Circuit Description
The automatic transmission input shaft speed (AT ISS) sensor assembly is a three-wire hall-effect sensor that is mounted internally to the transmission on the oil pump assembly. The AT ISS utilizes the gear teeth, located on the turbine shaft, to generate a voltage signal of varying frequency that corresponds to the rotational speed of the turbine shaft. The AT ISS signal is an input to the powertrain control module (PCM) and is used to determine line pressure, transmission shift patterns, torque converter clutch (TCC) slip speed and gear ratio.
If the PCM detects AT ISS input less than 100 RPM with the engine running, DTC P0717 sets. DTC P0717 is a type B DTC.
DTC Descriptor
This diagnostic procedure supports the following DTC:
DTC P0717 Input Speed Sensor Circuit Low Voltage
Conditions for Running the DTC
| • | No vehicle speed sensor (VSS) DTCs P0722 or P0723. |
| • | No AT ISS DTC P0716. |
| • | No TFP DTC P1810. |
| • | The vehicle speed is greater than 16 km/h (10 mph). |
| • | The engine torque is greater than 90 N·m (66 lb ft). |
Conditions for Setting the DTC
The AT ISS RPM is less than 100 RPM for 5 seconds.
Action Taken When the DTC Sets
| • | The PCM illuminates the malfunction indicator lamp (MIL) during the second consecutive trip in which the Conditions for Setting the DTC are met. |
| • | The PCM commands maximum line pressure. |
| • | The PCM freezes transmission adapts. |
| • | The PCM calculates a default AT ISS RPM. |
| • | The PCM records the operating conditions when the Conditions for Setting the DTC are met. The PCM stores this information as Freeze Frame and Failure Records. |
| • | The PCM records the operating conditions when the Conditions for Setting the DTC are met. The PCM stores this information as Failure Records. |
| • | The PCM stores DTC P0717 in PCM history during the second consecutive trip in which the Conditions for Setting the DTC are met. |
Conditions for Clearing the MIL/DTC
| • | The PCM turns OFF the MIL after the third consecutive drive trip in which the MIL illumination request is not present. |
| • | A scan tool can clear the MIL/DTC. |
| • | The PCM clears the DTC from PCM history if the vehicle completes 40 warm-up cycles without an emission-related diagnostic fault occurring. |
Diagnostic Aids
| • | Inspect the connectors at the PCM, the AT ISS, and all other circuit connecting points for an intermittent condition. Refer to Testing for Intermittent Conditions and Poor Connections . |
| • | Inspect the circuit wiring for an intermittent condition. Refer to Testing for Electrical Intermittents . |
| • | Road test the vehicle while monitoring the Transmission ISS parameter on the scan tool. The Transmission ISS parameter should vary with engine speed changes and not abruptly drop out. |
| • | Inspect for an open or shorted AT ISS wire. |
| • | Inspect for a disconnected AT ISS connector. |
| • | Inspect for a faulty AT ISS. |
Step | Action | Values | Yes | No | ||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
1 | Did you perform the Diagnostic System Check - Vehicle? | -- | Go to Step 2 | |||||||||||
2 |
Important: Before clearing the DTCs, use the scan tool in order to record the Freeze Frame and Failure Records for reference. The Clear Info function will erase the data. Is the scan tool Transmission AT ISS parameter greater than the specified value? | 400 RPM | Go to Diagnostic Aids | Go to Step 3 | ||||||||||
3 |
Does the voltage measure near the specified value? | 12 V | Go to Step 4 | Go to Step 7 | ||||||||||
4 | Measure the voltage from the AT ISS 12-volt reference circuit to the AT ISS low reference circuit, at the AT 20-way connector, engine harness side. Does the voltage measure near the specified value? | 12 V | Go to Step 5 | Go to Step 8 | ||||||||||
5 |
Is the Transmission AT ISS RPM near the specified value and steady? | 602 RPM | Go to Step 9 | Go to Step 6 | ||||||||||
6 | Test the AT ISS signal circuit for the following conditions:
Refer to Circuit Testing and Wiring Repairs . Did you find and correct the condition? | -- | Go to Step 14 | Go to Step 13 | ||||||||||
7 | Test the AT ISS 12-volt reference circuit for the following conditions:
Refer to Circuit Testing and Wiring Repairs . Did you find and correct the condition? | -- | Go to Step 14 | Go to Step 13 | ||||||||||
8 | Test the AT ISS low reference circuit for an open or a short to voltage. Refer to Circuit Testing and Wiring Repairs . Did you find and correct the condition? | -- | Go to Step 14 | Go to Step 13 | ||||||||||
9 | Test the AT ISS internal transmission harness for the following conditions:
Refer to Circuit Testing . Did you find a condition? | -- | Go to Step 11 | Go to Step 10 | ||||||||||
10 |
Did you find and correct the condition? | -- | Go to Step 14 | Go to Step 12 | ||||||||||
11 | Replace the internal transmission harness. Refer to Valve Body and Pressure Switch Replacement . Did you complete the action? | -- | Go to Step 14 | -- | ||||||||||
12 | Replace the AT ISS. Refer to Oil Pump Disassemble . Did you complete the replacement? | -- | Go to Step 14 | -- | ||||||||||
13 | Replace the PCM. Refer to Control Module References for replacement, setup, and programming. Did you complete the replacement? | -- | Go to Step 14 | -- | ||||||||||
14 | Perform the following procedure In order to verify the repair:
Has the test run and passed? | -- | Go to Step 15 | Go to Step 2 | ||||||||||
15 | With the scan tool, observe the stored information, capture info and DTC info. Does the scan tool display any DTCs that you have not diagnosed? | -- | System OK |
