Timeline for Why does the A320’s maximum allowable aileron deflection decrease, rather than increase, when the flaps are extended?
Current License: CC BY-SA 4.0
13 events
| when toggle format | what | by | license | comment | |
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| Jun 17, 2020 at 8:28 | history | edited | CommunityBot |
Commonmark migration
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| Mar 9, 2019 at 3:01 | history | tweeted | twitter.com/StackAviation/status/1104215504049369089 | ||
| Feb 28, 2019 at 17:39 | answer | added | Peter Kämpf | timeline score: 8 | |
| Feb 28, 2019 at 9:34 | comment | added | Manu H | You may add drawing of the aileron and flaps to clarify your description. | |
| Feb 27, 2019 at 23:40 | comment | added | fooot | Effectiveness changes with airspeed and aircraft configuration so it can't be assumed to only be a result of authority. The 737 is also not fly-by-wire so changing authority based on flap position would be more complex. | |
| Feb 27, 2019 at 23:34 | comment | added | Vikki | @PeterKämpf: The latter. | |
| Feb 27, 2019 at 23:29 | comment | added | Peter Kämpf | Would this answer be sufficient or do you need more information? | |
| Feb 27, 2019 at 22:43 | comment | added | Vikki | @fooot: ...which is an indirect measure of aileron effectiveness, and, therefore, the available aileron authority. | |
| Feb 27, 2019 at 22:42 | comment | added | fooot | I'm not seeing where you're getting allowable aileron deflection from that table. It looks to me like it's just listing the control wheel input needed for the different conditions. | |
| Feb 27, 2019 at 22:35 | review | Close votes | |||
| Mar 1, 2019 at 9:24 | |||||
| Feb 27, 2019 at 22:22 | comment | added | Vikki | @fooot: Not only that, it's in the portion of the references that is specifically quoted in the question itself. | |
| Feb 27, 2019 at 22:20 | comment | added | fooot | Where's the reference for the 737 behaving in the opposite way? Is it somewhere in the references in the linked question? | |
| Feb 27, 2019 at 21:57 | history | asked | Vikki | CC BY-SA 4.0 |