W DOC AIRBUS | TSM A320F

77-20 (CFMI) - TEMPERATURE


    77-20-00 (CFMI) - TEMPERATURE

  • PB.201 TEMPERATURE - FAULT ISOLATION PROCEDURES
    • 77-20-00-810-803-A [CFMI] [8]
      Loss of the EGT Thermocouple Signal to the ECU on Engine 1
    • 77-20-00-810-804-A [CFMI] [8]
      Loss of the EGT Thermocouple Signal to the ECU on Engine 2
    • 77-20-00-810-805-A [CFMI] [8]
      Loss of the T3 Thermocouple Signal - Engine 1 - Channel A and Channel B
    • 77-20-00-810-806-A [CFMI] [8]
      Loss of the T3 Thermocouple Signal - Engine 2 - Channel A and Channel B
    • 77-20-00-810-809-A [CFMI] [8]
      Loss of the T3 Thermocouple Signal - Engine 1 - Channel A
    • 77-20-00-810-810-A [CFMI] [8]
      Loss of the T3 Thermocouple Signal - Engine 2 - Channel A
    • 77-20-00-810-811-A [CFMI] [8]
      Loss of the T5 Sensor Signal to the ECU on Engine 1
    • 77-20-00-810-812-A [CFMI] [8]
      Loss of the T5 Sensor Signal to the ECU on Engine 2
    • 77-20-00-810-822-A [CFMI] [8]
      Loss of the T5 Sensor Signal to the ECU on Engine 1
    • 77-20-00-810-823-A [CFMI] [8]
      Loss of the T5 Sensor Signal to the ECU on Engine 2
    • 77-20-00-810-826-A [CFMI] [8]
      Loss of the EGT Thermocouple Signal to the ECU on Engine 1
    • 77-20-00-810-827-A [CFMI] [8]
      Loss of the EGT Thermocouple Signal to the ECU on Engine 2
    • 77-20-00-810-828-A [CFMI] [8]
      Loss of the T3 Thermocouple Signal - Engine 1 - Channel B
    • 77-20-00-810-829-A [CFMI] [8]
      Loss of the T3 Thermocouple Signal - Engine 2 - Channel B
    • 77-20-00-810-830-A [CFMI] [8]
      The EGT indication fluctuates while other parameters are stable on Engine 1
    • 77-20-00-810-831-A [CFMI] [8]
      The EGT indication fluctuates while other parameters are stable on Engine 2
    • 77-20-00-810-832-A [CFMI] [8]
      Engine Thrust Levers not Set at Correct Position