KR> KR2 accident

2011-03-14 Thread STEVE bennett

  Damage: Destroyed

LOCATION
  City: LUDLOW   State: CA   Country: US

DESCRIPTION
  AIRCRAFT CRASHED UNDER UNKNOWN CIRCUMSTANCES, THE 1 PERSON ON BOARD WAS 
  FATALLY INJURED, AIRCRAFT WAS THE SUBJECT OF AN ALERT NOTICE, WRECKAGE 
  LOCATED 2 MILES FROM HECTOR NEAR LUDLOW, CA

INJURY DATA  Total Fatal:   1
 # Crew:   1 Fat:   1 Ser:   0 Min:   0 Unk:
 # Pass:   0 Fat:   0 Ser:   0 Min:   0 Unk:
 # Grnd: Fat:   0 Ser:   0 Min:   0 Unk:


OTHER DATA
  Activity: Pleasure  Phase: Unknown  Operation: OTHER


  FAA FSDO: RIVERSIDE, CA  (WP21) Entry date: 03/10/2011 

Preliminary data on KR2 crash.

Steve Bennett

ifly...@msn.com





KR> kr2 accident (long) with the facts

2010-10-12 Thread Jim Morehead
Netters,
 
To answer the question on my collapsed news gear.  It was a standard Diehl 
metal nose gear that was  sold for the VW powered standard KR.  
 
It really survived the first hard hit but the second hit was much harder.  It 
bent just below the upper socket that it fits into.,  Also it bent back about 
half way down the gear leg.  We slid down the runway on the lower bend and 
almost ware through it.  The nose wheel turned 180 degrees after we went off 
the pavement and into the dirt.  It sheared off the nose gear stops that were 
to keep it from going to far around.
 
There isn't any damage to the tire, wheel, the aluminum casting or the fire 
wall.  I'm impressed with how strong the wooden KR fuselage is!
 
The Diehl gear comes with a socket fitting that bolts to the firewall and also 
to the lower motor mount.  It doesn't show any damage.  The only damage to the 
(home made) motor mount is from the acid that ran out of the battery vent tube. 
and messed up my paint job job on the motor mount. 
 
The vertical tail was snapped off.  I have removed the elevator and carved out 
the two spars.  I have enough foam  to make the new vertical and rudder. After 
I get my Spruce order I will get on it.
 
David Goodman's E-mail with the pictures of my KR gives you a good look ot the 
bent nose gear.
 
 
Be safe everone,
 
Jim Morehead
N522PC (will fly again!)
 
 
 
 --- On Tue, 10/12/10, David Goodman <dgood...@verticalavionics.com> wrote:


From: David Goodman <dgood...@verticalavionics.com>
Subject: RE: KR> kr2 accident (long) with the facts
To: "'KRnet'" <kr...@mylist.net>
List-Post: krnet@list.krnet.org
Date: Tuesday, October 12, 2010, 3:14 PM


KrNetters,

Ted wrote:

Could you elaborate on the nose gear that collapsed?  Where did it fail?
Whose nose gear was it? Diehl?  He has two, a standard and a Corvair version
(don't know the difference). Do any recommendations come out of this
incident regarding the mounting of the nose gear?

Jim Morehead was the builder of this plane, so he final authority on the
nose gear.  It appeared to me to be a standard (VW) Diehl system.

As far as where it folded, you can take a look at link
http://sites.google.com/a/wildblue.net/goodmans/Home/2010-kr2-mishap.
There is a good photo from the side of just the nose gear located there.

We hit extremely hard on the nose on the first bounce.  I could not tell you
how hard the second hit was compared to the first, as my eyes were
completely uncaged for about one second after the first impact.  What I can
tell you is the gear did not shatter until after the second impact
nose-first of the plane onto the runway.  I know this because though my eyes
were uncaged I could still see the prop shatter on the second hit.

That the landing gear withstood the first impact is a testimony to the Diehl
gear's solid design.

Having nose-planted my own plane three years ago on a Corvair-weight gear
(which bent, but did not fail) and last year taking that same strut
off-roading at 35 KTS off a runway in California the Diehl gear is superb.
In both my excursions outside the norm I took the strut to a muffler shop
and had it bent back out ~15 degrees or so... good as new.

A safety plug (again) for those new to the plane.  My own first bent strut
came from an inadvertent takeoff during high speed taxi.  I pushed the nose
over (1/16 to 1/4 inch stick forward) and came crashing down on the nose.
The second came on a landing in very rough weather and one of my brake
pistons failed.  Not able to stop, I bled as much speed off as I could
before the end of the runway.  Nothing I could do about it, but the strut
held again, though I dug a good sized furrow with the nose tire in the soft
dirt.

