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The Air Accidents Investigation Branch of the Department for Trade have now
published their report on the accident at Husbands Bosworth on 18th January 2004, both pilots were killed. The report may be found at http://www.aaib.gov.uk/sites/aaib/cms_resources/HCD.pdf , it runs to 21 pages. W.J. (Bill) Dean (U.K.). Remove "ic" to reply. |
#2
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I would urge all instructors to read the report carefully,
paying particular attention to the recomendations made by the AAIB with regard to spin entry and abandonment heights. At 19:30 13 January 2005, W.J. \bill\ Dean \u.K.\. wrote: The Air Accidents Investigation Branch of the Department for Trade have now published their report on the accident at Husbands Bosworth on 18th January 2004, both pilots were killed. The report may be found at http://www.aaib.gov.uk/sites/aaib/cms_resources/HCD.pdf , it runs to 21 pages. W.J. (Bill) Dean (U.K.). Remove 'ic' to reply. |
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A very thorough report...don't see how the Puchasz
can be the culprit here....things that would concern me a 1.) Spin entries are permitted at 1500', with an easy spinning ship this does not give one a lot of leeway. 2.) Having an instructor with a bad ticker teaching these manuevers. 3.) Combining (1) and (2) with a relatively green trainee...who might not recognize when things head south. So although no blatant disregarding of rules happened, it might be time to rethink a few issues. At 19:30 13 January 2005, W.J. \bill\ Dean \u.K.\. wrote: The Air Accidents Investigation Branch of the Department for Trade have now published their report on the accident at Husbands Bosworth on 18th January 2004, both pilots were killed. The report may be found at http://www.aaib.gov.uk/sites/aaib/cms_resources/HCD.pdf , it runs to 21 pages. W.J. (Bill) Dean (U.K.). Remove 'ic' to reply. |
#4
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Is this likely to result in JAR madical requirements for BGA instructors?
"W.J. (Bill) Dean (U.K.)." wrote in message ... The Air Accidents Investigation Branch of the Department for Trade have now published their report on the accident at Husbands Bosworth on 18th January 2004, both pilots were killed. The report may be found at http://www.aaib.gov.uk/sites/aaib/cms_resources/HCD.pdf , it runs to 21 pages. W.J. (Bill) Dean (U.K.). Remove "ic" to reply. |
#5
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At 23:00 13 January 2005, T O D D P A T T I S T wrote:
Stewart Kissel wrote: A very thorough report...don't see how the Puchasz can be the culprit here.... I read it and came away thinking the Puch was still a possible culprit. How? As stated in the report the Puch spins readily but recovers very easily. Quoted from the report: 'It can reasonably be concluded that the only control mishandling of the PUCHACZ that can lead to delay in spin exit is the retention of full pro spin elevator…. ' It is actually difficult for us to teach proper spin recover in the Puch simply because it recovers so easily. You have to watch what rudder pedals are doing, common problems a 1. Not removing pro spin rudder but moving the stick forward (glider usually recovers). 2. Centralising the rudder and moving the stick forward (glider pretty much always recovers). 3. Not removing opposite rudder promptly after spin stops (danger of flicking the other way or overloading the rudder). The danger is that a pilot gets the impression 'all I have to do to recover is relax the back pressure' that'll kill you in a glider with genuinely nasty spin recovery characteristics like the DG500. 1.) Spin entries are permitted at 1500', with an easy spinning ship this does not give one a lot of leeway. 1500' should be enough, but the report indicated that the Puch was more difficult to recover than other trainers and implied that this might have contributed to the accident. Eh? Where did it say that? It's easier to recover than other trainers! 2.) Having an instructor with a bad ticker teaching these manuevers. Regardless of the advisability of instructing with this medical condition: 1) The instructor was still alive after the accident, not dead/incapacitated. 2) The instructor's legs were injured, and they seemed to be leg injuries consistent with conscious reaction to the imminent approach of the ground. 3.) Combining (1) and (2) with a relatively green trainee...who might not recognize when things head south. The trainee's right leg was injured in a way the report considered to be consistent with applying full opposite rudder to the left spin. They had made at least two successful full spin recoveries prior to their final spin (perhaps more, the witnesses didn't see the full flight). Two or three full spins and recoveries down from 3000 to 1500' sounds about right, usually you have to have at least a few seconds of debrief after each recovery along the lines of 'you forgot this or that, try again'. Personally I'm happy enough demonstrating a spin entry and recovery at 1500' but I won't let the P2 initiate the spin below 2000' except maybe if every entry and recovery up to then has been 'textbook'. Having said which, quite often at my club we can climb to 3200', push out over flat ground, practice spinning down to 1800' then climb back up to 3200' on the ridge again for another go. Sure it's possible that they did two correctly, and then screwed up. It's also possible, the instructor had a partial attack, slumped to block the stick, then recovered, etc. But the bottom line is we still don't know why. I'm sorry, 'slumped to block the stick', the last time I flew HCD (a long time ago admittedly) I'm pretty sure it had a five point harness, how the heck do you 'slump to block the stick' wearing a five point harness? I do, however, have to agree, we will never know exactly what happened in this awful tragedy and any further speculation over it is probably counter productive. |
