Interesting Stall Information
#12
Pilot education of tailplane icing is definitely worth the time.
A few years ago NASA came out with several videos discussing icing. They dedicated one video to tailplane icing.
Here's a link to the video on part135.com.
NASA Tailplane Icing
The video itself is very well done. It's a sobering 23 minutes.
Hog
A few years ago NASA came out with several videos discussing icing. They dedicated one video to tailplane icing.
Here's a link to the video on part135.com.
NASA Tailplane Icing
The video itself is very well done. It's a sobering 23 minutes.
Hog
#13
Banned
Joined: Jan 2006
Posts: 6,929
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From: A-320
Look guys if we were speculating a drunk crew, thats one thing but we are all educated pilots and talking about it helps, it appears that ICING is a BIG factor here. I am not saying we should be insensitive but jeez c'mon lets be realistic everyone who was flying topday was talking about what MIGHT have happened, not what did, but what might have happened.
#14
#15
I`m not speculating either....too soon to do that, however. I recall that the DC9 and in the Mad Dog, when de-icing was selected. every so often (15 minutes, I think) the de-icing would shift to the tail and when it was turned off, it automatically deiced the tail again. Another observation...the 400 wing looks way too small. I know new planes have smaller and smaller wings due to computer designs plus some magic thrown in...wonder what the wing loading on the -400 is?
Last edited by Roll Inverted and Pull; 02-13-2009 at 12:47 PM.
#16
Gets Weekends Off
Joined: Oct 2008
Posts: 265
Likes: 0
From: CL-65 F/O
I flew Beech 1900's for the USAF. While I was there, an air directive came out about tail icing. I believe this was in response to the ATR crash that was holding for approach in Chicago. There was also a video we watched from the FAA which was created by NASA.
Essentially what TZADIK posted is spot on. For T-Tail aircraft, due to the flow of air over the wing which effects the flow of air over the T-Tail, this can lead to significant ice build up on the T-Tail. In fact, if you see a little ice on the wings or cockpit, you already have TOO MUCH ice on the tail. NASA showed video of the wing and T-Tail of a plane that was flown into heavy icing. Even though the wing had maybe an inch of ice on the leading edge, the tail had 4 times as much! They also showed recovery techniques which are the same as given above and are opposite for a normal wing stall recovery.
This air directive changed how often and when to blow the boots on the Beech 1900 and the procedure was changed in our manuals.
I have to admit, I am kind of surprised that this is something new for the guys who are flying T-tails. If you don't know it.
-Fatty
Essentially what TZADIK posted is spot on. For T-Tail aircraft, due to the flow of air over the wing which effects the flow of air over the T-Tail, this can lead to significant ice build up on the T-Tail. In fact, if you see a little ice on the wings or cockpit, you already have TOO MUCH ice on the tail. NASA showed video of the wing and T-Tail of a plane that was flown into heavy icing. Even though the wing had maybe an inch of ice on the leading edge, the tail had 4 times as much! They also showed recovery techniques which are the same as given above and are opposite for a normal wing stall recovery.
This air directive changed how often and when to blow the boots on the Beech 1900 and the procedure was changed in our manuals.
I have to admit, I am kind of surprised that this is something new for the guys who are flying T-tails. If you don't know it.
-Fatty
So I was also doing some snooping around, and apparently back in December of 1989 out in Washington state, there was a United Express prop plane that went down as a result of icing, and it sounded from what information I could gather similar to what we are talking about here. It's United Express 2415 I think it was. Here is a link to the NTSB about it.
DCA90MA011
#17
Pilot education of tailplane icing is definitely worth the time.
A few years ago NASA came out with several videos discussing icing. They dedicated one video to tailplane icing.
Here's a link to the video on part135.com.
NASA Tailplane Icing
The video itself is very well done. It's a sobering 23 minutes.
Hog
A few years ago NASA came out with several videos discussing icing. They dedicated one video to tailplane icing.
Here's a link to the video on part135.com.
NASA Tailplane Icing
The video itself is very well done. It's a sobering 23 minutes.
Hog
#18
Why exactly does the tail pick up more ice? Its running in the clear well above the fuselage. It seems that it should accumulate ice in the same proportion to the rest of the airplane.
