Re: [Aus-soaring] Spin training

2014-12-27 Thread Ulrich Stauss
Is this what you had in mind Anthony?
http://www.dg-flugzeugbau.de/index.php?id=seitenfaden-e

Ulrich
-Original Message-
From: aus-soaring-boun...@lists.internode.on.net 
[mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Anthony Smith
Sent: Saturday, 27 December 2014 16:49
To: 'Discussion of issues relating to Soaring in Australia.'
Subject: Re: [Aus-soaring] Spin training

You probably could do something very easily for modern non-flapped gliders.  
AoA indicators have been around for a long time.  You could have three critical 
angles annotated on the device display: stall, climb and cruise.  Flapped 
gliders would need to have a method of knowing what the flap deflection is 
which would change these angles a bit depending on the deflection.  The problem 
would be whether pilots would want an extra device protruding into the laminar 
flow on the forward fuselage or not.

I may have mentioned the following previously:

As an aside, the static system on the P-3 Orion is excellent for detecting 
stall - just not in the expected way.  The original static system was on the 
forward fuselage.  However , it was found to have disturbed airflow when the 
bomb bay doors were open.  An alternate static location was found on the aft 
fuselage.  Arguably it was a better site as the error correction for the static 
system was significantly smaller and it was not affected by the bomb bay doors 
being open.  However, the new static ports were in the wake from the upper 
surface of the wing.  As soon as the wing root airflow on the wing upper 
surface starts to separate, the static system becomes subject to large pressure 
disturbances and the ASI and the altimeter become unresponsive and both of the 
needles start to bounce around.  So if you experience buffet in a P-3 and the 
ASI and altimeter needles are bouncing around, it is a stall. 

During discussions a few years ago about P-3 stall warning, I suggested that it 
may be feasible to directly tap into the static system and detect the pressure 
fluctuations from the flow separation and hence provide a stall warning.  The 
proposal was rejected as it needed a lot of R  D thrown at it to develop the 
idea.

Something like this may be the 'better mouse trap' for gliders.  A pressure 
transducer system connected to the upper surface trailing edge of the wing at a 
suitable point on each side  that trips a warning if separated flow is 
detected.  This would be a direct measurement of impending stall rather than 
implied through AoA or computing speed, g and wing loading etc.

Anthony

-Original Message-
From: aus-soaring-boun...@lists.internode.on.net 
[mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Michael Derry
Sent: Saturday, 27 December 2014 10:29 AM
To: Discussion of issues relating to Soaring in Australia.
Subject: Re: [Aus-soaring] Spin training

The report reminds us how useless the ASI is during spins. You are better off 
judging speed using the noise levels assessed by your ears.

Why hasn't some instrument maker built a better mousetrap than the one we have ?

On Sat, 27 Dec 2014 08:56:09 +1030
Ulrich Stauss usta...@internode.on.net wrote:

 This is a multipart message in MIME format.
 
 
 http://faculty.chicagobooth.edu/john.cochrane/research/Data_and_Progra
 ms/CFI/AFFTC-TR-89-27%20Spin%20Test.pdf
 
  
 
 Ulrich
 
  
 
 From: aus-soaring-boun...@lists.internode.on.net 
 [mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Ron 
 Sanders
 Sent: Saturday, 27 December 2014 08:44
 To: Discussion of issues relating to Soaring in Australia.
 Subject: Re: [Aus-soaring] Spin training
 
  
 
 Bernard,  good morning, i would lke o read that report too please?
 
  
 
 Ron
 
  
 
 On 27 December 2014 at 08:18, Bernhard ec...@internode.on.net wrote:
 
 Hello Paul, good morning all
 
  
 
 You might be interested to know that the US Air Force has already been 
 using the ASK21 for spin training over several
 
 decades.
 
  
 
 Therefore you might want to refer to a report by the US Air Force on 
 the spin characteristics of the ASK 21. It was done
 
by experts in the field and true professionals. When you read the 
 report you will find that it was perhaps the most
 
comprehensive study into the subject ever done. 
 
  
 
 To save you digging around I have attached a copy for you!
 
  
 
 Kind regards to all
 
  
 
 Bernard
 
  
 
 
 
 
 
 On 26 Dec 2014, at 10:05 pm, Paul Bart pb2...@gmail.com 
 mailto:pb2...@gmail.com  wrote:
 
  
 
  
 
 On 26 December 2014 at 19:33, Daryl Mackay darylmac...@gmail.com 
 mailto:darylmac...@gmail.com  wrote:
 
  
 
  
 
 Suffice to say no instructor willingly uses the ASK21 for spin awareness 
 training at Beverley.
 
  
 
 ​Hi Daryl
 
  
 
 Would you mind explaining why? This is a genuine inquiry as my club is 
 about to take a delivery of one.​
 
  
 
  
 
 ​Cheers
 
  
 
 Paulâ

Re: [Aus-soaring] Spin training

2014-12-27 Thread Anthony Smith
Actually, yes.  I must try that out sometime!


