W DOC AIRBUS | TSM A320F

75-23 (CFMI) - ROTOR ACTIVE CLEARANCE CONTROL SYSTEM (RACC)


    75-23-00 (CFMI) - ROTOR ACTIVE CLEARANCE CONTROL SYSTEM (RACC)

  • PB.201 ROTOR ACTIVE CLEARANCE CONTROL SYSTEM (RACC) - FAULT ISOLATION PROCEDURES
    • 75-23-00-810-805-A [CFMI] [8]
      Failure of the RACC Valve on Engine 1
    • 75-23-00-810-805-B [CFMI] [8]
      Failure of the RACSB Valve on Engine 1
    • 75-23-00-810-806-A [CFMI] [8]
      Failure of the RACC Valve on Engine 2
    • 75-23-00-810-806-B [CFMI] [8]
      Failure of the RACSB Valve on Engine 2
    • 75-23-00-810-807-A [CFMI] [8]
      Loss of the feedback signal from the RAC Valve through the two channels on Engine 1
    • 75-23-00-810-808-A [CFMI] [8]
      Loss of the feedback signal from the RAC Valve through the two Channels on Engine 2
    • 75-23-00-810-809-A [CFMI] [8]
      Loss of the feedback signal from the RAC Valve through the channel A on Engine 1
    • 75-23-00-810-810-A [CFMI] [8]
      Loss of the feedback signal from the RAC Valve through the Channel A on Engine 2
    • 75-23-00-810-811-A [CFMI] [8]
      Loss of the feedback signal from the RAC Valve through the Channel B on Engine 1
    • 75-23-00-810-812-A [CFMI] [8]
      Loss of the feedback signal from the RAC Valve through the Channel B on Engine 2
    • 75-23-00-810-817-A [CFMI] [8]
      Failure of the RACC Valve on Engine 1
    • 75-23-00-810-818-A [CFMI] [8]
      Failure of the RACC Valve on Engine 2