77-32 (CFMI) - ENGINE VIBRATION INDICATING SYSTEM

77-32-34 (CFMI) - MONITORING UNIT - ENGINE VIBRATION (EVMU)

PB.401 MONITORING UNIT - ENGINE VIBRATION (EVMU) - REMOVAL/INSTALLATION
- 77-32-34-000-040-A [CFMI] [10]
  Removal of the Monitoring Unit Engine Vibration (EVMU)
- 77-32-34-400-040-A [CFMI] [10]
  Installation of the Vibration Monitoring Unit (EVMU)
PB.501 MONITORING UNIT - ENGINE VIBRATION (EVMU) - ADJUSTMENT/TEST
- 77-32-34-710-040-A [CFMI] [10]
  Operational Check of EVMU through CFDS for Advisory Indication on ECAM
- 77-32-34-869-041-A [CFMI] [10]
  Change the configuration of the Accelerometer
- 77-32-34-869-042-A [CFMI] [10]
  Acquire Unbalance Data During the Flight and Read Unbalance Data
- 77-32-34-869-043-A [CFMI] [10]
  Unbalance Parameter Acquisition on the Ground
- 77-32-34-869-044-A [CFMI] [10]
  Load Frequency Analysis
- 77-32-34-869-045-A [CFMI] [10]
  Cancel Frequency Analysis Demand
- 77-32-34-750-002-A [CFMI] [10]
  Fan Trim Balance with the EVMU (one Shot Method)
- 77-32-34-750-002-A-01 [CFMI] [10]
  Fan Trim Balance with the EVMU (Vectorial Method)