EDIT: Specifically pressurization cycles and metal fatigue, since that's how aircraft lifespan is measured.
EDIT: Specifically pressurization cycles and metal fatigue, since that's how aircraft lifespan is measured.
Regardless, fuel burn is certainly a factor to consider when looking at savings and there are interesting studies on it (See “Fuel burn implications“ for an idea of factors [1])
[0] http://large.stanford.edu/courses/2013/ph240/eller1/ [1] https://www.purdue.edu/discoverypark/nextrans/assets/pdfs/08...
If you make one really long flight, you need more fuel - and then you need more fuel to carry that fuel (though less). Basically you need an exponential amount of fuel for more range, not linear. (It works just the same as the rocket equation, though less drastic.)
But landing and takeoff take kind of a fixed amount of fuel.
So, for short trips, the fixed amount is more - so better to fly directly.
But for really long trips, you're on the right side, the steep end of the exponential curve. Adding more range there takes a lot more fuel. So then it's smarter to put less fuel at start and make a refueling stop instead.
Fuel burn is also usually the largest component of expenditure, and is especially likely to be when looking at elderly freighters with low capital costs and relatively inefficient engines
They were loaded into a flight I was on from Costa Rica to Paris.