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You are here: home->amg->C02->C.8.1.7.3.A.1
8173
The maximum weight as used in weight and balance control of a given aircraft can normally be found
| | A) in the Aircraft Specification or Type Certificate Data Sheet. |
| | B) by adding the weight of full fuel, pilot, passengers, and maximum allowable baggage to the empty weight. |
| | C) by adding the empty weight and payload. |
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