R1:
GY earlier posted that stall warning was triggered depending on, amongst other things, F/CTL law. Is it the case that stall warning is NOT inhibited below 60kts IF you're flying anything other than normal law?
That's not mentioned in the books !!!
Vane resolver sin and cos is input for ADR, ADR generates AOA from this input if CAS =>60 Kts if not AOA=0 and NCD. This is ADR output fed into the PRIMS/SECS and FWC.
More on AOA:
ATSB TRANSPORT SAFETY REPORT
Aviation Occurrence Investigation AO-2008-070
In-flight upset
7 October 2008
VH-QPA
Angle of attack spikes
For an A330, during all phases of flight, the typical operational range of AOA is +1 degree to +10 degrees. In cruise, a typical AOA is +2 degrees.
Complete report including detailed description of polling logic.