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Old 08-09-2019, 05:13 AM
  #241  
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Originally Posted by flydiamond
I hear they want to derate the engines as well. Knowing that, it’s 100% understandable why the airplane would need to undergo certification. It’s not simply seats being removed.
Anytime seats are added, removed, cabin configuration is changed etc. it requires a change in BOW and CG at a minimum. And yes, D rating the engines would require recertification and manual changes would need approval
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Old 08-09-2019, 05:15 AM
  #242  
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Originally Posted by DL31082
According to the FAA website this aircraft is still certified as a CL-600-2C10, which is a CRJ-700. Looks like they did the interior and re-painted it but didn’t actually re-certify it as an actual CRJ-550 yet.
So it’s type will still be CL-600-2C10, that’s driven by the engine code. The series will be a 550, the conversion facility will add a second supplemental data plate near the aft equipment bay stating it’s been converted to a 550 series.

A good example is N8886A, depending on what database you check it’s will say CRJ-440 or CRJ-200, it was manufactured as a 440, and converted to a 100. In either case the FAA says it’s a CL-600-2B19.
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Old 08-09-2019, 05:17 AM
  #243  
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Originally Posted by gojo
Anytime seats are added, removed, cabin configuration is changed etc. it requires a change in BOW and CG at a minimum. And yes, D rating the engines would require recertification and manual changes would need approval
Also it has to get certificated in Canada first, then the US. The original airworthiness certificate came from Canada, the supplemental will need to do the same.
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Old 08-09-2019, 05:21 AM
  #244  
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Originally Posted by Flyinlynn
Why would the feds require 2 FA’s for 50 pax? Not required by regs
FAs required are what the Feds certify. I heard it has something to do with the evacuations and the Feds feel that two are needed for the size of the aircraft. What you cited are the minimums. Doesn't mean the Feds can't ask for more if safety requires it.
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Old 08-09-2019, 05:47 AM
  #245  
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Originally Posted by Meow1215
Also it has to get certificated in Canada first, then the US. The original airworthiness certificate came from Canada, the supplemental will need to do the same.
It is already certified in Canada. Transport Canada has already signed off on it. Just waiting for the FAA
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Old 08-09-2019, 08:55 AM
  #246  
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Originally Posted by FlyingKat
FAs required are what the Feds certify. I heard it has something to do with the evacuations and the Feds feel that two are needed for the size of the aircraft. What you cited are the minimums. Doesn't mean the Feds can't ask for more if safety requires it.
Well that would be good for the FA’s employment wise and trying to run the show in the back solo doesn't sound like a good time with pax getting up to go to the self serve beverages.
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Old 08-09-2019, 10:30 AM
  #247  
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6 to 8 months is what the FAA is looking at. Probably be less if no problems come up.
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Old 08-09-2019, 10:30 AM
  #248  
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I don’t disagree at all. The question is - has the exercise been done?

Originally Posted by Excargodog
Absolutely, but seriously, how hard is it to get something that is already certified to be flown at a weight that INCLUDES that lower weight to be certified at NO MORE than that reduced gross weight.

Increasing an aircraft max TOW is an ENGINEERING ISSUE. Lowering it - at least lowering it to within its currently allowable TOW within the CG envelope, is a paperwork exercise.
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Old 08-09-2019, 10:31 AM
  #249  
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Originally Posted by FlyingKat
FAs required are what the Feds certify. I heard it has something to do with the evacuations and the Feds feel that two are needed for the size of the aircraft. What you cited are the minimums. Doesn't mean the Feds can't ask for more if safety requires it.
I hope they require 2.
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Old 08-09-2019, 01:20 PM
  #250  
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Originally Posted by pangolin
I hope they require 2.
I hope they do not require two. If they do, means less profitable (even though it is small amount) and less chance of this whole 550 thing working.
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