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Airbus Control question
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| Al Fraser 2005-02-20, 9:57 pm |
| Perhaps one for Mr Oskar??
I just received a few more MyWorld DVD's for Airbus A320 and A340. Amazing
aircraft I have to say.
In both DVD's the pilots are explaining the cockpit controls and both
mention the Auto Thrust control as being different to the usual Auto
Throttle control. They didn't go into detail so I didn't get to hear what
the actual difference is.
Can someone clarify this for me please ?
Thanks,
Al
| |
| Oskar Wagner 2005-02-20, 9:57 pm |
| "Al Fraser" <A-C.Fraser@shaw.ca> schrieb im Newsbeitrag
news:VI8Sd.444959$Xk.169076@pd7tw3no...
quote:
> Perhaps one for Mr Oskar??
>
> I just received a few more MyWorld DVD's for Airbus A320 and A340.
> Amazing aircraft I have to say.
> In both DVD's the pilots are explaining the cockpit controls and both
> mention the Auto Thrust control as being different to the usual Auto
> Throttle control. They didn't go into detail so I didn't get to hear what
> the actual difference is.
> Can someone clarify this for me please ?
>
> Thanks,
>
> Al
There IS a significant difference. The Airbus has so called "fixed throttle"
levers which simply means that they act (in normal system operation) like
thrust limit switches. They have 5 position detents corresponding (from
below) to: REVERSE, IDLE, CLIMB, MCT/FLEX, TOGA.
It's not easy to describe the system in two words as - as said before - it
is completely different to other systems. The most significant thing is that
the throttle lever do not move when the autothrust system is working. They
will be in the climb detent throughout the whole flight. The throttle levers
have no mechanical linkage to the engines.
To clarify things a bit let's got through a normal flight sequence to
understand the operation.
After engine start everything is like in a conventional A/C. You move the
trottle levers and the engines will respond to it. So taxiing is as usual.
For T/O you set the throttle levers to the TOGA or - if reduced T/O thrust
is used - to MCT/FLEX detent.
The FADEC (Full Authority Digital Engine Control) will now supply Max T/O
thrust or reduced T/O thrust according to the FLEX temperature entered into
the FMGC. Furthermore setting the levers to the aforementioned detent will
set the FMGC in SRS mode (Speed Reference System) thus the Flight Director
will command V2 after take-off or speed at liftoff - whichever is greater.
When reaching power reduction altitude (usually 1500 ft AGL) the throttle
levers are retarded to the CLIMB detent. (one or two notches, depending on
the Take-off setting). The FADEC will now command max. climb thrust and the
Flight Guidance will revert to Managed Climb, which is basically an open
climb. Open Climb in that context means that the engines will maintain a
constant thrust setting (max. climb thrust) and the A/C speed is maintained
through elevator inputs.
As soon as cruising altitude is reached, the Flight Guidance reverts to
speed hold mode. The throttle levers remain in CLIMB detent, however thrust
is reduced to maintain the desired cruising speed. That's the strange part
when there's no throttle movement is to observe although engines are
throttling back to maintain the selected (or managed -> by FMGC) speed.
For descent nothing will change as speed control is either by elevator (Open
Descent, pwr idle) or by thrust when another descent schedule is required.
Observe that the thrust limit is always max. climb thrust.
Prior to touchdown there is a Radio Altimeter call-out "retard" at around 20
ft. (yes I know the joke about "retard" ;-)) ). That's where you just
retard the throttles to IDLE detent, and after nosewheel touchdown to
"REVERSE".
Not retarding the throttles will have two different effects, depending on
whether you're on Autoland or Manual Land.
On Autoland the power will go to idle as it is commanded through the
Autoland Sequence. However the throttle levers not being in Idle Position
will prevent the (armend of course) ground spoliers from deploying.
On a manual landing the speed will be maintained as long as the throttle
levers are in the CLIMB detent thus upon flaring the engines would rev up
and you could float down the runway for hours.. ;-)
Ok, that's it in short and I know that it sounds a bit weird. But I can
assure you that you get very quickly familiar with the system and then it's
not so weird anymore....