-Original Message-
From: aus-soaring-boun...@lists.internode.on.net 
[mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Ulrich Stauss
Sent: Saturday, 27 December 2014 8:07 PM
To: 'Discussion of issues relating to Soaring in Australia.'
Subject: Re: [Aus-soaring] Spin training

Is this what you had in mind Anthony?
http://www.dg-flugzeugbau.de/index.php?id=seitenfaden-e

Ulrich
-Original Message-
From: aus-soaring-boun...@lists.internode.on.net 
[mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Anthony Smith
Sent: Saturday, 27 December 2014 16:49
To: 'Discussion of issues relating to Soaring in Australia.'
Subject: Re: [Aus-soaring] Spin training

You probably could do something very easily for modern non-flapped gliders.  
AoA indicators have been around for a long time.  You could have three critical 
angles annotated on the device display: stall, climb and cruise.  Flapped 
gliders would need to have a method of knowing what the flap deflection is 
which would change these angles a bit depending on the deflection.  The problem 
would be whether pilots would want an extra device protruding into the laminar 
flow on the forward fuselage or not.

I may have mentioned the following previously:

As an aside, the static system on the P-3 Orion is excellent for detecting 
stall - just not in the expected way.  The original static system was on the 
forward fuselage.  However , it was found to have disturbed airflow when the 
bomb bay doors were open.  An alternate static location was found on the aft 
fuselage.  Arguably it was a better site as the error correction for the static 
system was significantly smaller and it was not affected by the bomb bay doors 
being open.  However, the new static ports were in the wake from the upper 
surface of the wing.  As soon as the wing root airflow on the wing upper 
surface starts to separate, the static system becomes subject to large pressure 
disturbances and the ASI and the altimeter become unresponsive and both of the 
needles start to bounce around.  So if you experience buffet in a P-3 and the 
ASI and altimeter needles are bouncing around, it is a stall. 

During discussions a few years ago about P-3 stall warning, I suggested that it 
may be feasible to directly tap into the static system and detect the pressure 
fluctuations from the flow separation and hence provide a stall warning.  The 
proposal was rejected as it needed a lot of R  D thrown at it to develop the 
idea.

Something like this may be the 'better mouse trap' for gliders.  A pressure 
transducer system connected to the upper surface trailing edge of the wing at a 
suitable point on each side  that trips a warning if separated flow is 
detected.  This would be a direct measurement of impending stall rather than 
implied through AoA or computing speed, g and wing loading etc.

Anthony

-Original Message-
From: aus-soaring-boun...@lists.internode.on.net 
[mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Michael Derry
Sent: Saturday, 27 December 2014 10:29 AM
To: Discussion of issues relating to Soaring in Australia.
Subject: Re: [Aus-soaring] Spin training

The report reminds us how useless the ASI is during spins. You are better off 
judging speed using the noise levels assessed by your ears.

Why hasn't some instrument maker built a better mousetrap than the one we have ?

On Sat, 27 Dec 2014 08:56:09 +1030
Ulrich Stauss usta...@internode.on.net wrote:

 This is a multipart message in MIME format.
 
 
 http://faculty.chicagobooth.edu/john.cochrane/research/Data_and_Progra
 ms/CFI/AFFTC-TR-89-27%20Spin%20Test.pdf
 
  
 
 Ulrich
 
  
 
 From: aus-soaring-boun...@lists.internode.on.net
 [mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Ron 
 Sanders
 Sent: Saturday, 27 December 2014 08:44
 To: Discussion of issues relating to Soaring in Australia.
 Subject: Re: [Aus-soaring] Spin training
 
  
 
 Bernard,  good morning, i would lke o read that report too please?
 
  
 
 Ron
 
  
 
 On 27 December 2014 at 08:18, Bernhard ec...@internode.on.net wrote:
 
 Hello Paul, good morning all
 
  
 
 You might be interested to know that the US Air Force has already been 
 using the ASK21 for spin training over several
 
 decades.
 
  
 
 Therefore you might want to refer to a report by the US Air Force on 
 the spin characteristics of the ASK 21. It was done
 
by experts in the field and true professionals. When you read the 
 report you will find that it was perhaps the most
 
comprehensive study into the subject ever done. 
 
  
 
 To save you digging around I have attached a copy for you!
 
  
 
 Kind regards to all
 
  
 
 Bernard
 
  
 
 
 
 
 
 On 26 Dec 2014, at 10:05 pm, Paul Bart pb2...@gmail.com 
 mailto:pb2...@gmail.com  wrote:
 
  
 
  
 
 On 26 December 2014 at 19:33, Daryl Mackay darylmac

Re: [Aus-soaring] Spin training

2014-12-27 Thread Anthony Smith
Actually, I was thinking a flush mounted static probe rather than a pitot.
It would be interesting to see if a transducer could pick up the pressure
fluctuations from separated flow and be able to see the difference from
attached flow.

After doing some work with the RAAF's P-3 wing tips, I am pretty sure it is
feasible.