Furthermore, to recover, you are supposed to pitch up. However, if the tail is stalled anyway, depending on the depth of the stall there may be little authority left with which to push the tail down. Retracting flaps makes sense from the viewpoint that the center of pressure is forced forward as compared to its relative aft position when flaps are extended. The forward CoP puts more weight on the tail helping to push it down. Reducing thrust could work, but this is more a factor of where the engines are located relative to the lateral axis right? On a rear engine mounted A/C (not the Q, I know) with a T-tail, adding or reducing thrust would have little effect on pitch besides merely airspeed changes resulting.
Furthermore, to recover, you are supposed to pitch up. However, if the tail is stalled anyway, depending on the depth of the stall there may be little authority left with which to push the tail down. Retracting flaps makes sense from the viewpoint that the center of pressure is forced forward as compared to its relative aft position when flaps are extended. The forward CoP puts more weight on the tail helping to push it down. Reducing thrust could work, but this is more a factor of where the engines are located relative to the lateral axis right? On a rear engine mounted A/C (not the Q, I know) with a T-tail, adding or reducing thrust would have little effect on pitch besides merely airspeed changes resulting.
Last edited by bryris; 02-13-2009 at 12:56 PM.
#20
Fatty,
The ATR accident was an uncommanded aileron reversal due to ice build up beyond the reach of the (wing) boots, not tail. The ATR had transversal boots instead of annual boots. The way the system worked lured you into a false sense of security that you had an anit-ice system and not a de-ice system.
Changes were made to the physical boot itself. They were elongated. Recovery procedures were changed. Heavy ice, get out of it, no auto pilot and if you had an un-commanded roll you were to add flaps to increase the chamber of the wing.
While on approach to STL one evening in conditions much like BUF, an ATR crew (friend and coworker) almost went in on about a 4 mile final. They had just selected flaps and got a tail stall. Recovered as in above posts, with retracting flaps up, etc. Ironically this is just the opposite of a stall recovery as well as the opposite of un-commanded roll reversal. (Lots to think about!)
Since moving to turbojets, my experience is that the airflow and ramrise temperature is much different to the characteristics of icing. You still have to worry about icing but not nearly as much. I have been in icing conditions that were to me in a turboprop moderate to severe with a DC9 in front and behind calling a trace of ice. I've seen just the opposite when I'm in a jet seeing a trace with turbo-props calling much greater.
Not saying what Colgan flight encountered but it sure seems as if they had a tail stall especially after hearing (the NTSB) that they just selected Flaps 15 and started to oscillate in both pitch and roll axis. Sounds like they attempted to retract flaps and gear but it was too late.
Thoughts and prayers to the Colgan family, crew and passengers aboard.
The ATR accident was an uncommanded aileron reversal due to ice build up beyond the reach of the (wing) boots, not tail. The ATR had transversal boots instead of annual boots. The way the system worked lured you into a false sense of security that you had an anit-ice system and not a de-ice system.
Changes were made to the physical boot itself. They were elongated. Recovery procedures were changed. Heavy ice, get out of it, no auto pilot and if you had an un-commanded roll you were to add flaps to increase the chamber of the wing.
While on approach to STL one evening in conditions much like BUF, an ATR crew (friend and coworker) almost went in on about a 4 mile final. They had just selected flaps and got a tail stall. Recovered as in above posts, with retracting flaps up, etc. Ironically this is just the opposite of a stall recovery as well as the opposite of un-commanded roll reversal. (Lots to think about!)
Since moving to turbojets, my experience is that the airflow and ramrise temperature is much different to the characteristics of icing. You still have to worry about icing but not nearly as much. I have been in icing conditions that were to me in a turboprop moderate to severe with a DC9 in front and behind calling a trace of ice. I've seen just the opposite when I'm in a jet seeing a trace with turbo-props calling much greater.
Not saying what Colgan flight encountered but it sure seems as if they had a tail stall especially after hearing (the NTSB) that they just selected Flaps 15 and started to oscillate in both pitch and roll axis. Sounds like they attempted to retract flaps and gear but it was too late.
Thoughts and prayers to the Colgan family, crew and passengers aboard.
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