Degrees of movement of spoiler panels on take off.
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Degrees of movement of spoiler panels on take off.
On previous posts there has been intensive discussion on spoiler drag with excessive control wheel deflection on a cross wind take off. From anecdotes heard, excessive pilot control wheel input in crosswind take offs may be much more common than realised. It seems to largely stem from habits ingrained in ab-initio flight training and carried over. On the other hand perhaps the argument is trivial as aircraft are not going off the end of runways due unforeseen insidious drag.
Has anyone any specific figures on the amount of spoiler panel movement in degrees for say half wheel movement during a take off? As speed increases down the runway with constant wheel angle, do the spoilers change angle in any way - blowing down the faster the aircraft goes and so on?
Has anyone any specific figures on the amount of spoiler panel movement in degrees for say half wheel movement during a take off? As speed increases down the runway with constant wheel angle, do the spoilers change angle in any way - blowing down the faster the aircraft goes and so on?
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Originally Posted by A37575
Has anyone any specific figures on the amount of spoiler panel movement in degrees for say half wheel movement during a take off? As speed increases down the runway with constant wheel angle, do the spoilers change angle in any way - blowing down the faster the aircraft goes and so on?
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Yes i would agree.
Spoiler deflection cannot be related to IAS or something like that.
It starts at a specific point of control wheel displacement and is proportional to this.
In my opinion during some x-wind conditions you have to give much aileron input (with spoiler rise) to keep the wings level during rotation. No matter if it causes too much drag, according to the FCTM. (Still better than a wing tip touching the grass
)
Spoiler deflection cannot be related to IAS or something like that.
It starts at a specific point of control wheel displacement and is proportional to this.
In my opinion during some x-wind conditions you have to give much aileron input (with spoiler rise) to keep the wings level during rotation. No matter if it causes too much drag, according to the FCTM. (Still better than a wing tip touching the grass
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Originally Posted by Michael1282
Spoiler deflection cannot be related to IAS or something like that.
It starts at a specific point of control wheel displacement and is proportional to this.)
It starts at a specific point of control wheel displacement and is proportional to this.)
there WILL be some speed above which the hinge moment on the spoilers will overcome the capability of the actuation; whether that speed is operationally significant or not is type-dependent, but I'd expect that you'd start seeing effects at about Vmo. (below that, you typically want to have the spoilers available; less need above, so Vmo as a design speed wouldn't be a bad first guess)
Also, it is conceivable that one might vary the wheel-spoiler schedule with speed (perhaps Mach, most likely) to reflect changes in control effectiveness. (Though off the top of my head I don't *think* we do so)
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I do not have the manual in front of me, but from memory.
B757
0deg to 11deg control wheel no spoilers
11deg to 55deg control wheel, spoiler on the down going wing deploys as an inboard aileron.
On swept wing jets it is very important to have into wind aileron on take off and upto 55 deg control wheel will not increase drag.
With experience the amount of deflection required can be jugded by the amount of rudder required to keep straight.
At lift off all is revealed and then roll must be corrected if nessesary.
B757
0deg to 11deg control wheel no spoilers
11deg to 55deg control wheel, spoiler on the down going wing deploys as an inboard aileron.
On swept wing jets it is very important to have into wind aileron on take off and upto 55 deg control wheel will not increase drag.
With experience the amount of deflection required can be jugded by the amount of rudder required to keep straight.
At lift off all is revealed and then roll must be corrected if nessesary.
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A37575, a word you use implies you have picked up the wrong end of the stick in the thread you refer to:
Can you guess which one it is?
Now why do you think the discussion was about excessive use of control wheel displacement leading to spoiler displacement? The discussion was actually about using the recommended amount of control wheel into wind to prevent wing lift as opposed to using none until the wing actually lifts and then using control wheel displacement to lower it again. It therefore makes your comment read differently
.....habits as supported by current training practices and instruction to apply the correct recommended amount of control wheel displacement for a crosswind. If people are applying excessive control, then they must be stopped immediately!
On previous posts there has been intensive discussion on spoiler drag with excessive control wheel deflection on a cross wind take off.
Now why do you think the discussion was about excessive use of control wheel displacement leading to spoiler displacement? The discussion was actually about using the recommended amount of control wheel into wind to prevent wing lift as opposed to using none until the wing actually lifts and then using control wheel displacement to lower it again. It therefore makes your comment read differently
It seems to largely stem from habits ingrained in ab-initio flight training and carried over.
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