I must add however that it is of course possible to use manual throttle. It
is often used on final approach in gusty weather as no computer can match
the "feeling by the pants". It is then a very accurate manual thrust system
as there's no asymmetry due to improper cable tension or so.....
Sorry, it's been a bit lenghty but as I said at the beginning, it's not
possible to explain it in two words.. ;-))
--
Oskar
(retired captain)
Remember, in the great scheme of things, we're all small potatoes...
| |
| Arthur 2005-02-21, 9:56 pm |
| I think you should send Al a bill for all that info, Oskar : ))
Arthur
"Oskar Wagner" <rengaw@swissonline.ch> wrote in message
news:cvbdc5$q6b$1@news.hispeed.ch...
quote:
> "Al Fraser" <A-C.Fraser@shaw.ca> schrieb im Newsbeitrag
> news:VI8Sd.444959$Xk.169076@pd7tw3no...
>
>
> There IS a significant difference. The Airbus has so called "fixed
> throttle" levers which simply means that they act (in normal system
> operation) like thrust limit switches. They have 5 position detents
> corresponding (from below) to: REVERSE, IDLE, CLIMB, MCT/FLEX, TOGA.
>
> It's not easy to describe the system in two words as - as said before - it
> is completely different to other systems. The most significant thing is
> that the throttle lever do not move when the autothrust system is working.
> They will be in the climb detent throughout the whole flight. The throttle
> levers have no mechanical linkage to the engines.
>
> To clarify things a bit let's got through a normal flight sequence to
> understand the operation.
> After engine start everything is like in a conventional A/C. You move the
> trottle levers and the engines will respond to it. So taxiing is as usual.
>
> For T/O you set the throttle levers to the TOGA or - if reduced T/O thrust
> is used - to MCT/FLEX detent.
> The FADEC (Full Authority Digital Engine Control) will now supply Max T/O
> thrust or reduced T/O thrust according to the FLEX temperature entered
> into the FMGC. Furthermore setting the levers to the aforementioned detent
> will set the FMGC in SRS mode (Speed Reference System) thus the Flight
> Director will command V2 after take-off or speed at liftoff - whichever is
> greater.
>
> When reaching power reduction altitude (usually 1500 ft AGL) the throttle
> levers are retarded to the CLIMB detent. (one or two notches, depending on
> the Take-off setting). The FADEC will now command max. climb thrust and
> the Flight Guidance will revert to Managed Climb, which is basically an
> open climb. Open Climb in that context means that the engines will
> maintain a constant thrust setting (max. climb thrust) and the A/C speed
> is maintained through elevator inputs.
>
> As soon as cruising altitude is reached, the Flight Guidance reverts to
> speed hold mode. The throttle levers remain in CLIMB detent, however
> thrust is reduced to maintain the desired cruising speed. That's the
> strange part when there's no throttle movement is to observe although
> engines are throttling back to maintain the selected (or managed -> by
> FMGC) speed.
>
> For descent nothing will change as speed control is either by elevator
> (Open Descent, pwr idle) or by thrust when another descent schedule is
> required. Observe that the thrust limit is always max. climb thrust.
>
> Prior to touchdown there is a Radio Altimeter call-out "retard" at around
> 20 ft. (yes I know the joke about "retard" ;-)) ). That's where you just
> retard the throttles to IDLE detent, and after nosewheel touchdown to
> "REVERSE".
>
> Not retarding the throttles will have two different effects, depending on
> whether you're on Autoland or Manual Land.
>
> On Autoland the power will go to idle as it is commanded through the
> Autoland Sequence. However the throttle levers not being in Idle Position
> will prevent the (armend of course) ground spoliers from deploying.
>
> On a manual landing the speed will be maintained as long as the throttle
> levers are in the CLIMB detent thus upon flaring the engines would rev up
> and you could float down the runway for hours.. ;-)
>
> Ok, that's it in short and I know that it sounds a bit weird. But I can
> assure you that you get very quickly familiar with the system and then
> it's not so weird anymore....
>
> I must add however that it is of course possible to use manual throttle.
> It is often used on final approach in gusty weather as no computer can
> match the "feeling by the pants". It is then a very accurate manual thrust
> system as there's no asymmetry due to improper cable tension or so.....
