2P8907 SPIDER AS-FAN Caterpillar parts
120G, 12G, 130G, 140G, 14G, 160G
Rating:
Alternative (cross code) number:
CA2P8907
2P-8907
2P8907
CA2P8907
2P-8907
2P8907
Weight: 30 pounds 13 kg.
Information:
BLADE WIDTH
71.38
mm
BOLT CIRCLE DIAMETER
119.38
mm
DIAMETER OF PITCH CIRCLE HOLES
10.31
mm
HUB THICKNESS
13.97
mm
NUMBER OF BLADES
6
NUMBER OF PITCH HOLES
6
OD
843.03
mm
PILOT HOLE DIAMETER
95.22
mm
TYPE
BLOWER
MOTOR GRADER,
Related part:
2P8907
SPIDER-AS-FAN-YM
3309289
CL
Compare Prices: .
As an associate, we earn commssions on qualifying purchases through the links below
CTP 2P8907 Standard Fan for Models 12G/120G/14G/130G/160G
CTP With the engine off, the ignition locked in the off position, and any required guarding removed, you are now ready to reverse your fan; There is a pink "DANGER" tag provided with your fan that should also be fastened to the ignition switch panel || Individually reverse each blade by simply pushing inward (towards the hub) to compress the spring and then begin to rotate the blade; it should only turn in one direction || Once the blade begins to rotate, you no longer need to keep pushing inward; continue to turn the blade toward the desired position; continue to reverse the remaining blades so that they are all in the same position || Once the blade is rotated fully to the desired position, the blade will "spring" outward and lock itself into place; Now the blade will not be able to be turned around without pushing it inward again; The reversing of one blade is now complete || Now that all of the blades have been reversed, the fan will force the air in the opposite direction; You are now ready to re-install the guarding, unlock the ignition switch, and continue operating the equipment with increased comfort
CTP With the engine off, the ignition locked in the off position, and any required guarding removed, you are now ready to reverse your fan; There is a pink "DANGER" tag provided with your fan that should also be fastened to the ignition switch panel || Individually reverse each blade by simply pushing inward (towards the hub) to compress the spring and then begin to rotate the blade; it should only turn in one direction || Once the blade begins to rotate, you no longer need to keep pushing inward; continue to turn the blade toward the desired position; continue to reverse the remaining blades so that they are all in the same position || Once the blade is rotated fully to the desired position, the blade will "spring" outward and lock itself into place; Now the blade will not be able to be turned around without pushing it inward again; The reversing of one blade is now complete || Now that all of the blades have been reversed, the fan will force the air in the opposite direction; You are now ready to re-install the guarding, unlock the ignition switch, and continue operating the equipment with increased comfort
2P8907 Spider A (New AFTERMARKET) - G&T Engine Parts
G&T Engine Parts Condition: NEW AFTERMARKET || Weight: 39.27 lbs || Items are sold by part number only. Picture is for illustration purposes and the part or parts may be different in color or quantity. || Use of any OEM manufacturer name is not intended to represent any relationship between the two companies, instead it indicates that we sell replacement parts that are compatible with OEM components.
G&T Engine Parts Condition: NEW AFTERMARKET || Weight: 39.27 lbs || Items are sold by part number only. Picture is for illustration purposes and the part or parts may be different in color or quantity. || Use of any OEM manufacturer name is not intended to represent any relationship between the two companies, instead it indicates that we sell replacement parts that are compatible with OEM components.
2P8907 Spider A (New AFTERMARKET) - G&T Engine Parts
G&T Engine Parts Condition: NEW AFTERMARKET || Weight: 39.27 lbs || Items are sold by part number only. Picture is for illustration purposes and the part or parts may be different in color or quantity. || Use of any OEM manufacturer name is not intended to represent any relationship between the two companies, instead it indicates that we sell replacement parts that are compatible with OEM components.
G&T Engine Parts Condition: NEW AFTERMARKET || Weight: 39.27 lbs || Items are sold by part number only. Picture is for illustration purposes and the part or parts may be different in color or quantity. || Use of any OEM manufacturer name is not intended to represent any relationship between the two companies, instead it indicates that we sell replacement parts that are compatible with OEM components.