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![]() Andrew Warbrick wrote: At 23:00 13 January 2005, T O D D P A T T I S T wrote: Stewart Kissel wrote: A very thorough report...don't see how the Puchasz can be the culprit here.... I read it and came away thinking the Puch was still a possible culprit. How? As stated in the report the Puch spins readily but recovers very easily. Quoted from the report: 'It can reasonably be concluded that the only control mishandling of the PUCHACZ that can lead to delay in spin exit is the retention of full pro spin elevator.... ' It is actually difficult for us to teach proper spin recover in the Puch simply because it recovers so easily. You have to watch what rudder pedals are doing, common problems a 1. Not removing pro spin rudder but moving the stick forward (glider usually recovers). 2. Centralising the rudder and moving the stick forward (glider pretty much always recovers). 3. Not removing opposite rudder promptly after spin stops (danger of flicking the other way or overloading the rudder). The danger is that a pilot gets the impression 'all I have to do to recover is relax the back pressure' that'll kill you in a glider with genuinely nasty spin recovery characteristics like the DG500. 1.) Spin entries are permitted at 1500', with an easy spinning ship this does not give one a lot of leeway. 1500' should be enough, but the report indicated that the Puch was more difficult to recover than other trainers and implied that this might have contributed to the accident. Eh? Where did it say that? It's easier to recover than other trainers! 2.) Having an instructor with a bad ticker teaching these manuevers. Regardless of the advisability of instructing with this medical condition: 1) The instructor was still alive after the accident, not dead/incapacitated. 2) The instructor's legs were injured, and they seemed to be leg injuries consistent with conscious reaction to the imminent approach of the ground. 3.) Combining (1) and (2) with a relatively green trainee...who might not recognize when things head south. The trainee's right leg was injured in a way the report considered to be consistent with applying full opposite rudder to the left spin. They had made at least two successful full spin recoveries prior to their final spin (perhaps more, the witnesses didn't see the full flight). Two or three full spins and recoveries down from 3000 to 1500' sounds about right, usually you have to have at least a few seconds of debrief after each recovery along the lines of 'you forgot this or that, try again'. Personally I'm happy enough demonstrating a spin entry and recovery at 1500' but I won't let the P2 initiate the spin below 2000' except maybe if every entry and recovery up to then has been 'textbook'. Having said which, quite often at my club we can climb to 3200', push out over flat ground, practice spinning down to 1800' then climb back up to 3200' on the ridge again for another go. Sure it's possible that they did two correctly, and then screwed up. It's also possible, the instructor had a partial attack, slumped to block the stick, then recovered, etc. But the bottom line is we still don't know why. I'm sorry, 'slumped to block the stick', the last time I flew HCD (a long time ago admittedly) I'm pretty sure it had a five point harness, how the heck do you 'slump to block the stick' wearing a five point harness? I do, however, have to agree, we will never know exactly what happened in this awful tragedy and any further speculation over it is probably counter productive. Three statistics would be interesting to compare, although I doubt if there is data for all of them. 1. Number of accidents and/or fatalities resulting from spin training. 2. Number of accidents and/or fatalities from accidents in which pilots had previously undergone the above-mentioned spin training. 3. Number of spin recoveries resulting in accident avoidance from pilots who had previously undergone the above-mentioned spin training. I'm hoping that the lives saved through the spin recovery training far exceeds the lives lost. |
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On 14 Jan 2005 09:44:06 GMT, Andrew Warbrick
wrote: How? As stated in the report the Puch spins readily but recovers very easily. It is actually difficult for us to teach proper spin recover in the Puch simply because it recovers so easily. Considering the sheer number of spin accidents with instructors on board of Puchacz I dare to doubt that statement. The danger is that a pilot gets the impression 'all I have to do to recover is relax the back pressure' that'll kill you in a glider with genuinely nasty spin recovery characteristics like the DG500. DG500 nasty spin recovery characteristics? Which ones? I'm doing a lot of spin training in the DG-505 with 17.2m wingtips and the spin behaviour is really nice. Bye Andreas |
#8
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At 15:00 14 January 2005, Andreas Maurer wrote:
On 14 Jan 2005 09:44:06 GMT, Andrew Warbrick wrote: How? As stated in the report the Puch spins readily but recovers very easily. It is actually difficult for us to teach proper spin recovery in the Puch simply because it recovers so easily. Considering the sheer number of spin accidents with instructors on board of Puchacz I dare to doubt that statement. Have you ever spun one? I will repeat myself, it recovers from most spins with most cockpit loads if you let go the stick, so on the majority of occasions the instructor has to be vigilant that the pupil applies the correct recovery or an incorrect recovery technique will have been learnt. The danger is that a pilot gets the impression 'all I have to do to recover is relax the back pressure' that'll kill you in a glider with genuinely nasty spin recovery characteristics like the DG500. DG500 nasty spin recovery characteristics? Which ones? I'm doing a lot of spin training in the DG-505 with 17.2m wingtips and the spin behaviour is really nice. Bye Andreas The DG-500 is fully compliant with JAR22 when the CofG is within limits. When the CofG is near the aft limit it requires the correct spin recovery to be applied, in the correct order, or the ground will do the recovery for you, it will continue to autorotate with the stick on the front stop if you just heave the stick forward without first centralising the ailerons and applying full opposite rudder. It may be possible to recover by applying the full opposite rudder after heaving the stick forward but it will be a delayed recover due to control surface masking. A pilot who has acquired the impression from the Puch that all is required is to let go or relax the back pressure could be killed in this situation. |
#9
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On 14 Jan 2005 16:13:14 GMT, Andrew Warbrick
wrote: Have you ever spun one? I will repeat myself, it recovers from most spins with most cockpit loads if you let go the stick, so on the majority of occasions the instructor has to be vigilant that the pupil applies the correct recovery or an incorrect recovery technique will have been learnt. Until now I have not even seen a Puchacz in real life - but the sheer number of spin accidents with experienced pilots suggests that something is wrong, don't you agree? I wonder about "letting go the stick" and letting the glider recover itself - is this really being taught as a procedure? We teach our student pilots to center the stick, and apply opposite rudder - in that order. Letting go the stick is an unknown procedure for me, I have to admit. The DG-500 is fully compliant with JAR22 when the CofG is within limits. When the CofG is near the aft limit it requires the correct spin recovery to be applied, in the correct order, or the ground will do the recovery for you, it will continue to autorotate with the stick on the front stop if you just heave the stick forward without first centralising the ailerons and applying full opposite rudder. It may be possible to recover by applying the full opposite rudder after heaving the stick forward but it will be a delayed recover due to control surface masking. Hmm... looks like the missing 80 cm of wingspan on the 505 really seem to make a difference here - our 505 recovers nicely even at fully aft CG positions. A pilot who has acquired the impression from the Puch that all is required is to let go or relax the back pressure could be killed in this situation. I don't think this is the problem. A typical Puchacz spin accident has the instructor onboard, and I'm pretty sure that most of these instructors knew about the correct spin recovery procedure. Here in Germany we also had our share of Puchacz spin accident. One was a successful spin recovery that went into an opposite spin - the IP was not able to recover the second spin before impact. Bye Andreas |
#10
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![]() Uzytkownik "Andreas Maurer" napisal w wiadomosci ... On 14 Jan 2005 16:13:14 GMT, Andrew Warbrick wrote: Have you ever spun one? Until now I have not even seen a Puchacz in real life - but the sheer number of spin accidents with experienced pilots suggests that something is wrong, don't you agree? Why doesn't it surprise me? Most of the pilots who write the worst opinions on Puchacz never have flown it, or even seen it. I don't think this is the problem. A typical Puchacz spin accident has the instructor onboard, and I'm pretty sure that most of these instructors knew about the correct spin recovery procedure. I think that they're often crashed in spins just because they're most often used ships for spin training. Just because they spin in a textbook way and need a textbook recovery to get out of a spin, not only 'releasing the stick' just like the Bocian or Junior. Here in Germany we also had our share of Puchacz spin accident. One was a successful spin recovery that went into an opposite spin - the IP was not able to recover the second spin before impact. Maybe they were too surprised by the fact that the glider entered another spin due to inproper recovery action that they had lost a little bit too much time. Regards, -- Janusz Kesik Poland to reply put my name.surname[at]gazeta.pl ------------------------------------- See Wroclaw (Breslau) in photography, The XIX Century, the Festung Breslau, and photos taken today. http://www.wroclaw.dolny.slask.pl |
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