-Original Message-

I saw a photo from 30 years ago of your upper wing surface near the trailing
edge pitot probe, Anthony. Pressure should be equal to pitot until the
thickening separated boundary layer encompasses the wing probe when the
pressure difference should increase rapidly. Might be useful on some gliders
which are very well behaved at low speeds and thermal nicely but don't climb
well unless flown a fair bit faster. 

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[Aus-soaring] Spin training

2014-12-26 Thread Daryl Mackay
 Sorry for this long response but I am passionate about this issue and some
clarifications are necessary.

It is only true that most spins can be prevented if 1.5Vs is maintained. A
mishandled entry of more than 1 G steady is possible at much higher
speeds. (E.g. Mishandling and Snap rolls)

Many things lead up to the inadvertent spin accident. Having reached
autorotation, only a successful spin recovery can save the final accident
chain outcome.

We must mitigate against this identified risk. Obviously, safe speed near
the ground training is not working all the time and only gives the training
department a false sense of security in their job of preparing a safe
pilot. We all perform this monkey do action for the instructor and yet we
still have spin accidents. The fact is that all pilots can make mistakes
when loaded up in a circuit and our best laid plan is falling apart. This
stress can and has resulted in slower than intended speeds. The majority of
spin accident result from too slow/high angle of attack flight.

When everything else has failed, it is the ability to recover from;

1. Slow flight

2. Stall,

3. Incipient spin, and finaly

4. Spin

that may save the day. I certainly wouldn’t give up on a full spin recovery
well below 1000ft AGL! An incipient spin recovery on final should still
result in a controlled landing. And every one of us has recognised
inadvertent slow flight on short final and done something about it to avoid
the heavy landing. Instructors see this one every day.

We need more low speed, high angle of attack flying training; not less. A
yearly check in a training ACFT by an instructor under pressure to accept
the minimum requirement, with the average pilot, no longer current and now
in another type, 12 months later, who has inadvertently allowed his IAS to
decrease below some nominated speed is an accident chain. If progressed to
this stage, then the final outcome will only be saved by knowing how to
identify high angle of attack flight and a speedy recovery.

With regard to the “slippery” training ACFT not providing realistic anti
spin training.

It is the instructor who makes the over-riding difference but even then,
one should not blame the tools he has to work with. I also note the high
drag/low drag and the money savings/pilot satisfaction arguments. I address
the high drag verses low drag argument as it applies to the ACFT I'm
familair with, having read their Flight Manuals. I use the techniques
personally taught me and described in AG by Mike Valentine and the GFA
Instructors Manual and I do have aerobatic endorsements. I mention this
because I want to stress that the aerodynamic/gyroscopic/CofG
characteristics of the preferred types mentioned are consistant when using
Mike's technique.

I know that the DG1000 can be recovered with the same or less height loss
as the Puchacz and both of these take a little more than the older L13 and
the L23. This is directly related to the type of *autorotation*
entry/recovery characteristics of the types, not the pull out from the
ensuring dive. The Blaniks take just a little over 90 degrees of turn to
recover from the autorotation. I have also extensively checked the spin
entry and recovery characteristics of the ASK21 with its required spin kit
fitted. Suffice to say no instructor willingly uses the ASK21 for spin
awareness training at Beverley. Other clubs may have no other choice.

The full spin recovery is designed to minimise the height loss once a spin
has been allowed to develop. A major part of height conservation is gained
by correctly identifying when the ACFT has recovered from the autorotation
phase and we can therefore re-apply back stick but importantly play “G”
against airspeed. Amazingly, in the majority of cases on all types, this is
the area where most will lose excessive height; just when the ACFT is under
their complete control! The problem is one of identification and this can
only be improved by determined training and greater currency; not less. It
is not ACFT specific and it is a cop out to propose one ACFT is worse than
another. The instructor needs to become current with all his ACFT and teach
minimum height loss with that particular tool. After all, it is a club ACFT
and will be flown be a wide cross section of club members, all of whom form
an accident chain sooner or later.

The DG1000 autorotation recovery is both predictable and quick at all pilot
weight combinations because of the ingenious and quick tail ballasting
facility allowing a generous CofG range for spin training, even with the
GFA 5% reduction over the Flight Manual range. The following pull-out
phase, due to the initial lower zero “G” drag and subsequent increasing “G”
lower drag during pull out provides a higher acceleration meaning less time
to achieve safe flying recovery speed and therefore less height loss in
this fully aerobatic ACFT. One should be achieving a recovery speed maximum
of 65-70IAS on this type or redoing the exercise 

Re: [Aus-soaring] Spin training

2014-12-26 Thread Daryl Mackay
Hi Paul,
Detailed response sent to your personal email address just now.
Kind regards,
Daryl
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Re: [Aus-soaring] Spin training

2014-12-26 Thread Bernhard
 Hello Paul, good morning all
 
 You might be interested to know that the US Air Force has already been using 
 the ASK21 for spin training over several 
 decades.
 
