Yes, we can use the aircraft for cargo lift but the maximum load is affected by temperature and altitude. The standard load distribution is as follows: on rear cabin floor = 310 kgs, on LH forward cabin floor 150 kgs. In the rear hold 80 kgs, in the LH hold 120 kgs. In the RH hold 100 kgs. The maximum permissible wt. 2250 kgs which includes aircraft empty weight and fuel.