Given that the MZFM is 47,000 kg, the MTOM is 62,800 kg, and the MLM is 54,900 kg, assuming no performance limits and that the regulated take-off and landing masses equal the structural limits, with a DOM of 34,000 kg, an actual traffic load of 12,400 kg, a take-off fuel load of 16,000 kg, and 8,000 kg of fuel used in flight, can additional load be carried? If so, how much?
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