A320 Landing with Slats and Flaps Jammed (QRH Series)

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You are putting plenty of effort dear Captain and what I like about your videos are very standard Airbus philosophy of management of abnormal operations. The conceptual informations are very precise and subjective which makes watching your videos more interesting and educational. I think I wrote similar comments on your other videos. Best wishes. Thank you for your time and dedication.

aimhigheagle
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Ur doing a great work sharing ur experience on YouTube so everyone across the globe gets to know more of flying & handling emergency!
Can think of discussing all the emergencies that u practice in simulator..

joydasgupta
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Why aren’t you the most famous guy explaining the A320 failures so well

rumpadas
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Thank you Captain! Great effort and work done by you.

salmansaeed
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Good job explaining SLATS FLAPS JAMMED problem and very entertaining. I wished my sim instructor explained it to me that way…

harrismagallanes
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The recommended diversion speed is LRC 😉

lucasassuncao
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thanks again Capt. SQ
I think there is no recommended diversion speed, we have only maximum speed depend on flaps position

mustafaelbaz
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This is really good stuff! Very good instructing!!

tordenbob
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Make more video on emergency handling of A320.. 👍👍

joydasgupta
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Good job, just that after take off check list is no more there, it’s become an acceleration flow.

nishantchander
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Diversion speed is cost index zero or previous cost index. Depends MSN

jasper_north
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The function of wing tip brake to hold and stop rotation of flap/slat transmission shaft when slat/flap control computer sense asymmetry, uncommanded or runways condition of flap/slat.
Function of Wing tip brake
WTB is electrical control and hydraulic actuated component. WTB mainly consist of friction disc, piston and solenoid valve.
When Solenoid valve de-energized hydraulic fluid pressure not acting on piston. Due to absence of piston force on friction disc transmission shaft turns freely.
When Solenoid valve Energized hydraulic fluid pressure act on piston. Piston apply force on friction disc which hold transmission shaft.
Solenoid valve get energization signal from slat/flap control computer.
The function of ( Pressure off brake) POB and WTB is same. Both apply brake and hold transmission shaft.

onefive
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Hi Captain. Thanks for the videos, I have two questions please to ask you: In case as shown here in this video appear on the status Vref+10 knots, it means Vls + 10 in config full ? Is that right ? And in case landing will be in flap 3 ? How do you convert vref +10 in the correct vapp ? 

Second question is please: in case youre doing a go around in flap 3 you go directly at flap 1, is that right ? In case you're doing in flap full are you going in flap 3 and then 1 ? Is that correct ? ( of course Im talking in normal operations, not in this case as shown in the video ) Thanks a lot,

eugeniocoschignano
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Nice job Captain. I have two questions.
1. What simulator are you using?
2. Please make a video about the new TCAS (NEO) memo item.
Thanks

jtrimarchi
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Hi Capt, allow me to ask your opinion on the selection of speed after the landing configuration is set. Do you select the Vapp or let the Vapp be managed? The procedure does not state on how to decelerate to Vapp. If the Vapp is selected, GSmini function will not be activated for the approach. Appreciate your reply.

winhoeliew
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Just rode a plane where this happened. Landed safely

natureofnow
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With double slat channel failure…do you select FL 1-2-3-GEAR? IN CASE ALTN DIECT LAW…

jasper_north
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Where can you find the fuel consumption for a certain altitude?

harpertwelve
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In this situation should pilot declare emergency or not(only slat or flap jam condition)? there is no land asap in status, so i wonder your thought? ^^

처음처럼-cb
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didnt like the intro but then i really liked the content!

flightfred