Elements and Performance Criteria
- Calculate the weight and balance impact of a modification
- The requirement for aircraft weighing is determined
- The new empty weight of the aircraft is determined and it is ensured that the weight is within the predetermined limits set by the Continuing Airworthiness Management Organisation (CAMO)
- The new empty weight centre of gravity of the aircraft is calculated using the weight and moment arm data for a modification and it is ensured that the centre of gravity is within the predetermined limits set by the CAMO
- Maintenance records are updated with new figures