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EN ATPL Mass and Balance Questions in English
Practise Mass and Balance
For an aircraft operated in EASA commercial air transport using individual aircraft masses, the mass and CG must be established by weighing before initial entry into service and thereafter:
When preparing to carry out the weighing procedure on an aircraft, which of the following is not required?
An aircraft may be weighed
An aeroplane must be re-weighed at certain intervals. Where an operator uses 'fleet masses' and provided that changes have been correctly documented, this interval is
For the purpose of completing the Mass and Balance documentation, the Operating Mass is considered to be Dry Operating Mass plus
An aircraft is weighed prior to entry into service. Who is responsible for deriving the Dry Operational Mass from the weighed mass by the addition of the 'operational items'?
The responsibility for determination of the mass of 'operating items' and 'crew members' included within the Dry Operating Mass lies with
To calculate a allowable take-off mass, the factors to be taken into account include:
Prior to departure an aircraft is loaded with 16500 litres of fuel at a fuel density of 780 kg/m3. This is entered into the load sheet as 16500 kg and calculations are carried out accordingly. As a result of this error, the aircraft is
An additional baggage container is loaded into the aft cargo compartment but is not entered into the load and trim sheet. The aeroplane will be heavier than expected and calculated take-off safety speeds
