W DOC AIRBUS | AMM A320F

73-21 (CFMB) - CONTROLLING


    73-21-10 (CFMB) - HYDRO-MECHANICAL UNIT (HMU)

  • PB.301 CONF:[06] HYDRO-MECHANICAL UNIT (HMU) - SERVICING
  • PB.401 CONF:[06] HYDRO-MECHANICAL UNIT (HMU) - REMOVAL/INSTALLATION
  • 73-21-20 (CFMB) - T25 TEMPERATURE SENSOR

  • PB.401 CONF:[06] T25 TEMPERATURE SENSOR - REMOVAL/INSTALLATION
  • PB.601 CONF:[06] T25 TEMPERATURE SENSOR - INSPECTION/CHECK
  • 73-21-30 (CFMB) - ALTERNATOR - CONTROL

  • PB.401 CONF:[06] ALTERNATOR - CONTROL - REMOVAL/INSTALLATION
  • 73-21-40 (CFMB) - SENSOR - T12 TEMPERATURE

  • PB.401 CONF:[06] SENSOR - T12 TEMPERATURE - REMOVAL/INSTALLATION
  • PB.601 CONF:[06] SENSOR - T12 TEMPERATURE - INSPECTION/CHECK
  • 73-21-50 (CFMB) - WIRING HARNESS

  • PB.401 CONF:[06] WIRING HARNESS - REMOVAL/INSTALLATION
  • PB.601 CONF:[06] WIRING HARNESS - INSPECTION/CHECK
  • PB.801 CONF:[06] WIRING HARNESS - REPAIRS
  • 73-21-60 (CFMB) - ELECTRONIC CONTROL UNIT (ECU)

  • PB.401 CONF:[06] ELECTRONIC CONTROL UNIT (ECU) - REMOVAL/INSTALLATION
  • PB.501 CONF:[06] ELECTRONIC CONTROL UNIT (ECU) - ADJUSTMENT/TEST
  • 73-21-70 (CFMB) - TCC SENSOR

  • PB.401 CONF:[06] TCC SENSOR - REMOVAL/INSTALLATION
    • 73-21-70-000-002-A [CFMB] [10]
      Removal of the High Pressure Turbine Clearance Control (HPTCC) Sensor
    • 73-21-70-400-002-A [CFMB] [10]
      Installation of the High Pressure Turbine Clearance Control (HPTCC) Sensor
  • 73-21-80 (CFMB) - P25 PROBE

  • PB.401 CONF:[06] P25 PROBE - REMOVAL/INSTALLATION
  • PB.601 CONF:[06] P25 PROBE - INSPECTION/CHECK
  • 73-21-90 (CFMB) - IDENTIFICATION CONNECTOR

  • PB.401 CONF:[06] IDENTIFICATION CONNECTOR - REMOVAL/INSTALLATION
  • PB.501 CONF:[06] IDENTIFICATION CONNECTOR - ADJUSTMENT/TEST
    • 73-21-90-860-001-A [CFMB] [10]
      Programming of the Identification Plug (Push-Pull Design) for SAC engines
    • 73-21-90-860-001-A-01 [CFMB] [10]
      Programming of the Identification Plug (Push-Pull Design) for DAC engines