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#1
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On Monday, May 5, 2014 4:13:02 PM UTC-4, son_of_flubber wrote:
On Monday, May 5, 2014 3:30:29 PM UTC-4, wrote: Because it was not adequately drilled into his head during training and subsequent retraining that you can't make that turn back safely. Will the NTSB look in his log book for a self-induced PTOT(aka simulated PTOT for training purposes)? What is it you are describing? UH |
#2
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I have flown into and out of Sampley's a few times. The terrain at Sampley's rises to the east and falls to the west. Heading west, you are over slightly falling terrain with open fields for landing. On an easterly departure, you may be at an indicated 200 feet above take-off but may only be 100' over terrain. Straight-ahead landing options are not very enticing to the east once you've passed the end of the strip, so a turn back from an indicated 200' may seem like the best option.
Since we have no direct eyewitness reports, we don't know how high he was at disconnect, but Sampley's towplane is a powerful and fast climber. The Zuni was equipped with a logger, so maybe that will throw some more light onto it. A bit of a shadow on us all. Mike |
#3
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MAYBE, there was something wrong with the Zuni and he released because he couldn't control it?????? For instance........aileron linkage failure. I would be interested in others thoughts on this. John |
#4
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On 5/24/2014 8:21 AM, John L Fleming wrote:
son_of_flubber;883103 Wrote: On Sunday, May 4, 2014 12:27:10 AM UTC-4, Waveguru wrote:- Premature termination of the tow at 100ft. Did not complete the turn back to the runway. - My sympathy to everyone touched by this tragedy. Turning 180 back to the runway from only 100 feet AGL is unusual. I wonder why he did that. I've been watching this thread from day one. I'm back here in New York and was a friend of Bob and am puzzled by the turn as he always had his ducks all in a row. I'm too am a glider pilot and I find it hard to believe he made a steep bank at 100 feet. Bob had accumulated 1000's of hours in both fighters and the two single engine aircraft he owned. MAYBE, there was something wrong with the Zuni and he released because he couldn't control it?????? For instance........aileron linkage failure. I would be interested in others thoughts on this. John My condolences for the loss of your friend. I hadn't been in aviation but two or three years before personal aviation acquaintances and friends began dying in aviation-related accidents. All I could do was mourn their passing, try and extract lessons for myself (if any), rationalize that they died doing something they loved, and take some decision(s) for my own future. Many glider pilots often roll their eyes at "the obviousness" of NTSB probable cause conclusions (e.g. pilot failed to maintain sufficient speed), but one thing I think NTSB investigators are quite adept at is establishing control connection continuity, particularly in the aftermath of low-speed accidents as this (where wreckage is minimally disturbed from effects of the crash itself), so probably the best answer to your puzzlement can be expected to come from the final NTSB report on this crash. Bob W. |
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At 16:00 25 May 2014, Bob Whelan wrote:
On 5/24/2014 8:21 AM, John L Fleming wrote: son_of_flubber;883103 Wrote: On Sunday, May 4, 2014 12:27:10 AM UTC-4, Waveguru wrote:- Premature termination of the tow at 100ft. Did not complete the turn back to the runway. - My sympathy to everyone touched by this tragedy. Turning 180 back to the runway from only 100 feet AGL is unusual. I wonder why he did that. I've been watching this thread from day one. I'm back here in New York and was a friend of Bob and am puzzled by the turn as he always had his ducks all in a row. I'm too am a glider pilot and I find it hard to believe he made a steep bank at 100 feet. Bob had accumulated 1000's of hours in both fighters and the two single engine aircraft he owned. MAYBE, there was something wrong with the Zuni and he released because he couldn't control it?????? For instance........aileron linkage failure. I would be interested in others thoughts on this. John My condolences for the loss of your friend. I hadn't been in aviation but two or three years before personal aviation acquaintances and friends began dying in aviation-related accidents. All I could do was mourn their passing, try and extract lessons for myself (if any), rationalize that they died doing something they loved, and take some decision(s) for my own future. Many glider pilots often roll their eyes at "the obviousness" of NTSB probable cause conclusions (e.g. pilot failed to maintain sufficient speed), but one thing I think NTSB investigators are quite adept at is