Sorry for the long answer.  If you need more data, let me know and I can
e-mail you privately.

IHS,

David Goodman
Vertical Avionics, Inc.
www.verticalavionics.com


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KR> kr2 accident (long) with the facts

2010-10-12 Thread David Goodman
KrNetters,

Ted wrote:

Could you elaborate on the nose gear that collapsed?  Where did it fail?
Whose nose gear was it? Diehl?  He has two, a standard and a Corvair version
(don't know the difference). Do any recommendations come out of this
incident regarding the mounting of the nose gear?

Jim Morehead was the builder of this plane, so he final authority on the
nose gear.  It appeared to me to be a standard (VW) Diehl system.

As far as where it folded, you can take a look at link
http://sites.google.com/a/wildblue.net/goodmans/Home/2010-kr2-mishap.
There is a good photo from the side of just the nose gear located there.

We hit extremely hard on the nose on the first bounce.  I could not tell you
how hard the second hit was compared to the first, as my eyes were
completely uncaged for about one second after the first impact.  What I can
tell you is the gear did not shatter until after the second impact
nose-first of the plane onto the runway.  I know this because though my eyes
were uncaged I could still see the prop shatter on the second hit.

That the landing gear withstood the first impact is a testimony to the Diehl
gear's solid design.

Having nose-planted my own plane three years ago on a Corvair-weight gear
(which bent, but did not fail) and last year taking that same strut
off-roading at 35 KTS off a runway in California the Diehl gear is superb.
In both my excursions outside the norm I took the strut to a muffler shop
and had it bent back out ~15 degrees or so... good as new.

A safety plug (again) for those new to the plane.  My own first bent strut
came from an inadvertent takeoff during high speed taxi.  I pushed the nose
over (1/16 to 1/4 inch stick forward) and came crashing down on the nose.
The second came on a landing in very rough weather and one of my brake
pistons failed.  Not able to stop, I bled as much speed off as I could
before the end of the runway.  Nothing I could do about it, but the strut
held again, though I dug a good sized furrow with the nose tire in the soft
dirt.

Sorry for the long answer.  If you need more data, let me know and I can
e-mail you privately.

IHS,

David Goodman
Vertical Avionics, Inc.
www.verticalavionics.com



KR> kr2 accident (long) with the facts

2010-10-12 Thread Ted Sanders
David,

Could you elaborate on the nose gear that collapsed?  Where did it fail?
Whose nose gear was it? Diehl?  He has two, a standard and a Corvair version
(don't know the difference). Do any recommendations come out of this
incident regarding the mounting of the nose gear?  My questions are
innocent, I know that if you land on the mains and then settle on the nose
gear you will be fine.

Thanks

On Mon, Oct 11, 2010 at 9:43 AM, David Goodman <
dgood...@verticalavionics.com> wrote:

