(In the spirit of useless speculation that is way too early...) Is it
normally fair to say that, if the fuselage is more or less intact, that
would indicate some external mishap rather than internal overpressure?
(In the spirit of trying to learn something...) I see @lars_0 thinking
about liquid air management on twitter; what are we talking about?
Insulation, runoff drains and guides, and clean drip trays?
(In the spirit of adding to "things worth thinking about"...) I'll toss
refuel ops static electricity management into the hat; mostly good
grounding afaik (based only on USAF flightline experience).
