Owain Glyndwr;
I think the quoted sentence was introduced with JAR-25 Amendment 96/1, effective 19.05.96, incorporated in Change 15 dated 1 October 2000. It must be read in conjunction with the provision you quoted earlier, that in the demonstration of stall characteristics recovery is initiated as soon as the airplane is stalled.
Furthermore, FAA Advisory Circular AC 25-7A dated 31/3/98 states:
"If artificial stall warning is provided for any airplane configuration, it must be provide for all configurations, and continue throughout the stall until the angle of attack is reduced to approximately that at which stall warning was initiated." and -
" Stall warning tests are normally conducted in conjunction with the stall testing required by 25.103 (stall speeds) and 25.203 (stall characteristics)."
Last edited by HazelNuts39; 10th July 2012 at 15:40.
Reason: FAA AC material