Go Back  PPRuNe Forums > Flight Deck Forums > Rumours & News
Reload this Page >

Atlas Air 767 down/Texas

Rumours & News Reporting Points that may affect our jobs or lives as professional pilots. Also, items that may be of interest to professional pilots.

Atlas Air 767 down/Texas

Old 13th Mar 2019, 15:52
  #521 (permalink)  
 
Join Date: Sep 2010
Location: calif/thailand
Age: 77
Posts: 9
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by GlueBall
​​​​​​Below 10,000 feet the pilots would normally be strapped in by the shoulder harnesses, making a full slump-over into the control column less likely.
I seem to remember that ATC offered a vector around weather when the crew said which way they wanted to go they were told to descend Expedishly to 3000 could've been hooking up straps jump seater leaning forward to watch the approach thrown onto pedestal and throttle.
last747fe is offline  
Old 13th Mar 2019, 16:32
  #522 (permalink)  
 
Join Date: Jun 2001
Location: Rockytop, Tennessee, USA
Posts: 5,898
Likes: 0
Received 1 Like on 1 Post
Originally Posted by dgordon42
Jump Seat pax getting out of a 'front seat' after sampling the B767 perhaps?
(See post #327 in this thread)

Dave.
Not likely in my experience, and why would they swap seats down low approaching a line of weather?

But, most of the other scenarios including an intentional crash don't seem likely either.

There was an infamous incident in 1994 where a crewmember tried to crash a freighter:

https://en.wikipedia.org/wiki/Federa...ess_Flight_705






Airbubba is offline  
Old 13th Mar 2019, 16:42
  #523 (permalink)  
 
Join Date: Nov 2007
Location: uk
Posts: 48
Likes: 0
Received 0 Likes on 0 Posts
Sounds plausible - and remember the Voyager

Originally Posted by dgordon42
Jump Seat pax getting out of a 'front seat' after sampling the B767 perhaps?
(See post #327 in this thread)

Dave.
This scenario sounds to me the most plausible explanation for this tragedy. There is a possible similarity to the RAF Voyager incident over Turkey, which was recovered because that occurred at high altitude.

The possibility of a deliberate act seems less likely when details are compared with Germanwings; in that case the pilot was alone in the cockpit, his colleague unable to return because of the security door, and, in retrospect, the pilot had a clear history of mental illness. In this case there is no suggestion that one pilot had left the cockpit, and in addition there was, exceptionally, a third person very close by, making this flight the least likely one during which to commit suicide. Of course we do not know if any of the three individuals had any relevant medical history, and that could tilt the balance of probabilities...
golf yankee one one is offline  
Old 13th Mar 2019, 17:53
  #524 (permalink)  
 
Join Date: Aug 2000
Posts: 1,499
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by suninmyeyes



I agree with Glueball that with a standard 5 point Boeing seat harness and in turbulence an incapacitated pilot would not be able to make any forward control input let alone the hefty sustained input required to override an autopilot and pitch down 45 degrees. My only suggestion (and this is pretty remote) would be that someone could have been adjusting his seat and in turbulence it slid forward and jammed the control column forward. I hope it does not turn out to be a nefarious act as it would increase a lot of already inappropriate security restrictions on pilots.
I believe the seats on the 767 have electric adjustment.
ManaAdaSystem is offline  
Old 13th Mar 2019, 17:57
  #525 (permalink)  
 
Join Date: Jun 2001
Location: Rockytop, Tennessee, USA
Posts: 5,898
Likes: 0
Received 1 Like on 1 Post
Originally Posted by ManaAdaSystem


I believe the seats on the 767 have electric adjustment.
On a freighter? I doubt it.
Airbubba is offline  
Old 13th Mar 2019, 18:01
  #526 (permalink)  
 
Join Date: Mar 2018
Location: Florida
Posts: 12
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by ManaAdaSystem


I believe the seats on the 767 have electric adjustment.
I flew the 200/300 20 years ago and I'm pretty sure ours were all manually adjusted (I'm not saying that it wasn't a possible option, though..).
Zlinguy is offline  
Old 13th Mar 2019, 18:06
  #527 (permalink)  
 
