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Colgan 3047 NEW

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I think I saw it

Severe ice is rare. Most guys who say they've seen it are mistaken.
Coming out of Pittsburg winter 78 in the L-188. In frezzing rain, the build up was above what the windshield would handle. FE was running the wings and tail heat at maximum cycle, ie do the wings, then do the tail, back to the wings. The hot air kept the wings clean, except where the support structure of the wing did not have heat. When you looked at the wing it was like an x-ray showing all the ribs and stringers behind the leading skin. The inlet scoops on the prop dome where all covered in ice even though the prop dome had continous heat. Climbed out of it and continued out trip. I had had seen a lot ice flying P-3's over the North Atlantic in the winter, but never anything like this. I think I remember in L-188 GS, the instructor said the L-188 was certified for flight in severe icing. But I never saw it in writing.
 
With all due respect, Auburn- and that means quite a bit of respect- what about knowing the limits of an airplane you've never flown, and what you can and can't do with it?

Looking at the top 30 on Piedmont's seniority list, I'm guessing the aggregate experience on the Dash 8 is almost half a million flight hours alone. We have captains with almost 20K in type. Not a single one of them has put one in because they didn't know the capabilities of the plane in ice, and I guarantee every one of them has seen truly severe icing.

The plane is exceptionally capable.

Agreed.

Every type of anti/deicing system has its plusses and minuses. While I agree that, by and large, hot wings provide outstanding protection against ice accretion, that does not mean that some boot equiped aircraft are not exceptionally capable.

I have flown the ATR and the Dash (100/200/300) through very challenging icing conditions that occurred in nearly all phases of flight. I have found over and over again that the Dash 8 models I fly are honest and predictable with ice on the airplane and exceptionally effective at removing it from the critical surfaces. That being said, I know that all airplanes have their limits, and the Dash is no exception. But I have no qualms whatsoever when it comes to operating the airplane in those conditions.
 
This is going to turn out a lot simpler than everyone is theorizing. Watch your airspeed whether or not you are in icing conditions and you won't fall out of the sky. Multiengine turboprops and jets have load of excess power. I cannot imagine a situation where there isn't enough excess power at low altitudes to keep the airspeed high enough. Follow the manufacturers' recommendations and you will be ok.
 
I have flown the ATR and the Dash (100/200/300) through very challenging icing conditions that occurred in nearly all phases of flight. I have found over and over again that the Dash 8 models I fly are honest and predictable with ice on the airplane and exceptionally effective at removing it from the critical surfaces.

Agree that the smaller dashes are exceptional in ice (though I have to wonder now how close I've been to catastrophe in the past). If memory serves, the airfoils on the 400 are not of the same design as the ones on the 1/2/3 models.

I should add that by exceptional, I don't mean invincible. I've seen climb capability KTFO several times crossing the Cascades.
 
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This is going to turn out a lot simpler than everyone is theorizing. Watch your airspeed whether or not you are in icing conditions and you won't fall out of the sky. Multiengine turboprops and jets have load of excess power. I cannot imagine a situation where there isn't enough excess power at low altitudes to keep the airspeed high enough. Follow the manufacturers' recommendations and you will be ok.

Yes, also while I was flying a 1900D model my Captain gave me a great tip that I have passed on to many of my FO's. While in cruise in icing conditions simple reach over and bug your Airspeed to what your cruise IAS reads. This is a easy way to notice if your airspeed bleeds off.
I have seen it slowly bleed off to look and see that I was in rapid building clear Ice at night.

So if your in cruise flight in icing use that Airspeed bug to your advantage.
 
This is going to turn out a lot simpler than everyone is theorizing. Watch your airspeed whether or not you are in icing conditions and you won't fall out of the sky. Multiengine turboprops and jets have load of excess power. I cannot imagine a situation where there isn't enough excess power at low altitudes to keep the airspeed high enough. Follow the manufacturers' recommendations and you will be ok.

If you increase power and airspeed on approach in the ice you also increase downwash, which is a leading cause of tailplane stalls.
 
Maybe it was 180 degrees because they were in a spin, maybe even a flat spin at the time of impact. That would also explain the severe roll and pitch movements. A spin on an FDR probably will take time to figure out if that is what it was. I thought about a tail stall, but doubt that. Who knows.

is the dash 8 at all recoverable from a spin?
 
Just read a news article that suggested the crew might have been doing a 180 degree turn - a standard procedure to shed the ice. Pulling the nose up or pushing it over is another common technique. Of course the stall shaker make have come on which points the airplane towards the ground. "God love 'em"
 
Chealander says the preliminary investigation indicates the autopilot was still on when the plane crashed.


Interesting.
 
is the dash 8 at all recoverable from a spin?


In the simulator, yes.

