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11-20-2005, 10:15 PM
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Join Date: Feb 2005
Location: Bakersfield ,Calyfornia
Posts: 922
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"A Bad Day at the Airport"-- crash
Date: Sat, 19 Nov 2005 13:49:07 -0700
From: "Merems" <merems@cox.net>
Subject: A very bad day at the airport
Fellow builders,
I want to share with you a very bad day at the airport.
I was attending a pancake breakfast with our local EAA chapter at La
Cholla Airpark just north of Tucson AZ. A dozen or so aircraft arrived
and another two dozen or so visitors arrived for a wonderful morning of
food and airplanes. One of the aircraft that arrived was a turbine
Legend (composite, high performance aircraft). It announced it's arrival
with a high speed flyby and landed. However when it went to takeoff,
something went wrong, very wrong. It appeared to lift off the runway
way too early (about 1/3 what you would have expected) pitch up and roll
sharply to the port side. At about 75-100' it was still nose high and
rolling sharply to its port side. Then the nose pitched down. The
aircraft was now heading towards the ground but my view became obscured by
a house and tree line (yes we do have trees in Arizona). A second
later was impact followed by smoke. Both soles on board died. No houses
or people on the ground were hurt.
Since it was a EAA breakfast fly-in there were pilots all around
speculating on what had happened. What went wrong. Some are speculating it
was a high performance takeoff the pilot lost control due to the torque
effect and the 700+ horse power engine. I don't know if we will ever
know. 15 years earlier an RV-4 pilot decided to do a roll on takeoff
at this same airport and killed himself and his passenger.
I hope I never have a day like this again.
Paul
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11-21-2005, 06:10 AM
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Join Date: Jan 2005
Location: Lake St. Louis, MO.
Posts: 2,346
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Quote:
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Originally Posted by mark manda
............when it went to takeoff, something went wrong, very wrong. It appeared to lift off the runway way too early (about 1/3 what you would have expected) pitch up and roll sharply to the port side. At about 75-100' it was still nose high and rolling sharply to its port side. Then the nose pitched down..................................Paul
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The details appear eerily similiar to an Army Caribou crash some years ago. In that case, the crew failed to remove the gust locks prior to flight.
http://tinyurl.com/axoap
Rick Galati RV-6A "Darla"
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11-21-2005, 05:27 PM
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Join Date: Jan 2005
Posts: 4,283
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Quote:
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Originally Posted by Rick6a
The details appear eerily similar to an Army Caribou crash some years ago. In that case, the crew failed to remove the gust locks prior to flight. Rick Galati RV-6A "Darla"
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We can guess at accidents, but this is not correct. First the Caribou was so damaged that the control lock was never determined to be a cause, only suspect. Also the Horz tail trim jack screw can get water in it and freeze and cause an extreme out of trim condition. It was going thru flight test for a turbine conversion and already had flown +25 hours (not a first flight as some think), the pilot was a Vietnam Vet with 25,000 hours, most in Caribou's; last this tape was never to be released per the request of the family's. The tape is real and was retained by the Canadian Civil authorities or the FAA after the investigation was complete, with the approval of kin, for training purposes only. Some how it got out to the web. Tragic loss three people died , but again the gust lock is in the middle of the wind shield of the Caribou and covers the controls, a very obvious control lock and no final conclusion was possible.
The cause of the 700hp Turbine powered Lancair accident, that rolled over, has yet to be determined, control lock or otherwise. However a similar accident with a Glasair with a turbine engine occurred many years ago. It was determined to be caused by engine torque roll. I understand the P-51 would do the same thing at taking off with full power and rotated at a slow speed. I have never flown a P-51 or turbine Lancair, but the phenomena is well known with high powered single engine aircraft. In my opinion there are no similarities except they where planes, taking off, crashed and the result was several people dying.
The thing to learn or be reminded of is: Be careful when taking off and landing because the ground is close, always fly the same way per the numbers and at fly-ins resisted the temptation to do "airshow" maneuvers you have never done at higher altitudes much less low. G
Last edited by gmcjetpilot : 11-21-2005 at 05:36 PM.
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11-21-2005, 05:41 PM
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Join Date: Jan 2005
Location: Broomfield, CO
Posts: 639
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I can't get this to work: http://tinyurl.com/axoap
Tobin
__________________
RV-7 Flying since 2004
1,100 hrs+
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11-21-2005, 06:12 PM
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Join Date: Jan 2005
Location: Lake St. Louis, MO.
