Maybe a spin recovery parachute for safety, when testing some limits ?
Highly doubt they'd put the plane anywhere near spin territory. In terms of civil aviation legislation, the aircraft needs to be in the utility category in order for pilots to put the plane in an intentional/induced spin. Certification for transport category aircraft goes up to +2.5Gs, and +2.0 Gs with flaps extended. You'd be pulling well above that limit (around +3-6Gs) recovering from a spin with a plane that heavy... The plane might land but it certainly won't be airworthy after.Maybe a spin recovery parachute for safety, when testing some limits ?
I can see how it'd work for flutter testing, since the plane would have to fly beyond Vmo/Vne in order to induce flutter, and flutter would damage the aerofoil and fuselage if sustained for long periods of time. The parachute would abruptly slow the plane right back into safe Vno territory.They use spin recovery chute for flutter testing on Gulfstream jet. It's not really to test the aircraft in a spin, it's more a way to save the aircraft if it happen. Testing the flight controller to the limit can bring unlucky surprises. Having a backup can save the day !