Number on catalog scheme:
1
For full view, you need register
Information:
System Operation Description:Use this procedure to troubleshoot suspect problems with the circuit for the turbocharger compressor bypass system.This procedure covers the following diagnostic codes:
1720-9 Turbocharger Compressor Bypass Valve Actuator : Abnormal Update Rate
1720-11 Turbocharger Compressor Bypass Valve Actuator invalid
1720-12 Turbocharger Compressor Bypass Valve Actuator : FailureThese codes indicate an abnormal operating condition in the turbocharger compressor bypass valve actuator. Refer to literature from the OEM for troubleshooting the turbocharger compressor bypass valve actuator.A bypass valve is connected between the outlets for the turbocharger compressors and the inlets for the turbocharger compressors. The bypass valve is activated by an actuator. The Electronic Control Module (ECM) activates the actuator for the bypass valve during these conditions:
Turbocharger surge
Engine shutdownTurbocharger SurgeA rapid drop in the output power of the generator can cause the engine's speed to quickly increase. The increased speed of the engine causes the turbochargers to overspeed temporarily. This is called a turbocharger surge. Surging can damage the turbochargers.The ECM continuously monitors the speed of the engine. The ECM responds to a rapid increase in the speed of the engine by activating the actuator for the bypass valve. The actuator opens the valve.The valve allows the compressed air/fuel mixture in the aftercooler's inlet to flow into the intake of the turbocharger's compressor. This reduces the boost pressure in the air inlet manifold.Engine ShutdownEngine shutdown occurs when the output for the fuel control relay is OFF and the engine RPM is above 100. The ECM activates the actuator for the bypass valve until the engine RPM drops to zero. This scavenges any unburned gases in the components of the system during engine shutdown.CAN Data LinkThe ECM and the actuator communicate via the CAN data link. The ECM sends a command signal to the actuator. The actuator sends the following information to the ECM: actuator position, CCM heartbeat, software version and internal fault diagnosis.If the ECM cannot communicate with the actuator, the ECM activates a 1720-9 diagnostic code and the engine is shut down. A 1720-9 diagnostic code is probably caused by a problem with an electrical connector or a harness. The next likely cause is a problem with the actuator. The least likely cause is a problem with the ECM.Terminating resistors must be connected to each end of the CAN data link. The terminating resistors improve the communication between the devices. If there is an intermittent diagnostic code for any of the devices that are connected to the CAN data link, be sure to check the terminating resistor that is on the right side of the terminal box. Also check the terminating resistor that is on the right front side of the engine. The resistor will be near the compressor bypass valve. Replace parts, if necessary.Identification on the CAN Data LinkWhen the actuator for the bypass valve is powered up, the actuator looks for a ground on terminal "A". If there is a ground on terminal "A", the actuator will have a unique identification on the CAN data link.If there is
1720-9 Turbocharger Compressor Bypass Valve Actuator : Abnormal Update Rate
1720-11 Turbocharger Compressor Bypass Valve Actuator invalid
1720-12 Turbocharger Compressor Bypass Valve Actuator : FailureThese codes indicate an abnormal operating condition in the turbocharger compressor bypass valve actuator. Refer to literature from the OEM for troubleshooting the turbocharger compressor bypass valve actuator.A bypass valve is connected between the outlets for the turbocharger compressors and the inlets for the turbocharger compressors. The bypass valve is activated by an actuator. The Electronic Control Module (ECM) activates the actuator for the bypass valve during these conditions:
Turbocharger surge
Engine shutdownTurbocharger SurgeA rapid drop in the output power of the generator can cause the engine's speed to quickly increase. The increased speed of the engine causes the turbochargers to overspeed temporarily. This is called a turbocharger surge. Surging can damage the turbochargers.The ECM continuously monitors the speed of the engine. The ECM responds to a rapid increase in the speed of the engine by activating the actuator for the bypass valve. The actuator opens the valve.The valve allows the compressed air/fuel mixture in the aftercooler's inlet to flow into the intake of the turbocharger's compressor. This reduces the boost pressure in the air inlet manifold.Engine ShutdownEngine shutdown occurs when the output for the fuel control relay is OFF and the engine RPM is above 100. The ECM activates the actuator for the bypass valve until the engine RPM drops to zero. This scavenges any unburned gases in the components of the system during engine shutdown.CAN Data LinkThe ECM and the actuator communicate via the CAN data link. The ECM sends a command signal to the actuator. The actuator sends the following information to the ECM: actuator position, CCM heartbeat, software version and internal fault diagnosis.If the ECM cannot communicate with the actuator, the ECM activates a 1720-9 diagnostic code and the engine is shut down. A 1720-9 diagnostic code is probably caused by a problem with an electrical connector or a harness. The next likely cause is a problem with the actuator. The least likely cause is a problem with the ECM.Terminating resistors must be connected to each end of the CAN data link. The terminating resistors improve the communication between the devices. If there is an intermittent diagnostic code for any of the devices that are connected to the CAN data link, be sure to check the terminating resistor that is on the right side of the terminal box. Also check the terminating resistor that is on the right front side of the engine. The resistor will be near the compressor bypass valve. Replace parts, if necessary.Identification on the CAN Data LinkWhen the actuator for the bypass valve is powered up, the actuator looks for a ground on terminal "A". If there is a ground on terminal "A", the actuator will have a unique identification on the CAN data link.If there is
Caterpillar parts catalog:
Parts spider Caterpillar catalog:
120G, 12G, 130G, 140G, 160G, 572G, 613C, 773B, 910E, 931B, 935C II, 939, D3B, D3C II, D4B, D4C, D4C II, D5C III, IT12B, IT14B
120G, 120H, 120H ES, 120H NA, 120K, 120K 2, 12G, 12H, 12H ES, 12H NA, 12K, 130G, 135H, 135H NA, 140G, 140H, 140H ES, 140H NA, 140K, 140K 2, 143H, 160G, 160H, 160H ES, 160H NA, 160K, 163H, 163H NA, 30/...
9J0695
SPIDER
130G, 613B, 931, D3
130G, 613B, 931, D3
12G, 140, 140B, 14E, 14G, 621E, 623E, 627E, 631E, 633E II, 637E, 651E, 657E
120G, 769C, 772, 773B, 777, 910
14G, 16G, 988B
120G
12G, 130G, 140G, 160G
14G, 14H, 14H NA
8D5204
SPIDER
14G
14G
1T0480
SPIDER
824, 824B, 834
824, 824B, 834
12H, 12H ES, 12H NA, 140H, 140H ES, 140H NA, 143H, 160H, 160H ES, 160H NA, 163H NA
120H, 120H ES, 120H NA, 12H, 12H ES, 12H NA, 135H, 135H NA, 140H, 140H ES, 140H NA, 143H, 14H NA, 160H, 160H ES, 160H NA, 163H NA
16G, 16H, 16H NA
14G, 14H, 14H NA
12G, 130G, 140G, 160G
120G