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Badwater Bill



 
 
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  #1  
Old October 26th 08, 01:24 AM posted to rec.aviation.homebuilt
Ron Wanttaja
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Posts: 756
Default Badwater Bill

NTSB Preliminary is out:
-----------------------------------------------------------------------
NTSB Identification: WPR09LA016
14 CFR Part 91: General Aviation
Accident occurred Saturday, October 18, 2008 in Parowan, UT
Aircraft: Heisler Lancair Legacy, registration: N151HT
Injuries: 1 Fatal, 1 Serious.

This is preliminary information, subject to change, and may contain errors. Any
errors in this report will be corrected when the final report has been
completed.

On October 18, 2008, about 1400 mountain daylight time, N151HT, a Heisler
Lancair Legacy, collided with terrain shortly after takeoff from the Parowan
Airport, Parowan, Utah. The pilot was operating the airplane under the
provisions of 14 Code of Federal Regulations Part 91. The airline transport
pilot was killed and the passenger sustained serious injuries. The airplane was
substantially damaged. Visual meteorological conditions prevailed and no flight
plan was filed.

According to law enforcement personnel, the pilot owned a cabin in the Parowan
area and rented a hangar at the Parowan Airport. At the time of the accident, he
was returning to North Las Vegas Airport, Las Vegas, Nevada, where the airplane
was based.

Witnesses reported that the airplane departed from runway 04 and climbed to an
estimated 400 to 500 feet above ground level. The witnesses said that initially
they thought that the airplane was a cropduster because it remained at such a
low altitude. The airplane then entered a left turn and witnesses saw objects
fall, "...off of or out of the airplane." The airplane continued in a left turn
and lost altitude until the left wing tip impacted the ground and the witnesses
saw a cloud of dust at the area of impact.

Law enforcement personnel that initially responded to the accident site went to
the area specified by the witnesses as the location where the objects departed
the airplane. At this location, personal effects including clothing were
identified.

An inspector from the Salt Lake City, Utah, Federal Aviation Administration
Flight Standards District Office, responded to the accident scene. The debris
field was approximately 200 feet in length on flat terrain. The first identified
point of impact contained green lens fragments and the main wreckage came to
rest facing northeast. One propeller blade had separated from the propeller
assembly and was identified in the debris field.

At 1353, an aviation routine weather report (METAR) at Cedar City Regional
Airport, Cedar City, Utah, located approximately 17 nautical miles southwest of
the accident site, was reporting, in part: wind, 170 degrees at 10 knots and
gusting to 21 knots; visibility, 10 statute miles; sky condition, clear;
temperature, 73 degrees Fahrenheit; dew point, 19 degrees Fahrenheit; altimeter,
30.21 inHg. According to initial responders, the wind conditions reported at
Cedar City were consistent with winds in the Parowan area at the time of the
accident.
------------------------------------------------------

Ron Wanttaja
  #2  
Old October 26th 08, 06:58 PM posted to rec.aviation.homebuilt
john smith
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Posts: 1,446
Default Badwater Bill

In article ,
Ron Wanttaja wrote:

Law enforcement personnel that initially responded to the accident site went
to the area specified by the witnesses as the location where the objects
departed the airplane. At this location, personal effects including clothing were
identified.


I am not familiar with the Lancair design, is there a baggage door on
the side of the fuselage?
  #3  
Old October 26th 08, 08:02 PM posted to rec.aviation.homebuilt
Ron Wanttaja
external usenet poster
 
Posts: 756
Default Badwater Bill

On Sun, 26 Oct 2008 13:58:39 -0400, John Smith wrote:

In article ,
Ron Wanttaja wrote:

Law enforcement personnel that initially responded to the accident site went
to the area specified by the witnesses as the location where the objects
departed the airplane. At this location, personal effects including clothing were
identified.


I am not familiar with the Lancair design, is there a baggage door on
the side of the fuselage?


I don't believe there is one, in the stock configuration. However, there are
aftermarket products to convert a rear window into a baggage door. I do not
know if one had been installed.

http://www.aircraftersllc.com/projec...ndow/index.htm

Baggage on a stock Legacy is loaded from the cabin, over the seat backs. In
this case, the only ways for baggage to exit in flight is if a rear window
breaks out or if the canopy opens.

The stock Legacy has a front-opening canopy:

http://www.bock.co.za/assetts/images...n/DSCF2925.jpg

The Lancair that crashed at Sun-N-Fun this year had its canopy open on
takeoff...

http://tinyurl.com/5t63s6

....but the NTSB preliminary seems to minimize this as being related to the
crash, except possibly as a distraction: "During the takeoff climb a witness
said he saw the cockpit canopy moving and believed the pilot was pushing it up
and down about 6 to 12 inches. Another witness stated that shortly after takeoff
the engine lost power, the airplane continued straight and level and there was
no attempt by the pilot to return to the runway....."

Lancair claims that an open canopy on a Legacy does not affect controllability.
One Legacy owner had it happen, and reported that the only real impact was a
high noise level. However, there are anecdotal reports that conflict with this.

There is a modification available to change the Lancair to a front-hinged
canopy...

http://www.aerochia.com/kits_aft-canopy.html

.... but not only does it apparently feature a LOT of locks, the canopy should
have been the first item to depart the airframe had it come open. It would have
been found with the personal items that came out.

Ron Wanttaja




  #4  
Old October 26th 08, 08:05 PM posted to rec.aviation.homebuilt
Ron Wanttaja
external usenet poster
 
Posts: 756
Default Badwater Bill (Correction canopy hinges)

I had my terms reversed

On Sun, 26 Oct 2008 12:02:33 -0700, Ron Wanttaja
wrote:

The stock Legacy has a front-opening canopy:


Correction, front-HINGED canopy....


