Hi DozyWannabe,
When A/THR is disengaged (or automatically disengages) then the thrust remains at the last setting prior to disconnect. The only way you'll end up in the situation you're describing is.....Or if they were in the climb detent at disconnect, you'd have to "jiggle" the levers and leave them in the climb detent/region - not recommended procedure in any aircraft, including "your" Boeing! |
You're right, rrr - I got myself muddled with A/THR disconnect via the FCU switch (which will, I believe, result in Thrust Lock activation). The "instinctive" switches require the levers to be set before disconnect.
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Originally Posted by dozy
When A/THR is disengaged (or automatically disengages) then the thrust remains at the last setting prior to disconnect.
The only way you'll end up in the situation you're describing is if you move the thrust levers to the climb detent after disconnecting.
Originally Posted by Altcrznav
I was going off of vilas' post. He shows a 2011 date for the bulletin.
After 15 years on the bus I am still surprised you have never been aware of such procedure as the Flight Crew Bulletins are part of the FCOM. |
CONF iture,rudderrudderrat
1. If ATHR is disengaged from ID button thrust needles will catch up with the doghnut where ever they are. To CLB if levers are in CLB. That is why you set it prior to disconnect. 2. If ATHR is disconnected from FCU, thrust will freeze in the present with thrust lock and ECAM warning. 3. If ATHR fails it will freeze with Thrust lock and ECAM. The FOB in question is very old. ACNav is unable to digest it. All this will invite another comment from bubbers44. That is his priviledge but it is not possible to conduct type rating through this channel. |
Originally Posted by vilas
If ATHR is disconnected from FCU, thrust will freeze in the present with thrust lock and ECAM warning.
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Vilas,
2. If ATHR is disconnected from FCU, thrust will freeze in the present with thrust lock and ECAM warning. 3. If ATHR fails it will freeze with Thrust lock and ECAM. "The Thrust Lock function is activated when the thrust levers are in the CL detent (or the MCT detent with one engine out), and:- The flight crew pushes the A/THR pb on the FCU, or - The A/THR disconnects due to a failure. The thrust is locked at its level prior to disconnection. Moving the thrust levers out of CL or MCT suppresses the thrust lock and gives the flight crew manual control with the thrust levers." I prefer the FCOM explanation thanks. |
CONF iture, RRR
In my reply I had assumed normal position of thrust levers in auto position which is in CLB. However if for some reason the thrust levers are not in CLB while stil in active auto thrust then thrust lock won't activate and thrust will remain at the present position when disconnected. |
All this will invite another comment from bubbers44. |
Originally Posted by Vilas
However if for some reason the thrust levers are not in CLB while stil in active auto thrust then thrust lock won't activate and thrust will remain at the present position when disconnected.
Originally Posted by Capn Bloggs
Is that an aeroplane you guys are flying or something the professor in "Back to the Future" made??
Nothing like the Boeing you know where the thrust is generally where the thrust lever is ... but was it too simplistic for Airbus ? |
Just watched Back To The Future again last week. Great flick. You may be right.
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Guess I 'll stick to a Boeing.
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Good choice!
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I must admit to a bit of misunderstanding regarding AT and bumping it into MCT.
While enroute, I bumped the levers out of CLB and into MCT thinking I'd lose AT as well and I didn't. The EPR started climbing, obviously, and putting them back into the CLB detent returned everything to normal. It was as dramatic a shift in automation levels - more of a hybrid change! but it was easily returned to the previous level. Always learning on the Bus. |
Originally Posted by Altcrznav
Always learning on the Bus.
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For the record, I was working off an old set of notes which were possibly incomplete - they didn't mention the CL/MCT detent in combination with the FCU A/THR button. I made a mistake, I put my hands up to it - no big deal.
So correct procedure has the pilot match the "doughnut" to the current thrust level before using the instinctive disconnect button - doesn't seem particularly onerous to me. The FCU button allows for a way to manually ensure that Thrust Lock mode is activated, which seems like a sensible thing to provide. |
Originally Posted by dozy
For the record, I was working off an old set of notes which were possibly incomplete
The FCU button allows for a way to manually ensure that Thrust Lock mode is activated, which seems like a sensible thing to provide. |
Originally Posted by CONF iture
(Post 8082639)
Another piece of your disinfo as no one is looking forward to activate the Thrust Lock function. That's something you want to suppress, not to activate.
Originally Posted by CONF iture
(Post 7732780)
We use [the FCU A/THR button] every time we want to arm or activate again the A/THR following a voluntary disconnection. No ABNORMAL situation involved.
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Dozy, you're so confused in your 'knowledge' that you don't even realize the difference between engaging the A/THR and activating the Thrust Lock function …
Keep showing your ignorance on this specific subject at your own pace. |
As you yourself say, disengaging A/THR using the FCU button with the thrust lever in the CL or MCT detent will trigger the Thrust Lock function, and in that post you claimed to use the FCU panel button "all the time". So if engaging Thrust Lock is to be avoided, why would you do that rather than use the "instinctive disconnect" buttons?
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Originally Posted by dozy
As you yourself say, disengaging A/THR using the FCU button with the thrust lever in the CL or MCT detent will trigger the Thrust Lock function, and in that post you claimed to use the FCU panel button "all the time". So if engaging Thrust Lock is to be avoided, why would you do that rather than use the "instinctive disconnect" buttons?
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