Originally Posted by JD_EE
rudderrat and takata, when rudderrat said or quoted "The elevator orders are progressively transferred to the THS through a low-speed integrator to decrease the drag." was this necessarily correct? Is that from documentation or a presumption?
Sorry, I'm a little bit lazzy (or too busy), as I didn't quoted the reference. It is from my notes about AMM 27-90-00, but I suppose it was from an A320 document as the g-load limits for an A330 THS is rather 1.3 / 0.5 g (instead of 1.25 / 0.5 g quoted). But both THS are basically the same thing, as far as the operating system is concerned.