I think it might help the discussion if certain speculations are clarified:
Pressurisation: The pressurisation controller allows the cabin to climb (and descend) at a much lower rate than the actual aircraft, typically less than 500 feet per minute. The aircraft itself can easily climb and descend at >3000 fpm. This is done to minimise discomfort to pax ears.
Typical cruise pressure differential is about 8psi (Pounds/Sq in) - equivalent to about an 8000ft cabin. That is why airliners are tubular with hemispherical pressure domes at either end and the underfloor cargo area cannot be independently depressurised. I'll leave it as an exercise to calculate how many thousands of tons of force is on the skin of the fuselage pressure vessel, but that force is why even a tiny bomb can have a big impact. This cyclical force once per flight is also a significant source of metal fatigue and is one limiter on the safe life of the aircraft.
Fly By Wire (FBW): Yes, the B777 does have FBW computer enhancements to the flight controls. But like all Boeings there is always a direct mechanical connection between the control yokes/pedals and the flight control surface hydraulic actuators. In the event of some runaway FBW/autopilot activity (or the hypothetical "remote control"), this direct steel cable control can overpower any autoflight control input.
This Boeing architecture is VERY different to an Airbus. In a typical Airbus, there is NO manual/direct connection - the joystick is used by the crew to inform the flight control computers what they want to do, and if the computer agrees then it moves the control surfaces. Even in degraded modes the pilot is still essentially flying through the computer.
I find it interesting that in all the events where modern airliners have allegedly been "remote controlled", not a single one has involved an Airbus, always a Boeing.