has been running for 12 minutes. Cold mode will also vary the fuel injection amount, the timing for the maximum start-up, and the timing for the control of white smoke. The time that is necessary for the engine to achieve the normal mode of operation is usually less than the time that is required for a walk-around inspection of the machine.Customer Specified Parameters
The engine is capable of being programmed for several customer specified parameters. Refer to System Operation, "Glossary of Words for Electronic Control" for a complete list of the customer specified parameters. Refer to the Operation and Maintenance Manual for your machine for a brief explanation of each of the customer specified parameters.
Parts propeller Volvo Penta:
871210
871210 Propeller
430; 430A; 430B, 500; 500A; 501A, 740A; BB740A, AD30A; AQAD30A; MD30A, AQ120B; AQ125A; AQ140A, AQ145A; BB145A, AQ225D; AQ225E; AQ225F, AQ260A; AQ260B; BB260A, BB231A; BB261A, KAD42A; KAMD42A; HS1A, MB10A, MD11; MD11C; MD11D, MD1B; MD2B; AQD2B, MD21B;
814629
814629 Propeller
AD30A; AQAD30A; MD30A, AQ190A; AQ240A, AQ200B; AQ225B, AQ200C; AQ200D; AQ225C, MD21B; AQD21B, MD31A; TMD31A; TMD31B, MD31A; TMD31B; TAMD31B, MD40A; TMD40A; TMD40B, TMD41A; TMD41B; D41A, TMD41B; D41B; TAMD41B
852612
852612 Propeller
230A; 230B; 250A, 251A, 430; 430A; 430B, 500; 500A; 501A, 571A, AD30A; AQAD30A; MD30A, AD31D; AD31D-A; AD31XD, AD41D; D41D; TAMD41D, AQ120B; AQ125A; AQ140A, AQ125B, AQ131A; AQ131B; AQ131C, AQ145A; BB145A, AQ145B, AQ151A; AQ151B; AQ151C, AQ171A; AQ171
814633
814633 Propeller
AD30A; AQAD30A; MD30A, AQ120B; AQ125A; AQ140A, AQ125B, AQ131A; AQ131B; AQ131C, AQ145A; BB145A, AQ145B, AQ175A, AQ190A; AQ240A, AQ200B; AQ225B, AQ200C; AQ200D; AQ225C, AQ200D; AQ200F; 280B, AQ225D; AQ225E; AQ225F, AQ260A; AQ260B; BB260A, AQ290A, MD21B
813297
813297 Propeller
230A; 230B; 250A, 251A, 430; 430A; 430B, 500; 500A; 501A, 571A, AD30A; AQAD30A; MD30A, AQ120B; AQ125A; AQ140A, AQ125B, AQ131A; AQ131B; AQ131C, AQ145A; BB145A, AQ145B, AQ151A; AQ151B; AQ151C, AQ171A; AQ171C, AQ175A, AQ190A; AQ240A, AQ200B; AQ225B, AQ2
852247
852247 Propeller, 3 blades
AD30A; AQAD30A; MD30A, AQ200D; AQ200F; 280B, AQ225D; AQ225E; AQ225F, MD31A; TMD31A; TMD31B, MD31A; TMD31B; TAMD31B, MD40A; TMD40A; TMD40B, TMD41A; TMD41B; D41A, TMD41B; D41B; TAMD41B
852253
852253 Propeller, 4 blades
AD30A; AQAD30A; MD30A, AQ200D; AQ200F; 280B, AQ225D; AQ225E; AQ225F, MD31A; TMD31A; TMD31B, MD31A; TMD31B; TAMD31B, MD40A; TMD40A; TMD40B, TMD41A; TMD41B; D41A, TMD41B; D41B; TAMD41B
852271
852271 Propeller, 3 blades
AD30A; AQAD30A; MD30A, AQ200D; AQ200F; 280B, AQ225D; AQ225E; AQ225F, MD31A; TMD31A; TMD31B, MD31A; TMD31B; TAMD31B, MD40A; TMD40A; TMD40B, TMD41A; TMD41B; D41A, TMD41B; D41B; TAMD41B