 Therefore you might want to refer to a report by the US Air Force on the spin 
 characteristics of the ASK 21. It was done
   by experts in the field and true professionals. When you read the report you 
will find that it was perhaps the most 
   comprehensive study into the subject ever done. 
 
 
 To save you digging around I have attached a copy for you!
 
 Kind regards to all
 
 Bernard 
 

 On 26 Dec 2014, at 10:05 pm, Paul Bart pb2...@gmail.com wrote:
 
 
 On 26 December 2014 at 19:33, Daryl Mackay darylmac...@gmail.com 
 mailto:darylmac...@gmail.com wrote:
 
 
 Suffice to say no instructor willingly uses the ASK21 for spin awareness 
 training at Beverley.
 
 ​Hi Daryl
 
 Would you mind explaining why? This is a genuine inquiry as my club is about 
 to take a delivery of one.​ 
 
 ​Cheers
 
 Paul​
 
 
 
 
 Cheers
 
 Paul
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Re: [Aus-soaring] Spin training

2014-12-26 Thread Ron Sanders
Bernard,  good morning, i would lke o read that report too please?

Ron

On 27 December 2014 at 08:18, Bernhard ec...@internode.on.net wrote:

 Hello Paul, good morning all

 You might be interested to know that the US Air Force has already been
 using the ASK21 for spin training over several
 decades.

 Therefore you might want to refer to a report by the US Air Force on the
 spin characteristics of the ASK 21. It was done

by experts in the field and true professionals. When you read the
 report you will find that it was perhaps the most
comprehensive study into the subject ever done.


 To save you digging around I have attached a copy for you!

 Kind regards to all

 Bernard


 On 26 Dec 2014, at 10:05 pm, Paul Bart pb2...@gmail.com wrote:


 On 26 December 2014 at 19:33, Daryl Mackay darylmac...@gmail.com wrote:


 Suffice to say no instructor willingly uses the ASK21 for spin awareness
 training at Beverley.


 ​Hi Daryl

 Would you mind explaining why? This is a genuine inquiry as my club is
 about to take a delivery of one.​


 ​Cheers

 Paul​




 Cheers

 Paul
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Re: [Aus-soaring] Spin training

2014-12-26 Thread Ulrich Stauss
http://faculty.chicagobooth.edu/john.cochrane/research/Data_and_Programs/CFI/AFFTC-TR-89-27%20Spin%20Test.pdf

 

Ulrich

 

From: aus-soaring-boun...@lists.internode.on.net 
[mailto:aus-soaring-boun...@lists.internode.on.net] On Behalf Of Ron Sanders
Sent: Saturday, 27 December 2014 08:44
To: Discussion of issues relating to Soaring in Australia.
Subject: Re: [Aus-soaring] Spin training

 

Bernard,  good morning, i would lke o read that report too please?

 

Ron

 

On 27 December 2014 at 08:18, Bernhard ec...@internode.on.net wrote:

Hello Paul, good morning all

 

You might be interested to know that the US Air Force has already been using 
the ASK21 for spin training over several 

decades.

 

Therefore you might want to refer to a report by the US Air Force on the spin 
characteristics of the ASK 21. It was done 

   by experts in the field and true professionals. When you read the report you 
will find that it was perhaps the most 

   comprehensive study into the subject ever done. 

 

To save you digging around I have attached a copy for you!

 

Kind regards to all

 

Bernard 

 





On 26 Dec 2014, at 10:05 pm, Paul Bart pb2...@gmail.com 
mailto:pb2...@gmail.com  wrote:

 

 

On 26 December 2014 at 19:33, Daryl Mackay darylmac...@gmail.com 
mailto:darylmac...@gmail.com  wrote:

 

 

Suffice to say no instructor willingly uses the ASK21 for spin awareness 
training at Beverley.

 

​Hi Daryl

 

Would you mind explaining why? This is a genuine inquiry as my club is about to 
take a delivery of one.​

 

 

​Cheers

 

Paul​

 






Cheers

Paul

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Re: [Aus-soaring] Spin training

2014-12-26 Thread Mike Borgelt
 the idea. 
Something like this may be the 'better mouse 
trap' for gliders.  A pressure transducer system 
connected to the upper surface trailing edge of 
the wing at a suitable point on each side  that 
trips a warning if separated flow is 
detected.  This would be a direct measurement of 
impending stall rather than implied through AoA 
or computing speed, g and wing loading etc. 
Anthony -Original Message- From: 
aus-soaring-boun...@lists.internode.on.net 
[mailto:aus-soaring-boun...@lists.internode.on.net] 
On Behalf Of Michael Derry Sent: Saturday, 27 
December 2014 10:29 AM To: Discussion of issues 
relating to Soaring in Australia. Subject: Re: 
[Aus-soaring] Spin training The report reminds 
us how useless the ASI is during spins. You are 
better off judging speed using the noise levels 
assessed by your ears. Why hasn't some 
instrument maker built a better mousetrap than 
the one we have ? On Sat, 27 Dec 2014 08:56:09 
+1030 Ulrich Stauss usta...@internode.on.net 
wrote:  This is a multipart message in MIME 
format.   
  