There is a modification available to change the Lancair to a front-hinged
canopy...


Correction, AFT-hinged canopy.

In short, the stock Lancair canopy has its hinges in the front, and opens in the
back. The airstream will limit its amount of opening in flight.


Ron Wanttaja
  #5  
Old October 26th 08, 08:09 PM posted to rec.aviation.homebuilt
Ron Wanttaja
external usenet poster
 
Posts: 756
Default Badwater Bill

Corrected version...

On Sun, 26 Oct 2008 13:58:39 -0400, John Smith wrote:

In article ,
Ron Wanttaja wrote:

Law enforcement personnel that initially responded to the accident site went
to the area specified by the witnesses as the location where the objects
departed the airplane. At this location, personal effects including clothing were
identified.


I am not familiar with the Lancair design, is there a baggage door on
the side of the fuselage?


I don't believe there is one, in the stock configuration. However, there are
aftermarket products to convert a rear window into a baggage door. I do not
know if one had been installed.

http://www.aircraftersllc.com/projec...ndow/index.htm

Baggage on a stock Legacy is loaded from the cabin, over the seat backs. In
this case, the only ways for baggage to exit in flight is if a rear window
breaks out or if the canopy opens.

The stock Legacy has a rear-opening (front-hinged) canopy:

http://www.bock.co.za/assetts/images...n/DSCF2925.jpg

The Lancair that crashed at Sun-N-Fun this year had its canopy open on
takeoff...

http://tinyurl.com/5t63s6

....but the NTSB preliminary seems to minimize this as being related to the
crash, except possibly as a distraction: "During the takeoff climb a witness
said he saw the cockpit canopy moving and believed the pilot was pushing it up
and down about 6 to 12 inches. Another witness stated that shortly after takeoff
the engine lost power, the airplane continued straight and level and there was
no attempt by the pilot to return to the runway....."

Lancair claims that an open canopy on a Legacy does not affect controllability.
One Legacy owner had it happen, and reported that the only real impact was a
high noise level. However, there are anecdotal reports that conflict with this.

There is a modification available to change the Lancair to a front-opening
canopy...

http://www.aerochia.com/kits_aft-canopy.html

.... but not only does it apparently feature a LOT of locks up forward, the
canopy should have been the first item to depart the airframe had it come open.
It would have been found with the personal items that came out.

Ron Wanttaja

  #6  
Old October 27th 08, 08:51 AM posted to rec.aviation.homebuilt
Stealth Pilot[_2_]
external usenet poster
 
Posts: 846
Default Badwater Bill

On Sun, 26 Oct 2008 12:09:54 -0700, Ron Wanttaja
wrote:


... but not only does it apparently feature a LOT of locks up forward, the
canopy should have been the first item to depart the airframe had it come open.
It would have been found with the personal items that came out.

Ron Wanttaja


it is tragic to see the number of people killed in lancairs.
canopies seem to have little to do with it.
the design seems so optimised for high speed flight that people
regularly come unstuck in the slow speed regime.

at one stage 50% of australian built lancairs had killed their
builders and passenger in slow speed flight fatal incidents.

tragic.
Stealth Pilot
  #7  
Old October 27th 08, 05:57 PM posted to rec.aviation.homebuilt
Gezellig
external usenet poster
 
Posts: 463
Default Badwater Bill

On Mon, 27 Oct 2008 16:51:57 +0900, Stealth Pilot wrote:

On Sun, 26 Oct 2008 12:09:54 -0700, Ron Wanttaja
wrote:

... but not only does it apparently feature a LOT of locks up forward, the
canopy should have been the first item to depart the airframe had it come open.
It would have been found with the personal items that came out.

Ron Wanttaja


it is tragic to see the number of people killed in lancairs.
canopies seem to have little to do with it.
the design seems so optimised for high speed flight that people
regularly come unstuck in the slow speed regime.

at one stage 50% of australian built lancairs had killed their
builders and passenger in slow speed flight fatal incidents.

tragic.
Stealth Pilot


I'm not doubting you but is that a pure cite or a guess. If a cite, then
Holy ****!
  #8  
Old October 28th 08, 12:15 PM posted to rec.aviation.homebuilt
Stealth Pilot[_2_]
external usenet poster
 
Posts: 846
Default Badwater Bill

On Mon, 27 Oct 2008 12:57:43 -0400, Gezellig
wrote:

On Mon, 27 Oct 2008 16:51:57 +0900, Stealth Pilot wrote:

On Sun, 26 Oct 2008 12:09:54 -0700, Ron Wanttaja
wrote:

... but not only does it apparently feature a LOT of locks up forward, the
canopy should have been the first item to depart the airframe had it come open.
It would have been found with the personal items that came out.

Ron Wanttaja


it is tragic to see the number of people killed in lancairs.
canopies seem to have little to do with it.
the design seems so optimised for high speed flight that people
regularly come unstuck in the slow speed regime.

at one stage 50% of australian built lancairs had killed their
builders and passenger in slow speed flight fatal incidents.

tragic.
Stealth Pilot


I'm not doubting you but is that a pure cite or a guess. If a cite, then
Holy ****!


that is a fact. sadly. it came up unexpectedly when an atsb chap was
grinding a spreadsheet on aircraft types to work out what were
inherently the safest designs.
sadly the lancair is at the very other end of the spectrum by a long
shot. ...in australia.

Stealth Pilot
 




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