No, no, I think they are referring to a failure. If there is a cockpit control for such I think I have never heard reference of it. I'll go over your manuals, but I don't remember ever seeing that.
If the pilot knows that the blow-up is functional, then he can operate up to 200 knots without fear. If it is not functional, then he must know the maximum operational speeds for each level of flaps as outlined in the manual. So, even with a functional blow-up device the aircraft could become damaged by operating above those speeds.
It should work the same way leaving your gear down does for the Typhoon, or P-51, except instead of shearing off there would be asymmetric deployment afterwards, or warped surfaces, or something like that.
If you want to test this just write out the levels and the maximum speeds (in knots) and then work out the conversion for mph. These speeds will be indicated speeds and operations will be below 8,000 feet, as they were originally conducted by Boone Guyton during WWII. I think his gauges would have been knots, whereas our gauges are mph I'm thinking. I think you're onto something here because when I tested it the speeds I got were not very close to the manual speeds, but I did rush through the procedure. To be sure you would want to conduct a careful, reproducible investigation.