 
http://faculty.chicagobooth.edu/john.cochrane/research/Data_and_Progra  
 
ms/CFI/AFFTC-TR-89-27%20Spin%20Test.pdf  
Ulrich  From: 
aus-soaring-boun...@lists.internode.on.net  
[mailto:aus-soaring-boun...@lists.internode.on.net] 
On Behalf Of Ron  Sanders  Sent: Saturday, 27 
December 2014 08:44  To: Discussion of issues 
relating to Soaring in Australia.  Subject: Re: 
[Aus-soaring] Spin training  
Bernard,  good morning, i would lke o read that 
report too please?  Ron  On 27 
December 2014 at 08:18, Bernhard 
ec...@internode.on.net wrote:   Hello Paul, 
good morning all  You might be 
interested to know that the US Air Force has 
already been  using the ASK21 for spin training 
over several   decades.  Therefore you 
might want to refer to a report by the US Air 
Force on  the spin characteristics of the ASK 
21. It was done  by experts in the field 
and true professionals. When you read the  
report you will find that it was perhaps the 
most  comprehensive study into the subject 
ever done.  To save you digging around I 
have attached a copy for you!  Kind 
regards to all  Bernard  
On 26 Dec 2014, at 10:05 pm, Paul Bart 
pb2...@gmail.com mailto:pb2...@gmail.com  
wrote: On 26 December 2014 at 
19:33, Daryl Mackay darylmac...@gmail.com 
mailto:darylmac...@gmail.com  
wrote: Suffice to say no 
instructor willingly uses the ASK21 for spin 
awareness training at Beverley.  
â€â€¹Hi Daryl  Would you mind 
explaining why? This is a genuine inquiry as my 
club is  about to take a delivery of 
one.​ â€â€¹Cheers  
Paul⢀‹   Cheers   
Paul   
  
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[Aus-soaring] spin training

2014-12-25 Thread Harry

Hi All,

I wrote the attached article and it received a few comments, both on and off 
the web.
I should have summarised as follows.

1. If you enter a spin a modern glider below 1,000 ft. AGL you will almost 
certainly die. No amount of prior training will make much difference.
2.Your first defence is to maintain safe speed near the ground. Your early 
training should be such that you feel very uncomfortable if below this criteria.
3. To maintain this speed you must monitor the ASI. Ground features mean 
relying on the horizon attitude is not accurate, particularly with modern 
slippery gliders. The ASI should be checked regularly and the closer to the 
ground and more adverse the conditions the more frequently the check. On final 
under turbulent conditions a quick check no more than every 5 seconds is needed 
to ensure safe speed is maintained.
4. Learning and practicing incipient recovery. If things go wrong incipient 
recovery means living to a ripe old age more certain, whether in a thermal or 
close to the ground.   
5. Spin training helps in spins at altitude. Enter a spin below about 1,000 ft 
AGL in a modern glider and you will most likely be dead in about 5 seconds. 

Harry Medlicott
Hi All,

Sorry to be controversial but I believe most of our spin training is marginal 
in saving lives in the real world. Of far greater significance are design 
factors reducing the propensity of gliders to spin. Spin related accidents in 
Europe have substantially reduced over time. No changes in spin training but 
modern gliders are far more forgiving.

My first club had winch launching only and every year a tug was brought in and 
towed gliders to 3,000 ft for spin training. After briefing, students were 
quite comfortable going through the standard recovery procedures.

My second club was winch launching only. Often there were periods when we had 
students due for spin training but weather conditions were such that thermals 
were not able to give us much by way of height. I experimented with a Blanik by 
a spin of the top of a winch launch which after one turn allowed recovery by 
1,000 ft. before using the procedure with a student. OK in a Blanik but 
certainly not in some other types

Despite very careful briefing a few minutes before the results were entirely 
different to those when entering a spin at 3,000 ft. Upon seeing the ground 
below them the student would immediately pull the control column right back and 
sometimes also move the control column away from the descending wing. It was an 
involuntary reaction but the one we would use to keep the glider in a spin.

So far as I am aware most spin accidents occur close to the ground, below about 
1,000 ft unless one is flying a particularly nasty glider such as an IS28, 
which can take over 1,000 ft for the whole process. If what I am saying is 
correct, then what are the chances of a pilot using the correct recovery 
processes in a low level spin, perhaps a considerable time after undergoing 
spin training or refreshing? Not very high. When asked to give a nervous pilot 
spin training I would say “We are going to undertake spin avoidance training” 
whereupon they would relax. After release at say 3,000 ft I would establish 
safe speed near the ground and invite them to mishandle the glider with  rudder 
and aileron and try and induce a spin. The message was that if you establish 
and maintain safe speed near the ground, a spin is improbable. After that, of 
course, we undertook standard spin training.