Posts: 2,346
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Quote:
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Originally Posted by gmcjetpilot
We can guess at accidents, but this is not correct. First the Caribou was so damaged that the control lock was never determined to be a cause, only suspect........................... last this tape was never to be released per the request of the family's. The tape is real and was retained by the Canadian Civil authorities or the FAA after the investigation was complete, with the approval of kin, for training purposes only. Some how it got out to the web. Tragic loss three people died , but again the gust lock is in the middle of the wind shield of the Caribou and covers the controls, a very obvious control lock and no final conclusion was possible....................... G
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An excellent reminder that there really are good reasons to do a
thorough preflight and to make sure the controls are free.
From R----M-----, FAA now but formerly Army Caribou Pilot. Caution this is
real ugly. Please preflight by the book. I was talking to J-- S--- who
was holding the video camera during this shot. This happened just north of
Winnipeg, and the aircraft was the first version with PT-6-67 Turboprops.
The Canadian DOT concluded that the control locks were still locked when the aircraft took off.
You who have flown the Caribou wonder how that could have happened when it is physically impossible to advance the throttles with the lock on - but this aircraft was being modified (still restricted category) and the throttle quadrant was not properly rigged to accommodate the throttle levers for the turbine engines. Three people were on board; two test pilots and an engineer.
Rick Galati RV-6A "Darla"
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11-21-2005, 06:34 PM
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Join Date: Jan 2005
Posts: 4,283
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OK thanks
Quote:
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Originally Posted by Rick6a
The Canadian DOT concluded that the control locks were still locked when the aircraft took off.
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I stand corrected. I talked to the company that produced the engine conversion and that was not their opinion. Never saw the final report, but know that the finding was not conclusive. Also jack screws have been an issue in the past. I did not know that the throttle quadrant was modified to mitigate the control lock safety features. G
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11-21-2005, 07:49 PM
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Join Date: Jan 2005
Location: Broomfield, CO
Posts: 639
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Msg to Rick
Rick,
You must have missed my last post. How do you get that link to work?
Tobin
__________________
RV-7 Flying since 2004
1,100 hrs+
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11-21-2005, 11:19 PM
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Join Date: Jan 2005
Location: 57AZ - NW Tucson area
Posts: 10,011
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Torque effect
Quote:
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Originally Posted by gmcjetpilot
The cause of the 700hp Turbine powered Lancair accident, that rolled over, has yet to be determined, control lock or otherwise. However a similar accident with a Glasair with a turbine engine occurred many years ago. It was determined to be caused by engine torque roll. I understand the P-51 would do the same thing at taking off with full power and rotated at a slow speed. I have never flown a P-51 or turbine Lancair, but the phenomena is well known with high powered single engine aircraft. In my opinion there are no similarities except they where planes, taking off, crashed and the result was several people dying.
The thing to learn or be reminded of is: Be careful when taking off and landing because the ground is close, always fly the same way per the numbers and at fly-ins resisted the temptation to do "airshow" maneuvers you have never done at higher altitudes much less low. G
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Another pilot reported that the plane in question announced over the radio a "maximum performance takeoff" before rolling.
Witnesses saw dust on the left side of the runway at the take-off point, and fresh tracks were in the dirt about 4 ft off the runway.
A leftward flight track and a left hand slow half roll all point to the torque roll effect.... As well as an airframe originally designed for an automotive V-8.
As quoted above, don't do "airshow" maneuvers when not at an airshow.....
gil in Tucson ... resident of La Cholla Airpark.....
Note - above is speculation at this time, no official cause has been determined....
Luckily, no houses or persons on the ground were hurt.... but the crash site was around 300 yards from the Pancake Breakfast location.... 
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11-22-2005, 05:05 AM
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Join Date: Jan 2005
Location: Lake St. Louis, MO.
Posts: 2,346
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Quote:
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Originally Posted by tobinbasford
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Tobin,
I really cannot answer why you can't access the link, works okay on my end. Hardly computer literate or savvy, I'm sure there must be one person that monitors this forum regularly who can offer any number of reasons you are experiencing those vexing technical problems. Sorry, I cannot help. If anyone can help Tobin, please jump in here.
Rick
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11-22-2005, 07:08 AM
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Join Date: Jan 2005
Location: St. Paul, MN.
Posts: 4,792
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Stupid question: What is a "maximum performance" takeoff?
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