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Old 09-05-2011, 09:11 AM
  #2191  
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Originally Posted by Adam West
You cannot safely take-off below Vmcg or Vmca with a failure of the critical engine. The crew can, though, retard the throttles and safely reject the takeoff, even if refusal speed is below Vmcg. If there is a gap between V1 and rotate and the takeoff is continued, and Vmcg is less than rotate, and Vmca is less than Vlo (liftoff speed), then you're in trouble

As for the test question, I was confused on the answer as well...something like a max 10 knots reduction. Not something I've ever seen or heard of before; we had a short discussion during the interview but I can't remember the company answer...just ask a lot of questions in the tech portion and the time will fly by.

Good Luck!
It was a while ago, but IIRC, the answer on the test was 10 knots. While trying to find the answer on the interwbz later on I stumbled across another mssg board where a pilot from an operator that flies both 74s and 76's (not Atlas) stated that his company uses a max reduction of 10kts on the 74 and 6kts on the 76. And of course, it can never be less than Vmcg+1kt.

I believe a pilot from another operator stated that they use more than 10kts sometimes, but of course, never less than Vmcg+1.
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Old 09-05-2011, 09:17 AM
  #2192  
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well, looks like I got that one wrong then... I always thought V1 can never be lower than Vmcg and Vr never lower than Vmca was all I needed to know. I didn't get any indication of which I got correct and which I got wrong, at least not that I was able to find. I looked all over, and haven't been able to find a definitive number for max reduction though.. Vmcg made sense for me since on the 747 the lowest usable V1 we have is 123KIAS, which also happens to be Vmcg.. oh well.. live and learn.
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Old 09-05-2011, 09:28 AM
  #2193  
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Don't know where it comes from, Boeing?, but for Atlas, the max reduction for wet or cantaminated runway is 10 kts.
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Old 09-05-2011, 10:08 AM
  #2194  
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Originally Posted by xjtguy
It was a while ago, but IIRC, the answer on the test was 10 knots. While trying to find the answer on the interwbz later on I stumbled across another mssg board where a pilot from an operator that flies both 74s and 76's (not Atlas) stated that his company uses a max reduction of 10kts on the 74 and 6kts on the 76. And of course, it can never be less than Vmcg+1kt.

I believe a pilot from another operator stated that they use more than 10kts sometimes, but of course, never less than Vmcg+1.
Thanks guys! I learned something also...

Cheers
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Old 09-05-2011, 10:58 AM
  #2195  
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Originally Posted by Whaledriver
Don't know where it comes from, Boeing?, but for Atlas, the max reduction for wet or cantaminated runway is 10 kts.
This new fangled math is hard for me, and stuff.
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Old 09-05-2011, 11:35 AM
  #2196  
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Does anyone know if there is a reapplication wait time after an unsuccessful interview? I got a "thanks, but no thanks" letter.
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Old 09-05-2011, 12:56 PM
  #2197  
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Originally Posted by CaptainMe
Does anyone know if there is a reapplication wait time after an unsuccessful interview? I got a "thanks, but no thanks" letter.
One year...
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Old 09-05-2011, 03:03 PM
  #2198  
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Originally Posted by Whaledriver
Nope...........
Has Kasher published his opinion yet? Given the level of detail of some new aspects of the TA, it seems he has, however I haven't come across a post or a thread stating such.
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Old 09-05-2011, 04:00 PM
  #2199  
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CaptainMe... how long after you interviewed did you get the letter?

Last edited by rflight2u; 09-05-2011 at 04:51 PM.
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Old 09-05-2011, 05:44 PM
  #2200  
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Originally Posted by OverspeedCowboy
Has Kasher published his opinion yet? Given the level of detail of some new aspects of the TA, it seems he has, however I haven't come across a post or a thread stating such.
No he hasn't, but it should (I used SHOULD on purpose) be out soon.

That being said, none of the published sections of the TA, obviously, were arbitrated.
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