jtramo wrote:
AOA has a lot of bearing on pitch and vice versa, and the aoa combined with airspeed controls the PLI (pitch limit indicator showing the pitch that will result in a stall). Pitch up and retard power as this crew did, and pitch/AOA increases to stall. They were deep stalled for 6 minutes! I suppose Im having issues conceptualizing the AOA VS Pitch as they were in straight and level flight and not an AOA driven accelerated stall. In this case critical pitch indications would not be the same as AOA but pitch stall angle would almost mirror AOA (-+chord) isnt that correct?
You didn't read my statement. My statement is that AoA referenced in the report is
NOT AVAILABLE to the crew. Additionally, no mention has been made in the report whether the
PITCH DATA referenced was being displayed on the PFD or not, only that there was a disagreement in IAS between the PFD and the standby instrument. As such, because they don't state it, then we must not assume that it was working. Conversely, we must not assume it was malfunctioning either. We simply don't have the information. My point for saying this is simple - AoA and pitch are not directly interrelated. You must have
airspeed to make AoA occur. You can be at any pitch and have an AoA of 0*. You can be at any speed and have an AoA of 0*. You can't be at any pitch and any speed and still have an AoA of 0*.
Additionally, the A330 flight laws went into the "Alternate Law" (as stated in the report) which removes most of the pitch and roll protections and in some modes removes the autotrim. As such, they are essentially flying a "dumb" airplane in this situation. So, it may be that they assumed there were protections in place that weren't, but again, without all of the information about what the PFDs were or weren't showing, we can't know that for sure.