Originally Posted by
punkalouver
I don't believe that theory. Otherwise max derate/reduced thrust would be just as likely to create a tailstrike hazard.
Which theory and why?
Here's another incident:
The tailstrike was the result of an excessive rate of rotation during the takeoff. This was exacerbated by a variable headwind component which contributed to a lift off speed that was lower than intended by the manufacturer and compounded the loss of tail clearance.
2005, a Thomsonfly 757,
https://www.fss.aero/accident-report...report_key=230