Instructors right from a students very first flight should emphasise that they 
have established and maintained safe speed near the ground when they are at a 
height at which they would not like to attempt a spin recovery. Just as 
importantly, that their lookout procedures are excellent. My message to a 
student or visitor in an introductory flight was that I could not see where we 
going from the back seat and that their good lookout  was needed to keep us 
safe,

Harry Medlicott








From: Peter (PCS3) 
Sent: Wednesday, December 24, 2014 10:48 PM
To: aus-soaring@lists.internode.on.net 
Subject: [Aus-soaring] Spinning Re: IS-28B CQC's last flying day:


On 24/12/2014 8:41 PM, Colin Collum wrote:

  G’day All,



  One of the ironies of gliding seems to be that modern sleek gliders are not 
only faster in virtually every sense, they are also safer in that many of them 
are much less likely to spin, but unfortunately our novice pilot can’t be 
guaranteed to always fly an aircraft that won’t spin.

I was instructing a girl in the front seat of a Twin Astir and said to her: 
Twin Astirs just mush instead of spinning  To my surprise, she managed to 
spin it easily (because of her light weight) and it required full opposite 
rudder to stop it as well as easing the stick forward and a very steep dive 
enough for a loop.

I was in a Ventus 2b on a Xcountry having lunch in a thermal.  I reached behind 
me to grab the water tube; the bottle was strapped on 

[Aus-soaring] Spin Training

2014-12-25 Thread Michael Derry
 in the front seat of a Twin Astir and said to her: 
Twin Astirs just mush instead of spinning  To my surprise, she managed to 
spin it easily (because of her light weight) and it required full opposite 
rudder to stop it as well as easing the stick forward and a very steep dive 
enough for a loop.

I was in a Ventus 2b on a Xcountry having lunch in a thermal.  I reached behind 
me to grab the water tube; the bottle was strapped on parcel shelf above and 
behind me and the tube had slipped down beside me out of reach and I was going 
to find it from the bottle. When I looked round, the paddocks were in my direct 
field of vision rotating.  I absolutely had no idea I was in a spin. Full 
opposite rudder took a lng time to stop the rotation and the height lost 
was significant but fortunately did not end in an outlanding.

I recite this to all my students when instructing on spins.

PeterS



  So we need to teach them in aircraft that can be spun safely, but we also 
need to keep them keen and I must say that when I was learning 10 years ago, 
even then the IS28s gave the impression of being way too out-of-date in their 
performance and appearance. After going solo I graduated to the giddy heights 
of a Junior—the novelty wore off that pretty quickly when from 8,500’ AGL I 
couldn’t make it 40km home at best LD into a light breeze without another 
thermal!

   

  It’s no use saying I learned in one of those, and if it was good enough for 
me then it is good enough for the current generation of learners. We need to 
keep them interested, a little excited, able to progress quickly enough for it 
to be satisfying and also very safe.

   

  I don’t claim to know the answers, but I doubt if it is IS28s, K13s, K6s and 
Juniors. K21s? Probably, but I don’t know what to recommend for a first 
single-seater.

   

  Merry Xmas,

   

  Colin








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Re: [Aus-soaring] IS-28B CQC's last flying ... Grant Davies
Re: [Aus-soaring] IS-28B CQC's last flying ... Christopher McDonnell
Re: [Aus-soaring] IS-28B CQC's last flying ... Derek Ruddock
Re: [Aus-soaring] IS-28B CQC's last flying ... Mark Newton
Re: [Aus-soaring] IS-28B CQC's last flying ... Darin McLean
Re: [Aus-soaring] IS-28B CQC's last flying ... Leigh Bunting
Re: [Aus-soaring] IS-28B CQC's last flying ... Colin Collum
[Aus-soaring] Spinning Re: IS-28B CQC's la... Peter (PCS3)
Re: [Aus-soaring] Spinning Re: IS-28B CQC'... Harry
Re: [Aus-soaring] Spinning Re: IS-28B CQC's... Daryl Mackay
[Aus-soaring] spin training Harry
Re: [Aus-soaring] IS-28B CQC's last flying ... Grant Davies
Re: [Aus-soaring] IS-28B CQC's last flying ... Leigh Bunting
Re: [Aus-soaring] IS-28B CQC's last flying ... Mark Newton
Re: [Aus-soaring] IS-28B CQC's last flying ... James Dutschke
Re: [Aus-soaring] IS-28B CQC's last flying ... Leigh Bunting
[Aus-soaring] German Soaring Picture Calendars ... Mike Cleaver
Re: [Aus-soaring] IS-28B CQC's last flying day: Mike Cleaver



   


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Re: [Aus-soaring] Spin Training

2014-12-25 Thread Michael Derry
Hi Harry

The dual car system is working well, plenty of power, tension control,
no cable breaks, no drum tangles and quick turnaround.

How is your winch going ?

Compared to Australia, the BGA have done a lot of winch launching so it
makes sense to look carefully at what they had done.

I have read much of the material published on the BGA website about safe
winch launching and much of it seems applicable to our operations, however
I welcome input from others in Australia experienced at winch launching.

The GFA sets a minumum, however as I understand it  there is nothing to
stop individual Clubs that are concerned about safety to up the minimum
winch launch speed to a higher figure such as 1.5 Vs.

