Electronic AOA display still works when mechanical is inop.

[NikolaiVChr]

The AoA indexer should match it

[ph-jake]

After reading and trying to interpret GR1F-16CJ-1 "AOA SYSTEM" again, and considering that the static port failure is used to model multiple AoA sensor failure, I want to introduce the following changes to approximate what's described:

• Lock alpha-indicated to 11 deg
• Leave AoA gauge and index operational
• Replace FLCS AOA FAIL by FLCS AOA WARN
• Remove the FPM from HUD

This is what I think the text suggest, apart from the FPM. Not sure what else is/should be affected.

[Rudolf339]

I am not that familiar with the details of the f-16, but the aircraft I know use INS velocities for FPM, it's independent of the AoA instrument (or used as backup)

[ph-jake]

Yeah, the relation between AoA sensors and FPM felt sketchy to me too. So we can assume that's left in.

[NikolaiVChr]

FPM is driven by gyros, not AoA or sideslip.