>
> Sorry, it's been a bit lenghty but as I said at the beginning, it's not
> possible to explain it in two words.. ;-))
> --
> Oskar
> (retired captain)
> Remember, in the great scheme of things, we're all small potatoes...
>
| |
|
| Hi Oskar, may I ask you what A/C you flew? You just gave such a detailed
descritption of the Airbus thrust system, before you explained things about
Boeings. So I wonder which A/Cs you flew.
Thx!
Steve
| |
| Oskar Wagner 2005-02-22, 9:59 pm |
| "Steve" <flying2000@web.de> schrieb im Newsbeitrag
news:cvfufn$too$05$1@news.t-online.com...
quote:
> Hi Oskar, may I ask you what A/C you flew? You just gave such a detailed
> descritption of the Airbus thrust system, before you explained things
> about
> Boeings. So I wonder which A/Cs you flew.
> Thx!
> Steve
>
>
Around 100 different models of Beech, Cessna, Piper, Socata,
Pilatus,.....etc. but my guess is that these are not the ones you want to
know.. ;-)
During my airline career I flew the following types:
Douglas DC9-32/34/51
Fokker 100
B747-300 (only for 4 months due to misplanning of the crew requirements....)
Airbus A319/320/321
Airbus A330
As to my knowledge we were the only company who operated cross-qualified on
short- and longrange Airbuses. So we could do 2 or 3 days of shortrange hops
and immediately thereafter go for a nice shopping trip to JFK.. ;-)
Although most pilots unions would nowadays oppose to that it was the most
interesting and enjoyable part of my flying career.
--
Oskar
(retired captain)
Remember, in the great scheme of things, we're all small potatoes...
| |
|
| Thanks for the information!
I can imagine it was interesting to fly long- and shortrange at the same
time. And that's something Airbus advertised with - the Cross Crew
Qualification due to similiar cockpit layout.
Don't you think that's somehow dangerous? As the 320-family ACs differ quite
a lot from the 330/340-Family ACs. Many, many details you have to know about
the different models! I think that even flying the A330-200 -300,
A340-200 -300 -600 as a pilot is a little too much. So many minor details
which are different, but which of course you have to know (e.g. different
call-outs in 330 and the 340 - to give only one example)!! And then even
thinking of different company deliveries (e.g. with center tank or not -
330), I think that all these many "minor" differences can be hard to
remember and therefore be dangerous. What do you think?
steve
"Oskar Wagner" <rengaw@swissonline.ch> schrieb im Newsbeitrag
news:cvghgo$da3$1@news.hispeed.ch...
quote:
> Around 100 different models of Beech, Cessna, Piper, Socata,
> Pilatus,.....etc. but my guess is that these are not the ones you want to
> know.. ;-)
>
> During my airline career I flew the following types:
>
> Douglas DC9-32/34/51
> Fokker 100
> B747-300 (only for 4 months due to misplanning of the crew
requirements....)
quote:
> Airbus A319/320/321
> Airbus A330
> As to my knowledge we were the only company who operated cross-qualified
on
quote:
> short- and longrange Airbuses. So we could do 2 or 3 days of shortrange
hops
quote:
> and immediately thereafter go for a nice shopping trip to JFK.. ;-)
> Although most pilots unions would nowadays oppose to that it was the most
> interesting and enjoyable part of my flying career.
> --
> Oskar
> (retired captain)
> Remember, in the great scheme of things, we're all small potatoes...
| |
| Oskar Wagner 2005-02-23, 7:01 am |
| "Steve" <flying2000@web.de> schrieb im Newsbeitrag
news:cvha9u$ct4$05$1@news.t-online.com...
quote:
> Thanks for the information!
> I can imagine it was interesting to fly long- and shortrange at the same
> time. And that's something Airbus advertised with - the Cross Crew
> Qualification due to similiar cockpit layout.
> Don't you think that's somehow dangerous? As the 320-family ACs differ
> quite
> a lot from the 330/340-Family ACs. Many, many details you have to know
> about
> the different models! I think that even flying the A330-200 -300,
> A340-200 -300 -600 as a pilot is a little too much. So many minor details
> which are different, but which of course you have to know (e.g. different
> call-outs in 330 and the 340 - to give only one example)!! And then even
> thinking of different company deliveries (e.g. with center tank or not -
> 330), I think that all these many "minor" differences can be hard to
> remember and therefore be dangerous. What do you think?