We do a lot of aerotowing in Australia so we should do a safe aerotowing
initiative for the Brits to follow although they have already beaten us
to it. !

Cheers

Michael

On Fri, 26 Dec 2014 15:04:44 +1100
Harry  hw.medlic...@optusnet.com.au wrote:

 Hi Michael,
 
 Not sure of your winch status. The Brits after an extensive investigation 
 introduced “Safe Winch Launch”. Its principles reduced the winching 
 accident 
 rate to 25% of what it was and has virtually eliminated fatalities.  Worth 
 checking out their web site if interested. It uses 1.5 VS as the winch 
 launch minimum. They have no record of an airworthy  glider being damaged by 
 overspeeding but many accidents and fatalities by being too slow. I tried to 
 get the GFA to adopt the principles in Safe Winch Launch. Initially they 
 accepted 1.5 VS as the minimum but reduced it to 1.3 VS after some clubs 
 complained that  1.5 VS  left too small a margin between it and the max. 
 winch launch speed allowed for some older gliders.
 
 I could go on with other instances.
 
 Harry
 
 -Original Message- 
 From: Michael Derry
 Sent: Friday, December 26, 2014 11:32 AM
 To: aus-soaring@lists.internode.on.net
 Subject: [Aus-soaring] Spin Training
 
 Hi All
 
 Why is there such a paranoa about maintaining safe airspeed (which is
 accepted to be 1.5 times Vs plus 1/2 windspeed) near the ground for
 general flying if below 1,000 feet however:
 winch launching pilots only have to maintain  1.3 Vs while they have a
 gigantic airbrake deployed (ie their wing at 30 degrees or more).
 
 Doesn't make a lot of sense.
 
 Michael Derry
 __
 Hi All,
 
 I wrote the attached article and it received a few comments, both on and off
 the web.
 I should have summarised as follows.
 
 
 1. If you enter a spin a modern glider below 1,000 ft. AGL you will almost
 certainly die. No amount of prior training will make much difference.
 2.Your first defence is to maintain safe speed near the ground. Your early
 training should be such that you feel very uncomfortable if below this 
 criteria.
 3. To maintain this speed you must monitor the ASI. Ground features mean
 relying on the horizon attitude is not accurate, particularly with modern
 slippery gliders. The ASI should be checked regularly and the closer to the
 ground and more adverse the conditions the more frequently the check. On 
 final
 under turbulent conditions a quick check no more than every 5 seconds is 
 needed
 to ensure safe speed is maintained.
 4. Learning and practicing incipient recovery. If things go wrong incipient
 recovery means living to a ripe old age more certain, whether in a thermal 
 or
 close to the ground.
 5. Spin training helps in spins at altitude. Enter a spin below about 1,000 
 ft
 AGL in a modern glider and you will most likely be dead in about 5 seconds.
 
 Harry Medlicott
 Hi All,
 
 Sorry to be controversial but I believe most of our spin training is 
 marginal
 in saving lives in the real world. Of far greater significance are design
 factors reducing the propensity of gliders to spin. Spin related accidents 
 in
 Europe have substantially reduced over time. No changes in spin training but
 modern gliders are far more forgiving.
 
 My first club had winch launching only and every year a tug was brought in 
 and
 towed gliders to 3,000 ft for spin training. After briefing, students were
 quite comfortable going through the standard recovery procedures.
 
 My second club was winch launching only. Often there were periods when we 
 had
 students due for spin training but weather conditions were such that 
 thermals
 were not able to give us much by way of height. I experimented with a Blanik 
 by
 a spin of the top of a winch launch which after one turn allowed recovery by
 1,000 ft. before using the procedure with a student. OK in a Blanik but
 certainly not in some other types
 
 Despite very careful briefing a few minutes before the results were entirely
 different to those when entering a spin at 3,000 ft. Upon seeing the ground
 below them the student would immediately pull the control column right back 
 and
 sometimes also move the control column away from the descending wing. It was 
 an
 involuntary

Re: [Aus-soaring] spin training

2014-12-25 Thread Tim Shirley

Hi Harry,

Merry Christmas to you.

You have of course (and as usual), correctly identified the real 
problem.  It is safe speed near the ground.  Maintain that and there 
will be no chance of spinning.  Spinning is a secondary effect of flying 
too slow, yet somehow it is now the spin and not the speed that is 
considered all important in our training system.


If we want to safely train for safe speed near the ground, including 
spin recognition and recovery, we should be making much more use of 
simulators, at every level of experience.  If people on the list have 
never tried this, visit Benalla and see what happens when you spin a 
Ventus 2, a K21, an Astir or an Antares. You can try all in the space of 
30 minutes.  It is genuinely realistic.  Recover wrong (depending on the 
glider) and it flicks the other way.And if it turns into a spiral 
dive and exceeds VNE it flutters and the wings fall off.   You can do a 
flat over-ruddered turn at any altitude including on final.  No one 
dies, but the experience is genuine and the lesson graphic.   The same 
by the way is true for teaching rope breaks and launch failures, on both 
aerotow and winch.  And if anyone thinks that simulators are not putting 
enough pressure on, try it first. You won't make that claim after you 
have just killed yourself. The sim at Benalla was made out of an IS28 
fuselage because it has all the controls, it has a wraparound 180 deg 
screen, and can be used for all phases of flight including 
cross-country.  It cost less than $10,000 to make, uses off the shelf 
components and costs next to nothing to run.  It isn't portable though.