> Guys,
>
> I was in this airplane when it crashed.  If you want to know what happened
> you are NOT going to find it in the pixels of an NTSB or FAA report.  If
> fact relying on either an FAA or NTSB report for details on anything other
> than a commercial or high interest (national media coverage) mishap is a
> colossal mistake.
>
> Facts everyone needs to know about this mishap, mishap investigations, and
> the KR2 in general.
>
> - The current NTSB report is a PRELIMINARY REPORT.  It says so right in the
> first box.  Most of the information they used was given to them by me, from
> the back of an ambulance enroute to UC Davis Medical Center 30 minutes
> after
> the mishap.
>
> If you contact the NTSB about a mishap, they will go down a 40 question
> form
> with you.  It is amazing how many facts I gave them they either got wrong,
> or chose to word incorrectly.  We will have to wait and see what the final
> report says, but so far, more than half of the "facts" in the PRELIMINARY
> REPORT are simply incorrect.
>
> Understand something about the NTSB.  They took my phone call, got a
> statement from Jim (PIC), looked at the plane for less than 45 minutes, and
> wrote a preliminary report.  The NTSB does not "investigate" mishaps of
> this
> nature other than to assess if they need to investigate it.  Since there
> was
> no indication of failure of the aircraft (controls, engine, linkages) and
> no
> fatality (thankfully) they neither care nor desire to spend any more time
> on
> such mishaps.  No threat to the public, no media interest nationally, no
> further involvement or brain power expended by them.  They have other,
> better, ways of maximizing the consumption of your taxpayer dollars.
>
> As a military trained and experienced mishap investigator I can tell you
> the
> amount of time spent on a mishap scene is directly reflected in the
> accuracy
> of the report of findings.  Do not hang your hat, or your biases, on a
> "report" that has so little time invested in investigation.  Just analyzing
> what happened to the nose strut should have taken more time than the NTSB
> spent total, if one wants to actually know what happened.  A trained mishap
> investigator can tell you what angle the plane impacted in pitch and roll,
> what the vertical vector into the ground was (which will give the plane's
> airspeed), and a host of other information, just from the nose strut.  45
> minutes total at the scene?  Translating this statement to other KR
> mishaps:
> They may get parts of a given mishap correct and they may be enroute to
> Pluto or points beyond on others.  Do not define your opinions by these
> reports.
>
> - There was nothing twitchy or overly sensitive about Jim's plane.  It was
> a
> well balanced, solid-responding plane.  I had more hours in it than anyone
> else (12.1) and I had zero problem with the flight characteristics of this
> aircraft.  If there had been any issues with it handling qualities, my
> logbook would have reflected a .1 total time in flight, just enough time to
> circle to land and walk away.  The plane responded to the inputs it
> received.  Jim's craftsmanship was very evident in how this plane flew.
>
> The KR design is responsive, not sensitive.  This may seem like semantics,
> but there is a very big difference.  Most people are used to flying
> aircraft
> with the responsiveness of a 18-wheeler, i.e., a Cessna 150 or Piper 140.
> These planes are totally forgiving of pilot errors because they are trainer
> airplanes.  The KR pedigree does not behave this way.  Simply put, if you
> fly a KR with the same heavy handedness most pilots fly with, you are going
> for Mr. Toad's wild ride.
>
> I flew with two other pilots in Jim's KR, once each in the left and right
> seat.  One was an ATP, the other a commercial pilot.  Neither chose to fly
> in the plane again.  Both made some of the classic mistakes new pilots to
> the KR make, and it was "exciting" to be in the right seat with both of
> them.  The intent was they would finish the test phase of flying the plane,
> but they declined.  The ATP pilot actually told someone this was the only
> plane he had ever flown that scared him, an unfortunate observation, but
> not
> a knock against the KR.  His comfort level remains in 18-wheelers.
>
> Before anyone flies the KR for the first time alone it is my STRONG opinion
> they need to fly with someone else in a KR first.  I also submit one should
> spend some time talking to someone who knows a 

KR> kr2 accident (long) with the facts

2010-10-11 Thread rdrace...@aol.com
Gentlemen,

With an attempt not to keep beating on the horse I would like to highlight  
a couple of things David wrote in his email (which I did not copy in it's  
entirety here to save space...reread his email.)

Number one is that the NTSB did not publish a complete accident  
investigation which determined the exact cause of the crash, and since no one  
was 
killed, will probably not actually conduct a complete investigation to  
"Standard".  So you can speculate all you want about the cause based on  what 
the 
"Preliminary Report" implies, or based on what the media reported,  or 
you can base your speculations on David's "eyewitness" account.   Since David 
was not at the controls, even as an "eyewitness" he can  not be expected to 
have known exactly what the PIC was thinking or telling his  hands on the 
controls to do at the time.  Has anybody ever talked to police  investigators 
about how completely skewed eyewitness accounts can be.   Still, as an 
experienced pilot trained by the military as an instructor and  accident 
investigator, I trust David to have been paying pretty good  attention to what 
was 
actually transpiring at the time of the mishap. So I would  put a lot of 
weight on his Account being a fairly accurate depiction of the  event.

The Second thing I would like to highlight is David's comments about KR  
Handling characteristics and flying them in general.  I have flown a couple  
of KR2s.  I don't have the experience David, or a lot of you other guys  have 
with them by flying multiple versions, but I have yet to experience this  
instability or twitchiness that is constantly being referred to, but even 
with  close to 8000 hours of flight time I wouldn't consider jumping into any 
aircraft  (even a cessna 152) that I had never flown before and attempting to 
fly it  alone.  So just like I would do with any other unknown aircraft, I 
chose to  fly first with an experienced KR2 pilot before flying my own KR2.  
He  carefully prepared me for the worst, and explained what to expect and 
how to  recover from "pilot induced oscillations", then sat back and chuckled 
when he  gave me the controls.  I asked him a few minutes after taking the 
controls  when to expect the "wierdness" to happen and he had to take the 
controls back  and put in some major inputs to simulate and demonstrate for me 
what everyone  was talking about.  I still haven't figured out how to make 
the airplane do  that, but will take everyone's word for it that some folks 
are ham fisted.   The key point here being that "ham fisted" or not, why 
would anyone not get  checked out in an unknown airplane before soloing in it?

