Download PDF by Friedrich Wilhelm Riegels: Aerofoil Sections: Results from Wind-Tunnel Investigations,

By Friedrich Wilhelm Riegels

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If it is faulty, repair it. If it is normal, the ECU could be faulty, so replace the ECU with a known good one and check if the symptoms appear. (1) Measure the resistance between the ECU ground terminal and the body ground. Resistance: 1P or less (2) Disconnect the ECU connector, check the ground terminals on the ECU side and the wire harness side for bend and check the contact pressure. IN–37 INTRODUCTION – VEHICLE LIFT AND SUPPORT LOCATIONS VEHICLE LIFT AND SUPPORT LOCATIONS IN–38 INTRODUCTION – ABBREVIATIONS USED IN THIS MANUAL ABBREVIATIONS USED IN THIS MANUAL ABS Anti–Lock Brake System ALR Automatic Locking Retractor A/T Automatic Transaxle ATF Automatic Transmission Fluid BDC Bottom Dead Center BTDC Before Top Dead Center Calif.

Indicates the condition of the connector of ECU during the check. INTRODUCTION HOW TO TROUBLESHOOT ECU CONTROLLED – SYSTEMS IN–31 HOW TO USE THE DIAGNOSTIC CHART AND INSPECTION PROCEDURE 1. For troubleshooting, diagnostic trouble code charts or problem symptom charts are provided for each circuit with detailed inspection procedures on the following page. 2. When all the component parts, wire harnesses and connectors of each circuit except the ECU are found to be normal in troubleshooting, then it is determined that the problem is in the ECU.

As some tachometers are not compatible with this Ignition system, we recommend that you confirm the compatibility of yours before use. 3. ADJUST IGNITION TIMING (a) Using SST, connect terminals TE1 and E1 of the data link connector 1. SST 09843–18020 HINT: After engine speed is kept at 1,000 – 1,300 rpm for 5 seconds, check that it returns to idle speed. (b) Using a timing light, check the ignition timing. Ignition timing: 10B BTDC @ idle (Transmission in neutral position) EG1–19 5S–FE ENGINE – ENGINE MECHANICAL (c) Loosen the bolt (California) or 2 bolts (except Califor– nia), and adjust by turning the distributor.

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Aerofoil Sections: Results from Wind-Tunnel Investigations, Theoretical Foundations by Friedrich Wilhelm Riegels


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