Oh and there is nothing at all wrong with old gliders.  They are often 
beautiful, historic and a pleasure to fly.  But basically irrelevant for 
training people who are going to fly modern gliders.


The way forward won't be found by looking in the rear view mirror :)


Cheers

/Tim Shirley/

/tra dire é fare c' é mezzo il mare/

On 26/12/2014 10:15 AM, Harry wrote:

Hi All,
I wrote the attached article and it received a few comments, both on 
and off the web.

I should have summarised as follows.
1. If you enter a spin a modern glider below 1,000 ft. AGL you will 
almost certainly die. No amount of prior training will make much 
difference.
2.Your first defence is to maintain safe speed near the ground. Your 
early training should be such that you feel very uncomfortable if 
below this criteria.
3. To maintain this speed you must monitor the ASI. Ground features 
mean relying on the horizon attitude is not accurate, particularly 
with modern slippery gliders. The ASI should be checked regularly and 
the closer to the ground and more adverse the conditions the more 
frequently the check. On final under turbulent conditions a quick 
check no more than every 5 seconds is needed to ensure safe speed is 
maintained.
4. Learning and practicing incipient recovery. If things go wrong 
incipient recovery means living to a ripe old age more certain, 
whether in a thermal or close to the ground.
5. Spin training helps in spins at altitude. Enter a spin below about 
1,000 ft AGL in a modern glider and you will most likely be dead in 
about 5 seconds.

Harry Medlicott
Hi All,
Sorry to be controversial but I believe most of our spin training is 
marginal in saving lives in the real world. Of far greater 
significance are design factors reducing the propensity of gliders to 
spin. Spin related accidents in Europe have substantially reduced over 
time. No changes in spin training but modern gliders are far more 
forgiving.
My first club had winch launching only and every year a tug was 
brought in and towed gliders to 3,000 ft for spin training. After 
briefing, students were quite comfortable going through the standard 
recovery procedures.
My second club was winch launching only. Often there were periods when 
we had students due for spin training but weather conditions were such 
that thermals were not able to give us much by way of height. I 
experimented with a Blanik by a spin of the top of a winch launch 
which after one turn allowed recovery by 1,000 ft. before using the 
procedure with a student. OK in a Blanik but certainly not in some 
other types
Despite very careful briefing a few minutes before the results were 
entirely different to those when entering a spin at 3,000 ft. Upon 
seeing the ground below them the student would immediately pull the 
control column right back and sometimes also move the control column 
away from the descending wing. It was an involuntary reaction but the 
one we would use to keep the glider in a spin.
So far as I am aware most spin accidents occur close to the ground, 
below about 1,000 ft unless one is flying a particularly nasty glider 
such as an IS28, which can take over 1,000 ft for the whole process. 
If what I am saying is correct, then what are the chances of a pilot 
using the correct recovery processes in a low level spin, perhaps a 
considerable time 

RE: [Aus-soaring] Spin Training

2004-09-23 Thread Ulrich Stauss
Having gone through my training in Germany (perhaps a little more recently
than Rolf?) I concur with Rolf. The general syllabus was very similar to
what we have here, including incipient and full spin training. There was A
LOT more theory though.

I can't remember whether there was a particular emphasis on spinning being
classified as an aerobatic manoeuvre though (nor whether any spins I may
have experienced solo were purely accidental ;-)).

The attitude of one of our instructors was that as (then) teenagers we would
try things anyway when out of visual range of an instructor so he might as
well show us how it's done safely and properly lest we kill ourselves going
it solo. It would make us better pilots anyway.
Not that he encouraged us in any way. On the contrary, he came down hard on
any known transgressions.

Ulrich Stauss

-Original Message-
From: [EMAIL PROTECTED]
[mailto:[EMAIL PROTECTED] On Behalf Of rolf a.
buelter
Sent: Thursday, 23 September 2004 20:31
To: [EMAIL PROTECTED]
Subject: [Aus-soaring] Spin Training

My knowledge is old but I believe still valid.

1. Spin training is done, fully developed spin is trained but emphasis is 
placed on recognition of incipient spin.
2. Spinning is an aerobatic manouvre. It is not permitted without the 
appropriate training and (aerobatic) endorsment in the license. Spinning a 
glider without an instructor sole is not permitted.

There are pilots in Australia with more recent experience who may be able to

correct me.

My personal opinion is that making a pilot comfortable with the spinning 
characteristics of a glider will enhance chances of reasoned response and 
recovery. Rgds - Rolf

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