Join Date: Jul 2013
Location: Everett, WA
Age: 68
Posts: 4,392
Received 179 Likes on 87 Posts
The shoulder portions of the five point harnesses on the 767 are the inertia type - so depending on the 'rate' it's quite feasible for a pilot to 'pitch' forward into the controls. Besides, he didn't need to suddenly 'pitch' forward - slumping forward would be sufficient and is unlikely to be fast enough to trigger the inertia reels.
Airbubba - I don't know if it was basic or an option - but as I recall the 767s I did flight tests on over the last 15 years all had electric seat adjusts - and most were new build freighters.
tdracer is offline  
Old 13th Mar 2019, 18:11
  #528 (permalink)  
 
Join Date: Jan 2008
Location: Reading, UK
Posts: 15,809
Received 199 Likes on 92 Posts
Originally Posted by Airbubba
On a freighter? I doubt it.
The airframe in question was a passenger aircraft until a few years ago.
DaveReidUK is online now  
Old 13th Mar 2019, 20:22
  #529 (permalink)  
 
Join Date: Sep 2007
Location: USA
Posts: 27
Likes: 0
Received 0 Likes on 0 Posts
Has any determination/guesstimation been made about the ceiling at the time and location of the accident? Or, the likelihood if they were IMC at the time of the "upset"?
TRey is offline  
Old 13th Mar 2019, 20:37
  #530 (permalink)  
 
Join Date: Dec 2001
Location: what U.S. calls Žold EuropeŽ
Posts: 941
Likes: 0
Received 0 Likes on 0 Posts
Below 10,000 feet the pilots would normally be strapped in by the shoulder harnesses,
Not from my jumpseat experience. Maybe 30% of the pilots do actually use them.
Having some poor weather ahead with a lot of red on the radar however, I would expect most of them to strap in properly.
Volume is offline  
Old 13th Mar 2019, 20:38
  #531 (permalink)  
 
Join Date: May 2006
Location: Here, there and everywhere
Posts: 224
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by ManaAdaSystem
I believe the seats on the 767 have electric adjustment.
Two of ours have electric adjustment and all the other have manual adjustment. All built originally as freighters. I guess it must be a customer option.
Broomstick Flier is offline  
Old 13th Mar 2019, 21:14
  #532 (permalink)  
 
Join Date: Jun 2005
Location: South of North, West of East
Posts: 30
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by tdracer
The shoulder portions of the five point harnesses on the 767 are the inertia type - so depending on the 'rate' it's quite feasible for a pilot to 'pitch' forward into the controls. Besides, he didn't need to suddenly 'pitch' forward - slumping forward would be sufficient and is unlikely to be fast enough to trigger the inertia reels.
Airbubba - I don't know if it was basic or an option - but as I recall the 767s I did flight tests on over the last 15 years all had electric seat adjusts - and most were new build freighters.
This particular 767 had manual seats.

Saludos,

SEQU
sequ is offline  
Old 13th Mar 2019, 22:02
  #533 (permalink)  
 
Join Date: Nov 2008
Location: USA
Posts: 22
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by flyingchanges
Pretty sure all wind shear warnings are inhibited at that altitude.
Predictive Windshear alerts from the weather radar should still function. Airbubba is right, reactive windshear alerts from the EGPWS are inhibited above 1500 feet AGL. So if they were responding to a WS alert at that altitude, it was from the WXR.
GroundProxGuy is offline  
Old 14th Mar 2019, 02:35
  #534 (permalink)  
 
Join Date: Nov 2007
Location: Texas
Posts: 1,919
Likes: 0
Received 1 Like on 1 Post
Originally Posted by Power
no, not if they went through KCM entry
There's no KCM to the MIA ramp areas.
MarkerInbound is offline  
Old 14th Mar 2019, 02:49
  #535 (permalink)  
 
Join Date: Nov 2007
Location: Texas
Posts: 1,919
Likes: 0
Received 1 Like on 1 Post
Originally Posted by TRey
Has any determination/guesstimation been made about the ceiling at the time and location of the accident? Or, the likelihood if they were IMC at the time of the "upset"?
Galveston was running about 2000 overcast, Hobby was 3500ish BKN and IAH was just reporting cirrus behind the weather.
MarkerInbound is offline  
Old 14th Mar 2019, 11:45
  #536 (permalink)  
 