> steve
>
> "Oskar Wagner" <rengaw@swissonline.ch> schrieb im Newsbeitrag
> news:cvghgo$da3$1@news.hispeed.ch...
> requirements....)
> on
> hops
>
>
Well Steve, it's not that hard. I don't think that you would do a cross
qualification over the whole range A320 to A340 but merely over two sub
ranges. We were intended to have a cross qualification A320/330 and later on
A330/A340, but not A320/A340.
According to my experience we never came across any difficulties of mixing
up different types although there are - as you state correctly - some minor
differences. We even had different layouts e.g. of aux. center tanks within
the same sub-type (A321) but this was perfectly handled through informative
sidenotes in the crew briefing documents. IMHO it's all a matter of
preparation to always be aware of the A/C under your pants.... ;-)
The most impressive difference shows up anyway when starting to taxi. You
have to make sure very quickly whether there are 17 or 30 m of wing sticking
out each side.... ;-))))
--
Oskar
(retired captain)
Remember, in the great scheme of things, we're all small potatoes...
| |
|
| Hi Oskar, thanks again for your answer.
Is it theoretically possible to have cross crew A320/A340? I thought Airbus
tried to make this possible as well, but I'm not quite sure anymore.
I just generally think that there are already so many details pilots need to
know about and be aware of (even when you just want to completely know all
the systems in a modern AC - Airbus - with all its computers and how they
work and interact) that you could easily live w/out having to focus on minor
differences of different AC models or even within one type. But I guess
you're right, it just depends on your preperation!
steve
quote:
> Well Steve, it's not that hard. I don't think that you would do a cross
> qualification over the whole range A320 to A340 but merely over two sub
> ranges. We were intended to have a cross qualification A320/330 and later
on
quote:
> A330/A340, but not A320/A340.
> According to my experience we never came across any difficulties of mixing
> up different types although there are - as you state correctly - some
minor
quote:
> differences. We even had different layouts e.g. of aux. center tanks
within
quote:
> the same sub-type (A321) but this was perfectly handled through
informative
quote:
> sidenotes in the crew briefing documents. IMHO it's all a matter of
> preparation to always be aware of the A/C under your pants.... ;-)
> The most impressive difference shows up anyway when starting to taxi. You
> have to make sure very quickly whether there are 17 or 30 m of wing
sticking
quote:
> out each side.... ;-))))
> --
> Oskar
> (retired captain)
> Remember, in the great scheme of things, we're all small potatoes...
>
>
| |
| Oskar Wagner 2005-02-23, 6:09 pm |
| "Steve" <flying2000@web.de> schrieb im Newsbeitrag
news:cvi76j$15u$03$1@news.t-online.com...
quote:
> Hi Oskar, thanks again for your answer.
> Is it theoretically possible to have cross crew A320/A340? I thought
> Airbus
> tried to make this possible as well, but I'm not quite sure anymore.
> I just generally think that there are already so many details pilots need
> to
> know about and be aware of (even when you just want to completely know all
> the systems in a modern AC - Airbus - with all its computers and how they
> work and interact) that you could easily live w/out having to focus on
> minor
> differences of different AC models or even within one type. But I guess
> you're right, it just depends on your preperation!
> steve
>
> on
> minor
> within
> informative
> sticking
>
Not only theoretically!! AS far as I know it has been evaluated within
Lufthansa some years ago but for unknown reasons (I believe pilots unions)
it has never been realized. The difference between A330 and A340 is really
minor except for the fact that it has 4 throttle levers instead of 2 ;-)
(no, of course some changes in fuel-, electric- and hydraulic system). So
whether you do A320/330 or A320/340 is not really to much of a difference.
The conversion course A330/A340 in our company took only 1 week without
flight training. Just the first 10 legs or so under supervision..... In fact
we had instructors that were qualified for the whole range from A320 to
A340.
It's definitely a great advantage to have standardized cockpit layouts as
well as flight guidance systems. If you know one, you know them all....
--
Oskar
(retired captain)
Remember, in the great scheme of things, we're all small potatoes...
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