Use of speed brakes in flight
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However, it was always amusing to watch a new TriStar pilot attempt the 'Boeing push' for an extra smooth landing.
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God bless Sqn Ldr Gell RAF who introduced me to this valuable technique
.. it is comparatively easy to divine those of our PPRuNe band who learnt to fly more than a few decades ago ..... for my group, the precise same technique had all, bar one, solo in 4-7 hours ...
.. it is comparatively easy to divine those of our PPRuNe band who learnt to fly more than a few decades ago ..... for my group, the precise same technique had all, bar one, solo in 4-7 hours ...
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On the CRJ200 you have the problem that with WING + COWL A/I selected on, the pressure at idle thrust is not sufficient to supply both systems, so you have to increase thrust again up to a certain level. Use of speedbrakes is almost always a must in this situation, especially in the latter stages of the approach when you are descending at minimum clean speed.
Apart from this, i agree with most what has been already said on this thread regrding (mis)use of sb...
Apart from this, i agree with most what has been already said on this thread regrding (mis)use of sb...
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If you are considering 'braking the speed' then definitely in the air and level flight. If you are considering increasing ROD then in the air and in descent.
On the ground they are primarily lift dumpers.
On the ground they are primarily lift dumpers.
If you are considering increasing ROD then in the air
After all, if they increase ROD while on the ground, you are in serious trouble!!
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Yeah mate,back in the day,doing my F/O 727 time,the Cappy AND the PFE would bark at me for using them,called them the,PPPD,S...(piss poor planning device),and occasionally,more often that not get a clip around the ear,now as the skipper I cringe every time I use them.I can still hear those crusty old ba$$tards barking at me in the after life...." You little Shi$$t,you should have started the decent way back when"......I miss those days
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Hi aviator3233,
I guess this is question came from an FAA ATP test.
The correct answer is "on ground". But just reviewing the concept of speedbrake, remember that the speedbrake is a function of the flight spoilers, which are also used for rolling combined with the ailerons; the spoilers used on ground are called ground spoilers, they are spoilers that only open on ground. Usually the flight spoilers are also used as "ground spoilers" while on ground, but at an higher angle than in flight. On the 737 aircraft, for instance, the speed brake lever have a flight detent and you should not extend the speedbrakes beyond this detent in flight, because beyond this detent the flight spoilers will open in an higher angle that is designed to be used only on ground. Once you land this kind of airplane, you should see this lever moving automatically to the full extended position; in this occasion, the flight spoilers will be being used as ground spoilers as I mentioned above.
So as you can see, this question is a little bit tricky. But for FAA purposes, choose the "on ground" answer.
I guess this is question came from an FAA ATP test.
The correct answer is "on ground". But just reviewing the concept of speedbrake, remember that the speedbrake is a function of the flight spoilers, which are also used for rolling combined with the ailerons; the spoilers used on ground are called ground spoilers, they are spoilers that only open on ground. Usually the flight spoilers are also used as "ground spoilers" while on ground, but at an higher angle than in flight. On the 737 aircraft, for instance, the speed brake lever have a flight detent and you should not extend the speedbrakes beyond this detent in flight, because beyond this detent the flight spoilers will open in an higher angle that is designed to be used only on ground. Once you land this kind of airplane, you should see this lever moving automatically to the full extended position; in this occasion, the flight spoilers will be being used as ground spoilers as I mentioned above.
So as you can see, this question is a little bit tricky. But for FAA purposes, choose the "on ground" answer.
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It's pretty actually pretty simple. The "stick of shame" as it was called in my youth is usually labelled SPD BRK. The clue is in the name... The faster you are going, the more difference they make.
Being high and clean at 210kts and sticking them out does not a lot more than make vibration.... At 320kts you can really alter your profile positively.
Most aircraft only use some panels for speed brakes. Some for roll augmentation, and all for lift dumping.
Being high and clean at 210kts and sticking them out does not a lot more than make vibration.... At 320kts you can really alter your profile positively.
Most aircraft only use some panels for speed brakes. Some for roll augmentation, and all for lift dumping.
All the old boys and girls from the 732 call it the lever of shame.
In modern slippery aircraft like the 738, it is the lever of necessity if you wish to meet stable approach criteria!
In modern slippery aircraft like the 738, it is the lever of necessity if you wish to meet stable approach criteria!
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Given the LOS label I offer the following mis-understanding.
B757/767. High downwind under radar home base, but could always expect a short turn in if ATC perceived it OK, and if a heavy was out on long finals. You are at minimum clean speed, 210kts. ATC gives a large descent change of altitude from FL 70 - 2000' which is a clue. Choices? Extend Spd Bks and keep speed 210kts? Select flap 1, 210kts, speed brake etc. etc. or as many newbies did, select 250kts. They had been told that to increase ROD you increased speed. Speed brakes had not featured in the education. Surely they are there for more than lift-dumping on landing & RTO's? They are a tool to be used as required.
What really did astound me was how many gung-ho top gun wannabes asked for >250kts below FL10 only to use speed brakes downwind as they struggled to slow down to min clean speed or called for flaps at max flap speed trying to remove the excess energy they had imparted to the a/c. Lessons slowly learnt.
B757/767. High downwind under radar home base, but could always expect a short turn in if ATC perceived it OK, and if a heavy was out on long finals. You are at minimum clean speed, 210kts. ATC gives a large descent change of altitude from FL 70 - 2000' which is a clue. Choices? Extend Spd Bks and keep speed 210kts? Select flap 1, 210kts, speed brake etc. etc. or as many newbies did, select 250kts. They had been told that to increase ROD you increased speed. Speed brakes had not featured in the education. Surely they are there for more than lift-dumping on landing & RTO's? They are a tool to be used as required.
What really did astound me was how many gung-ho top gun wannabes asked for >250kts below FL10 only to use speed brakes downwind as they struggled to slow down to min clean speed or called for flaps at max flap speed trying to remove the excess energy they had imparted to the a/c. Lessons slowly learnt.
Last edited by RAT 5; 19th May 2016 at 08:36.
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Select flap 1, 210kts, speed brake & V/S 1000fpm
In your scenario SPD BRK and V/S -1000 will work against each other. A/T in SPD mode (Boeing) to maintain V/S. FL CH and full boards if well above profile.