British Midland Interview Question
Guest
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I heard it from a reliable source that one of the questions that may be asked on the British Midland interview is "What are the benefits of an all flying tailplane?
My firend has an interview there and trying to prepare himself he asked me what I thought. (I guess he thinks I am most wise about things aeronautical)
Anyway, I'll impress him with my knowledge by "using a lifeline"., ie-polling ppruners, because, frankly, I don't have a clue what he's talking about, and I don't want him to realize I am not aviation's answer to Regis
Philbin.
Thanks for your help...
My firend has an interview there and trying to prepare himself he asked me what I thought. (I guess he thinks I am most wise about things aeronautical)
Anyway, I'll impress him with my knowledge by "using a lifeline"., ie-polling ppruners, because, frankly, I don't have a clue what he's talking about, and I don't want him to realize I am not aviation's answer to Regis
Philbin.
Thanks for your help...
Guest
Posts: n/a
I too had this question along with other technical questions I cant quite remember.
Caught out on the spot I replied with an honest answer,"I know what an all moving tailplane is but I'll be f*cked what the advantages are!"(well-not exactly in those words!!!!!!!)
I DID pass the interview by the way....
Caught out on the spot I replied with an honest answer,"I know what an all moving tailplane is but I'll be f*cked what the advantages are!"(well-not exactly in those words!!!!!!!)
I DID pass the interview by the way....
Guest
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Variable incidence ?
4 reasons
The requirment for large C.G. range
The need to cover a large speed range
The need to cope with possibly large trim changes due to wing leading and trailing edge high lift devices without limiting the amount of elevator remaining
The need to reduce trim drag to min
Spout that lot in an interview and you probably will not get in for being a smart arse ( no I am not, page 35,Handling the big jets, good book)
I wonder if it is copyrighted !
What am I doing its Friday night
[This message has been edited by Anti Freeze (edited 16 March 2001).]
4 reasons
The requirment for large C.G. range
The need to cover a large speed range
The need to cope with possibly large trim changes due to wing leading and trailing edge high lift devices without limiting the amount of elevator remaining
The need to reduce trim drag to min
Spout that lot in an interview and you probably will not get in for being a smart arse ( no I am not, page 35,Handling the big jets, good book)
I wonder if it is copyrighted !
What am I doing its Friday night
[This message has been edited by Anti Freeze (edited 16 March 2001).]
Guest
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Apart from being aerodynamically cleaner than the conventional tailplane/elevator set up, I understand that it overcomes the problem of control lock up or reversal at transonic speeds. I would hope that you guys do not intend to investigate the veracity of this statement.
Mike W
Mike W
Guest
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Flying tails tend to be pivoted at their aerodynamic centre, the upshot of which is that you get no torque through the pivot and no stick load (unless you stall the tailplane). Flying tails therefore will be fitted with some kind of feel system to provide feedback. This tends to be a simple spring trim on light aircraft and hydraulic or electrical autotrim on the heavier variety.




