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You are here: home->amg->C02->C.8.1.7.1.A.1
8171
When determining the empty weight of an aircraft, certificated under current airworthiness standards (14 CFR Part 23), the oil contained in the supply tank is considered
| | A) the same as the fluid contained in the water injection reservoir. |
| | B) a part of the empty weight. |
| | C) a part of the useful load. |
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