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Forum: Tech Log

27th Apr 2015, 13:31

Replies: 34

Airbus A 321 Managed/Open DES with no A/THR.

Views: 8,308

Posted By vilas

Heavy aircraft, on top of thunderstorm and above...

Heavy aircraft, on top of thunderstorm and above REC MAX you were lining up the swiss cheese holes. Why is that?

Forum: Tech Log

11th Apr 2015, 17:22

Replies: 34

Airbus A 321 Managed/Open DES with no A/THR.

Views: 8,308

Posted By vilas

Moral? In normal situations don't pull open...

Moral? In normal situations don't pull open descent at FL410 if you are descending into a tailwind / quickly weakening headwind.
Firstly when 100kts. head wind turns into 50kts. tail wind it is not...

Forum: Tech Log

9th Apr 2015, 03:20

Replies: 34

Airbus A 321 Managed/Open DES with no A/THR.

Views: 8,308

Posted By vilas

MD80rookie I don't have to try. I have seen it...

MD80rookie
I don't have to try. I have seen it and already know. If you had used the correct terminology this discussion was not required. What you meant was that the aircraft will enter steep...

Forum: Tech Log

8th Apr 2015, 13:45

Replies: 34

Airbus A 321 Managed/Open DES with no A/THR.

Views: 8,308

Posted By vilas

MD80rookie No, I am afraid we are not saying...

MD80rookie
No, I am afraid we are not saying the same thing. Firstly I am saying opposite of what you say about the weight. Secondly when you drop the speed aircraft continues to pitch down at...

Forum: Tech Log

8th Apr 2015, 05:17

Replies: 34

Airbus A 321 Managed/Open DES with no A/THR.

Views: 8,308

Posted By vilas

MD80rookie Your explanation of low inertia is...

MD80rookie
Your explanation of low inertia is very strange. Airbus FBW does not violently pitch down to capture speed. The AP maintains a steady comfortable pitch down rate that doesn't change and...

Forum: Tech Log

4th Apr 2015, 13:54

Replies: 34

Airbus A 321 Managed/Open DES with no A/THR.

Views: 8,308

Posted By vilas

pineteam In managed descent aircraft goes...

pineteam
In managed descent aircraft goes through repressurisation(when applicable), idle thrust and geometric segments and it will try to maintain its vertical profile. ATHR will keep changing from...

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