W DOC AIRBUS | TSM A320F

75-26 (CFMI) - TRANSIENT BLEED VALVE SYSTEM


    75-26-00 (CFMI) - TRANSIENT BLEED VALVE SYSTEM

  • PB.201 TRANSIENT BLEED VALVE SYSTEM - FAULT ISOLATION PROCEDURES
    • 75-26-00-810-801-A [CFMI] [8]
      Loss of the feedback signal from the TBV valve through the channel A on Engine 1
    • 75-26-00-810-802-A [CFMI] [8]
      Loss of the feedback signal from the TBV valve through the channel B on Engine 1
    • 75-26-00-810-803-A [CFMI] [8]
      Loss of the feedback signal from the TBV valve through the channel A on Engine 2
    • 75-26-00-810-804-A [CFMI] [8]
      Loss of the feedback signal from the TBV valve through the channel B on Engine 2
    • 75-26-00-810-805-A [CFMI] [8]
      Loss of the TBV torque motor control through the channel A on Engine 1
    • 75-26-00-810-806-A [CFMI] [8]
      Loss of the TBV torsque motor control through the channel B on Engine 1
    • 75-26-00-810-807-A [CFMI] [8]
      Loss of the TBV torque motor control through the channel A on Engine 2
    • 75-26-00-810-808-A [CFMI] [8]
      Loss of the TBV torque motor control through the channel B on Engine 2
    • 75-26-00-810-809-A [CFMI] [8]
      Failure of the TBV valve on Engine 1
    • 75-26-00-810-810-A [CFMI] [8]
      Failure of the TBV valve on Engine 1
    • 75-26-00-810-811-A [CFMI] [8]
      Failure of the TBV valve on Engine 2
    • 75-26-00-810-812-A [CFMI] [8]
      Failure of the TBV valve on Engine 2
    • 75-26-00-810-813-A [CFMI] [8]
      Loss of the feedback signal from the TBV valve through the two channels on Engine 1
    • 75-26-00-810-814-A [CFMI] [8]
      Loss of the feedback signal from the TBV valve through the two channels on Engine 2