Here is the procedure following the Stall Warning testing done on the ground.... One should never take a swept wing jet to Full Stall unless your a "qualified Test Pilot working directly with the factory.... Bac 1-11 and Trident are prime examples of very experienced pilots not recognizing the stall before it was unrecoverable... I think this check is done to first shaker like on a lot of other aircraft I have worked on over the years. The test is usually accomplished with the AOA being watched and referenced to the computed speed/altitude vs weight and balance at the time of check... which the AOA number calculated the 1st shaker is achieved. This requires that one of the Stall Computers say there is an impending stall... to get the secondary shaker you need both computers to agree (which include their AOA probes in agreement - i.e. 737 MAX FUBAR in Design). One should never get to this point as the push comes right beyond that AOA threshold. I worked at AirResearch as a line mechanic on the reengine from Viper to Garretts at LAX and after install this what checked, but only to the st shaker... Probably the first article was tested to the stall, the models from 1A to 700 series had wing fences and this precluded no stick push. the 800 removed the fences and installed the stick push and the stall trigger that is now on the later versions... The fences would have maybe saved their lives.... However, it is tragic and never - never go to full stall with a swept wing jet unless you are one of the young and bold...

Procedure on removal of TKS panels on 800 and later aircraft... We did this on the earlier series and this was not required....

CAUTION: After adjustment, replacement or Removal/installation of two or more wing distributor panels on one side, or either of the one piece titanium leading edge sections or adjustment, replacement or I Removal/installation of either Stall Trigger, the airplane must be test flown, using Flight Manual procedures, by a pilot familiar with the Stall Identification System and stall handling characteristics of the Series 800XP airplane, in order to check the stall characteristics.

The Stall Identification System must be operative at all times.