The rudder (both, really) is (are) ginormous. It was a JFNA part of a CQ once, where the instructor let us play for 20 minutes. We simulated both engines in reverse in flight, and the plane fully departed controlled flight. It was wild.

But that doesn't really apply here...

The rudder has so much authority single engine takeoffs are possible in the sim (with enough runway). ** Now that I think about it, any multiengine plane could do that...
 
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If you increase power and airspeed on approach in the ice you also increase downwash, which is a leading cause of tailplane stalls.

That is true and would be relevant if this were a tailplane stall. However, do you actually believe that this crew was unlucky enough to be the first, out of thousands of flights in this aircraft type, to encounter conditions conducive to a tail stall in an airplane that has never had one before? It's going to turn out that this airplane simply stalled. The reason why is another matter which will become known in time.

In 2001 there was a Comair Brasilia in FL that was flying along with the autopilot on and the pilots weren't paying attention to the airspeed. They encountered some ice at 17000 feet, the airspeed decayed, the autopilot disconnected when it couldn't compensate anymore and the airplane departed controlled flight with wild pitch and roll gyrations just like the accident we are currently discussing. That crew was lucky enough to recover at 10,000 feet with serious structural damage.

As I said, watch your airspeed, follow the manufacturer's, and your training provider's, recommendations and you will be fine barring any major mechanical malfunction.
 
That is true and would be relevant if this were a tailplane stall. However, do you actually believe that this crew was unlucky enough to be the first, out of thousands of flights in this aircraft type, to encounter conditions conducive to a tail stall in an airplane that has never had one before? It's going to turn out that this airplane simply stalled. The reason why is another matter which will become known in time.

In 2001 there was a Comair Brasilia in FL that was flying along with the autopilot on and the pilots weren't paying attention to the airspeed. They encountered some ice at 17000 feet, the airspeed decayed, the autopilot disconnected when it couldn't compensate anymore and the airplane departed controlled flight with wild pitch and roll gyrations just like the accident we are currently discussing. That crew was lucky enough to recover at 10,000 feet with serious structural damage.

As I said, watch your airspeed, follow the manufacturer's, and your training provider's, recommendations and you will be fine barring any major mechanical malfunction.

Are you serious? You can't make that assumption based on your crazy logic.
 

Almost every crash is a first of it's kind. If you applyed your logic to these below and many others then these accidents wouldn't of happened the way they actually did. Anyone else care to add other flights?

US Air flight 1549: Dual engine failure by birds.
American flight 587: Rudder comes off.
United flight 232: Catastrophic hydraulic failures.
Alaska Air flight 261: Jackscrew in tail.
 
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Almost every crash is a first of it's kind. If you applyed your logic to these below and many others then these accidents wouldn't of happened the way they actually did. Anyone else care to add other flights?

US Air flight 1549: Dual engine failure by birds.
American flight 587: Rudder comes off.
United flight 232: Catastrophic hydraulic failures.
Alaska Air flight 261: Jackscrew in tail.

No, almost every crash is something that has already happened many times previously. The accidents that you cited are the exceptions. There is a proven scientific principle that the simplest explanation is most often the correct one. In this case, no one was reporting any unusual icing, the airplane departed controlled flight with pitch and roll excursions, and impacted the ground in such a way as to indicate a possible spin. People want to believe that this was something unusual because they find it difficult to believe that a 2 man crew could let the airplane stall. It has happened before. I am also not saying that icing had no part in this.

And with a tail stall you don't have the roll gyrations because the wing is still flying so you still have roll control. At least that is my understanding.
 
No, almost every crash is something that has already happened many times previously. The accidents that you cited are the exceptions. There is a proven scientific principle that the simplest explanation is most often the correct one. In this case, no one was reporting any unusual icing, the airplane departed controlled flight with pitch and roll excursions, and impacted the ground in such a way as to indicate a possible spin. People want to believe that this was something unusual because they find it difficult to believe that a 2 man crew could let the airplane stall. It has happened before. I am also not saying that icing had no part in this.

And with a tail stall you don't have the roll gyrations because the wing is still flying so you still have roll control. At least that is my understanding.

That would be Occam's Razor... A philosophical principle but usually correct nonetheless.
 
Wikipedia says the Dash 8 Q400 entered service in 2000, and there are currently 140 in service. That's far from a proven design. The 737 was the most popular airliner in the world and was in service for 30 years before it was discovered it had a fatal problem (rudder jamming). Just because the -100, -200, and -300 can handle ice doesn't mean the -400 can. Considering NASA says the the aircraft most susceptible to tails stalls is high-wing T-tails, and considering that Lake Ontario produces some of the worst winter weather in the country (and definitely the worst in the Northeast), and considering Q400 pilots on this forum say they've experienced elevator buffeting in normal, non-icing conditions, it makes me concerned that the Q400 might have a design problem.
 