Sorry for being long winded.Just like all you builders  use the wisdom 
of the genius aeronautical engineering types (like Mark Langford,  etc.) to 
keep from having to learn building techniques the hard way, David  Goodman 
has graciously offered up his expertise as an instructor. Pick his brain  
about flying KR2s and if you can get to him, let him fly with you, before you  
have to learn flying techniques the hard way (like by having to practice 
your  building techniques again due to airframe damage.)

Todd Thelin
Spanaway, WA


In a message dated 10/11/2010 9:44:41 A.M. Pacific Daylight Time,  
dgood...@verticalavionics.com writes:

Guys,

I was in this airplane when it crashed.  If you want  to know what 
happened...


There are more photos and write-up of the  mishap aircraft  at:
http://sites.google.com/a/wildblue.net/goodmans/Home/2010-kr2-mishap

If  you have questions about flying a KR for the first time, call me as 
well.
I  will spend however much time you need or want to help you get ready  for
that first flight.

IHS,
David Goodman
Vertical Avionics,  Inc.
www.verticalavionics.com


___
Search  the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
to  UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
please see  other KRnet info at  http://www.krnet.org/info.html


KR> kr2 accident (long) with the facts

2010-10-11 Thread David Goodman
Guys,

I was in this airplane when it crashed.  If you want to know what happened
you are NOT going to find it in the pixels of an NTSB or FAA report.  If
fact relying on either an FAA or NTSB report for details on anything other
than a commercial or high interest (national media coverage) mishap is a
colossal mistake.

Facts everyone needs to know about this mishap, mishap investigations, and
the KR2 in general.

- The current NTSB report is a PRELIMINARY REPORT.  It says so right in the
first box.  Most of the information they used was given to them by me, from
the back of an ambulance enroute to UC Davis Medical Center 30 minutes after
the mishap.  

If you contact the NTSB about a mishap, they will go down a 40 question form
with you.  It is amazing how many facts I gave them they either got wrong,
or chose to word incorrectly.  We will have to wait and see what the final
report says, but so far, more than half of the "facts" in the PRELIMINARY
REPORT are simply incorrect.

Understand something about the NTSB.  They took my phone call, got a
statement from Jim (PIC), looked at the plane for less than 45 minutes, and
wrote a preliminary report.  The NTSB does not "investigate" mishaps of this
nature other than to assess if they need to investigate it.  Since there was
no indication of failure of the aircraft (controls, engine, linkages) and no
fatality (thankfully) they neither care nor desire to spend any more time on
such mishaps.  No threat to the public, no media interest nationally, no
further involvement or brain power expended by them.  They have other,
better, ways of maximizing the consumption of your taxpayer dollars.

As a military trained and experienced mishap investigator I can tell you the
amount of time spent on a mishap scene is directly reflected in the accuracy
of the report of findings.  Do not hang your hat, or your biases, on a
"report" that has so little time invested in investigation.  Just analyzing
what happened to the nose strut should have taken more time than the NTSB
spent total, if one wants to actually know what happened.  A trained mishap
investigator can tell you what angle the plane impacted in pitch and roll,
what the vertical vector into the ground was (which will give the plane's
airspeed), and a host of other information, just from the nose strut.  45
minutes total at the scene?  Translating this statement to other KR mishaps:
They may get parts of a given mishap correct and they may be enroute to
Pluto or points beyond on others.  Do not define your opinions by these
reports.

- There was nothing twitchy or overly sensitive about Jim's plane.  It was a
well balanced, solid-responding plane.  I had more hours in it than anyone
else (12.1) and I had zero problem with the flight characteristics of this
aircraft.  If there had been any issues with it handling qualities, my
logbook would have reflected a .1 total time in flight, just enough time to
circle to land and walk away.  The plane responded to the inputs it
received.  Jim's craftsmanship was very evident in how this plane flew.

The KR design is responsive, not sensitive.  This may seem like semantics,
but there is a very big difference.  Most people are used to flying aircraft
with the responsiveness of a 18-wheeler, i.e., a Cessna 150 or Piper 140.
These planes are totally forgiving of pilot errors because they are trainer
airplanes.  The KR pedigree does not behave this way.  Simply put, if you
fly a KR with the same heavy handedness most pilots fly with, you are going
for Mr. Toad's wild ride.

