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-   -   A320 question... (https://www.airlinepilotforums.com/major/85697-a320-question.html)

80ktsClamp 01-01-2015 10:57 AM
[QUOTE=Gypsy Pilot;1793842]
Originally Posted by 80ktsClamp (Post 1793195)
Ah, you're thinking of abnormal alternate law-

I think you mean Abnormal Attitude law. :)

The aircraft remains in Abnormal Attitude Law once the aircraft has been recovered from the abnormal attitude.

GP
Thanks. :) However stabilities and yaw damping return once out of the upset attitude- that was the big discussion.

Sliceback 01-01-2015 11:10 AM
aa73 - "It bears mentioning that this particular A300 was involved in an inflight upset years earlier that also weakened the tail."




The tail failed at approx 2.03 design load factor. That is as expected.

Greg Bockelman 01-01-2015 04:00 PM
What is this Abnormal Attitude Law?

There is Normal Law, Alternate Law and Direct Law.

gringo 01-01-2015 04:22 PM
Originally Posted by Greg Bockelman (Post 1793991)
What is this Abnormal Attitude Law?

There is Normal Law, Alternate Law and Direct Law.
It's reserved for those situations where you really really really phuck things up. Hard.

Airbus Flight Control Laws

asacimesp 01-01-2015 04:42 PM
Originally Posted by Greg Bockelman (Post 1793991)
What is this Abnormal Attitude Law?

There is Normal Law, Alternate Law and Direct Law.
It's when your buddy is too drunk and being a total douchebag....Abnormal Attitude Law says you get to smack him in the nuts for baing an a$$hat.

Bwipilot 01-01-2015 06:50 PM
This thread makes me glad that I fly Boeing instead of managing a computer that flies the Airbus that I'm riding in.

Shrek 01-01-2015 08:47 PM
Originally Posted by Bwipilot (Post 1794085)
This thread makes me glad that I fly Boeing instead of managing a computer that flies the Airbus that I'm riding in.
Like you have a choice at SWA. :rolleyes:

Boomer 01-02-2015 08:26 AM
Originally Posted by asacimesp (Post 1794026)
It's when your buddy is too drunk and being a total douchebag...
I thought that was Absolut Law.

Greg Bockelman 01-02-2015 08:30 AM
Originally Posted by Bwipilot (Post 1794085)
This thread makes me glad that I fly Boeing instead of managing a computer that flies the Airbus that I'm riding in.
Like it or not, if you end up flying anything other than a 737 or older Boeing, you WILL be flying something that is being managed by a computer.

aa73 01-02-2015 08:43 AM
Originally Posted by Sliceback (Post 1793856)

The tail failed at approx 2.03 design load factor. That is as expected.
Understood. I didn't say that the previous upset caused the tail to come off, but even the NTSB hinted that it might have played a role...one of the things I think they got right.


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