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Q330830

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  • Q330830

    Hi Everyone,

    For the answer on question 330830 I would assume that a fuel flow of 5420 kg/h would be a typical total fuel flow (for Both engines) at least if we look at LRJT data, not one engine.

    This would mean that the fuel flow for one engine equals 2710kg/h thus an endurance of 2h20 min @ 6365 kg fuel remaining per wing.

    Can someones please clarify?

    Thanks
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