Join Date: Jan 2008
Location: farmm intersection, our ranch
Age: 57
Posts: 206
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by GroundProxGuy
Predictive Windshear alerts from the weather radar should still function. Airbubba is right, reactive windshear alerts from the EGPWS are inhibited above 1500 feet AGL. So if they were responding to a WS alert at that altitude, it was from the WXR.
Might want to check your manual on that one.
flyingchanges is offline  
Old 14th Mar 2019, 20:11
  #537 (permalink)  
 
Join Date: Aug 2000
Posts: 1,499
Likes: 0
Received 0 Likes on 0 Posts
The NG starts to scan for predictive windshear below 2300 ft RA, and will issue warnings/cautilns below 1200 ft.
Reactive below 1500 ft.
Not the same aircraft, but probably similar WS system.
ManaAdaSystem is offline  
Old 14th Mar 2019, 21:31
  #538 (permalink)  
 
Join Date: Dec 2008
Location: America
Posts: 130
Likes: 0
Received 0 Likes on 0 Posts
Don't know if it's true, but I saw an article yesterday saying that Grieg Feith (former NTSB "Mud Stud") mentioned that "the autopilot was still engaged when the aircraft was on its rapid descent, meaning that the pilots were fighting the automation". As an old timer, I can't imagine sitting there below 10,000, watching the throttles go to 100% and the nose dropping to 49 degrees nose low without disconnecting the automation, throttles to idle, deploying the spoilers, and pulling for all I'm worth.

Last edited by Murexway; 14th Mar 2019 at 21:46.
Murexway is offline  
Old 14th Mar 2019, 21:48
  #539 (permalink)  
 
Join Date: Jul 2013
Location: Everett, WA
Age: 68
Posts: 4,392
Received 179 Likes on 87 Posts
Originally Posted by Murexway
Don't know if it's true, but I saw an article yesterday saying that Grieg Feith (former NTSB "Mud Stud") mentioned that "the autopilot was still engaged when the aircraft was on its rapid descent, meaning that the pilots were fighting the automation". As an old timer, I can't imagine sitting there below 10,000, watching the throttles go to 100% and the nose dropping to 49 degrees nose low without disconnecting the automation, deploying the spoilers, and pulling for all I'm worth.
"Disconnecting" the autopilot on a 767 is trivial - just push or pull with a few pounds of force and it disconnects (with an aural alert in case it's inadvertent). Similarly it takes about 2 lbs. force to move a throttle (4 lbs for both throttles) regardless of what the autothrottle is doing. It's also pretty easy to differentiate an autothrottle movement from a manual movement on the DFDR. There is a max A/T rate (six degrees/second at the throttle lever IIRC) so about ten seconds to go from idle to full forward (obviously less if the throttle is at an intermediate setting).
tdracer is offline  
Old 14th Mar 2019, 21:51
  #540 (permalink)  
 
Join Date: Feb 2009
Location: Seattle
Posts: 379
Likes: 0
Received 0 Likes on 0 Posts
Originally Posted by Murexway
Don't know if it's true, but I saw an article yesterday saying that Grieg Feith (former NTSB "Mud Stud") mentioned that "the autopilot was still engaged when the aircraft was on its rapid descent, meaning that the pilots were fighting the automation". As an old timer, I can't imagine sitting there below 10,000, watching the throttles go to 100% and the nose dropping to 49 degrees nose low without disconnecting the automation, deploying the spoilers, and pulling for all I'm worth.
One of the things that may need to be looked into on this is how the 767 control system responds if the pilot pushes the column while the autopilot is engaged. More recent models recognize pilot intervention via significant controller displacement as time to disconnect the autopilot. On older models the autopilot does not immediately disengage in response to pilot input. There may have been a period of time where both Hal and Row 0 were providing significant control inputs. Learning that the autopilot remained engaged would not necessarily mean that Hal was at fault.
FCeng84 is offline  

Thread Tools
Search this Thread

Contact Us - Archive - Advertising - Cookie Policy - Privacy Statement - Terms of Service

Copyright © 2024 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.