I flew with two other pilots in Jim's KR, once each in the left and right
seat.  One was an ATP, the other a commercial pilot.  Neither chose to fly
in the plane again.  Both made some of the classic mistakes new pilots to
the KR make, and it was "exciting" to be in the right seat with both of
them.  The intent was they would finish the test phase of flying the plane,
but they declined.  The ATP pilot actually told someone this was the only
plane he had ever flown that scared him, an unfortunate observation, but not
a knock against the KR.  His comfort level remains in 18-wheelers.

Before anyone flies the KR for the first time alone it is my STRONG opinion
they need to fly with someone else in a KR first.  I also submit one should
spend some time talking to someone who knows a good deal about how the KR
handles relative to other aircraft.  THIS DOES NOT INCLUDE people who have
most or all of their time in the KR, as they will miss a great deal of the
difference that needs to be explained to a new KR pilot.  This is not a cut
down, it is simply their familiarity and comfort with the KR platform may
cause them to skip key factors a new KR person needs to know about.  If you
spent a few years building something you are proud enough to go airborne in,
take the extra bit of time to get ready to fly it the right way, by/with
someone who can help you.  If you cannot find anyone else to talk to, give
Bill Clapp or I a 

KR> kr2 accident

2010-10-11 Thread Patrick and Robin Russo
What if it were true that the pilot had 50 years of flying experience and 
several hundred hours in the very same plane. Would you still suggest pitch 
sensitivity?? There are many other possible causes for this accident and 
many of us older (over seventy ) pilots would concludeoops, that was 
sloppy of me!!  Seldom would we blame the plane, unless of course we were 
lawyers!  I wonder how often we have mishaps and they never get reported. I 
know of many as well as my own. Just pick up the broken parts and bring it 
back home, I suppose tho, if the broken part were me, it would soon enough 
get reported.
- Original Message - 
From: "Craig Williams" <kr2seaf...@yahoo.com>
To: <kr...@mylist.net>
Sent: Monday, October 11, 2010 5:01 AM
Subject: KR> kr2 accident


> according to the article it looks like pitch sensitivity was possibly the
> problem
>
> http://cbs13.com/local/injury.plane.crash.2.1893161.html
>
>
>
>
> ___
> Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html
> 



KR> kr2 accident

2010-10-11 Thread Virgil N. Salisbury
  How about OVER CONTROLLING on the part of the pilot? Virg


 On 10/11/2010 5:01 AM, Craig Williams wrote:
> according to the article it looks like pitch sensitivity was possibly the
> problem
>
> http://cbs13.com/local/injury.plane.crash.2.1893161.html
>
>
>
>
> ___
> Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html
>



KR> kr2 accident

2010-10-11 Thread Craig Williams
My bad for believing the FAA guy in the article reporting that the aircraft 
bounced several times.  I looked up the preliminary NTSB report and it does not 
mention any bouncing.

--- On Mon, 10/11/10, Dan Heath <da...@windstream.net> wrote:

From: Dan Heath <da...@windstream.net>
Subject: RE: KR> kr2 accident
To: "'KRnet'" <kr...@mylist.net>
List-Post: krnet@list.krnet.org
Date: Monday, October 11, 2010, 9:33 AM

Old news.  A very good write-up was done on this by the passenger.  Pitch
sensitivity is not the issue here.

See N64KR at http://KRBuilder.org - Then click on the pics 
See you at the 2011 - KR Gathering in Mt. Vernon, Il - MVN
There is a time for building and it never seems to end.
Daniel R. Heath - Lexington, SC

-Original Message-
according to the article it looks like pitch sensitivity was possibly the 
problem


___
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KR> kr2 accident

2010-10-11 Thread Dan Heath
Old news.  A very good write-up was done on this by the passenger.  Pitch
sensitivity is not the issue here.

See N64KR at http://KRBuilder.org - Then click on the pics 
See you at the 2011 - KR Gathering in Mt. Vernon, Il - MVN
There is a time for building and it never seems to end.
Daniel R. Heath - Lexington, SC

-Original Message-
according to the article it looks like pitch sensitivity was possibly the 
problem



KR> kr2 accident

2010-10-11 Thread Craig Williams
according to the article it looks like pitch sensitivity was possibly the 
problem

http://cbs13.com/local/injury.plane.crash.2.1893161.html