That is true and would be relevant if this were a tailplane stall. However, do you actually believe that this crew was unlucky enough to be the first, out of thousands of flights in this aircraft type, to encounter conditions conducive to a tail stall in an airplane that has never had one before? It's going to turn out that this airplane simply stalled. The reason why is another matter which will become known in time.

In 2001 there was a Comair Brasilia in FL that was flying along with the autopilot on and the pilots weren't paying attention to the airspeed. They encountered some ice at 17000 feet, the airspeed decayed, the autopilot disconnected when it couldn't compensate anymore and the airplane departed controlled flight with wild pitch and roll gyrations just like the accident we are currently discussing. That crew was lucky enough to recover at 10,000 feet with serious structural damage.

As I said, watch your airspeed, follow the manufacturer's, and your training provider's, recommendations and you will be fine barring any major mechanical malfunction.

What a fu--ing dooshbag. How 'bout you keep your libelous speculation to yourself. :rolleyes:
 
In this case, no one was reporting any unusual icing,

Not true. Delta 1988 said they had 1/4" on their windscreen, which we all know means much more ice would be building on the tail and wings if this were a plane with boots instead of heated leading edges. Also, Cactus 1442? repeatedly mentioned that they were picking up moderate rime ice and needed to get out of it. These were hot wing jets. Now imagine the Q400 with cold surfaces and imagine the ice buildup possibilities. At the surface there was sleet and freezing rain, not good and conducive to rapid ice buildup. Unless they were cycling the boots often and doing everything they could to shed ice then it was going to be much more of a factor for them than the jets in the area.
 
It's also what a bunch of Caravan pilots used to say before that thing started dropping out of the sky regularly due to ice.

Guys, the bottom line is that straight wing turboprop aircraft with "deice" boots as the method of ice removal/prevention will never be "good" icing airplanes. They are scraping the barrel of icing protection. If you think about it a system designed at trying to take care of the problem after it has already started is behind the curve from the get go. Anti ice systems designed around prevention will always be the best systems, even TKS is better.

Ultimately turboprops will only be safe in ice if they can figure out a way to efficiently and cost effectively get some hot bleed air to the wing and tail surfaces. Also, if you watch the NASA video, the use of a fixed horizontal stab that has an elevator with a movable trim tab and a straight wing with large flaps that produce lots of downwash and increase the angle of attack on the stab, are design characteristics that will always be conducive to tail stalls.

If the industry is going to continue to use these types of airplanes in icing conditions they need to be honest with the pilots they train about the capabilities and limitations of said aircraft and the pilots need to be honest with themselves about them as well. The pilots that fly these airplanes and claim they are "great" in ice say so because they are reassuring themselves and protecting their egos. They are NOT great in ice, they are just barely adequate and meet the minimum requirements.

In the Caravan we were told NEVER to lower flaps if tail plane icing was suspected and to hold an approach speed of 120 kts (15 kts above the published minimum speed in ice of 105kts) until the flare if possible. It makes me really curious as to the training practices used at Colgan on this subject.

There are only two possibilities IF this was indeed a tail stall. Either the training at Colgan was not adequate and did not adress the subject like it should have, or it was adequate and these pilots forgot/disregarded their training for whatever reason, i.e. fatigue etc.


I was always taught that the boots on a turboprop help you get out of the ice.....not stay in it and fight the ice.
 
I guess you don't like the facts as they are currently known, huh?

You don't have any facts, you just have wild speculation.
 
Chealander says the preliminary investigation indicates the autopilot was still on when the plane crashed.


Interesting.


Not on WHEN the plane crashed but up until the stick shaker activated. At which point control was returned to the flight crew because it disengages when the shaker activates. Unfortunately by that time it was too late to do much about the situation as the plane was probably already really slow. Just pointing out the facts.
 
It's going to turn out that this airplane simply stalled.
Looks like the investigation is over. NTSB can go home.

"Twenty seconds later, pilots engaged the wings' flaps — a normal landing procedure. It was then that they apparently lost control of the aircraft."

Please tell us how lowering the flaps causes a stall. Funny, I thought flaps reduced stall speed.

No, almost every crash is something that has already happened many times previously.
There's a first time for everything. Inane logic.
 
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Looks like the investigation is over. NTSB can go home.

"Twenty seconds later, pilots engaged the wings' flaps — a normal landing procedure. It was then that they apparently lost control of the aircraft."

Please tell us how lowering the flaps causes a stall. Funny, I thought flaps reduced stall speed.

Are you serious? You're a pilot? You need to go do some research. Start with this video; http://video.google.com/videoplay?docid=2238323060735779946
 
I think I remember in L-188 GS, the instructor said the L-188 was certified for flight in severe icing. But I never saw it in writing.

Haha not quite. The very definition of severe icing is that which cannot be shed with the equipment on the plane. And by that logic any icing on say, a C172, is technically severe icing :)
 

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