Bon Temps Rouler....
ne plus plus. At handoff, the airframe was rotating up, as the ascent diminished, (The PITCH on PFD showed 0, four degrees 'low'). My surmise is that the PF's initial NU input created an unwanted PITCH moment (Normal Law, protected), and that caused the STALLSTALL, (the first WRN, a 'transient'). Still sufficient for the highest g accel, though.