establishing control connection continuity, particularly in the aftermath of low-speed accidents as this (where wreckage is minimally disturbed from effects of the crash itself), so probably the best answer to your puzzlement can be expected to come from the final NTSB report on this crash. Bob W. Some years ago I witnessed a fatal spin-in following a launch failure. It was a winch launch, the cable broke at about 150 feet agl. There was plenty of room to land ahead on the airfield but the glider started a turn to the left, flying obviously rather slowly. It completed about two thirds of a 360 degree turn and then spun, went down into some trees a few yards from the airfield boundary on ground about 20 feet lower than the airfield. I was one of those that extracted the badly injured pilot from the wreckage (he died in the ambulance before it left the airfield). In the UK it is almost universal practice to set QFE not QNH on glider altimeters (most gliding sites are less than 1,000 feet amsl), I noticed that the altimeter in the wrecked glider was reading about plus 260 feet. Later investigation showed that the millibar sub-scale setting was consistent with the pressure on the previous day on which the glider had flown. It seemed highly likely to me that the pilot had omitted to reset the altimeter before take-off and, when the launch failed, saw over 400 feet on the altimeter and reacted to that. |
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On Monday, May 26, 2014 6:44:41 PM UTC+12, Chris Rollings wrote:
Some years ago I witnessed a fatal spin-in following a launch failure. It was a winch launch, the cable broke at about 150 feet agl. There was plenty of room to land ahead on the airfield but the glider started a turn Well, that's clearly stupid. The place I normally fly is short (but long enough we have 150 ft or so over the fence on a normal day, less if dead calm, more if a decent headwind) and the options are houses houses and houses, or turn back. If you've got "cross the boundary fence and take the next paddock" that's a different matter. And if you've got a km of runway still in front of you then turning back from 150 ft is utterly stupid. I don't think anyone here is arguing for that. In the UK it is almost universal practice to set QFE not QNH on glider altimeters (most gliding sites are less than 1,000 feet amsl), I noticed Um. Who the heck looks at the *altimeter* at a time like that? Look out the window! A couple of years ago the field I usually fly from got a flight information service. They can't tell us what to do, in every regard except one. When we arrived back and joined the circuit they'd (along with wind etc) tell us the QNH and EXPECT US TO REPEAT IT BACK. And presumably expect us to set the altimeter to it. It's been a long process, but we seem to have finally convinced them that by the time we've made the decision to land and made the downwind call we are no longer interested in the altimeter, what it says, or what the QNH is. That was useful 20 or 30 km out, but from this point on we're ignoring the altimeter and looking out the window. |
#7
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On Monday, May 26, 2014 12:44:41 AM UTC-6, Chris Rollings wrote:
At 16:00 25 May 2014, Bob Whelan wrote: On 5/24/2014 8:21 AM, John L Fleming wrote: son_of_flubber;883103 Wrote: On Sunday, May 4, 2014 12:27:10 AM UTC-4, Waveguru wrote:- Premature termination of the tow at 100ft. Did not complete the turn back to the runway. - My sympathy to everyone touched by this tragedy. Turning 180 back to the runway from only 100 feet AGL is unusual. I wonder why he did that. I've been watching this thread from day one. I'm back here in New York and was a friend of Bob and am puzzled by the turn as he always had his ducks all in a row. I'm too am a glider pilot and I find it hard to believe he made a steep bank at 100 feet. Bob had accumulated 1000's of hours in both fighters and the two single engine aircraft he owned. MAYBE, there was something wrong with the Zuni and he released because he couldn't control it?????? For instance........aileron linkage failure. I would be interested in others thoughts on this. John My condolences for the loss of your friend. I hadn't been in aviation but two or three years before personal aviation acquaintances and friends began dying in aviation-related accidents. All I could do was mourn their passing, try and extract lessons for myself (if any), rationalize that they died doing something they loved, and take some decision(s) for my own future. Many glider pilots often roll their eyes at "the obviousness" of NTSB probable cause conclusions (e.g. pilot failed to maintain sufficient speed), but one thing I think NTSB investigators are quite adept at is establishing control connection continuity, particularly in the aftermath of low-speed accidents as this (where wreckage is minimally disturbed from effects of the crash itself), so probably the best answer to your puzzlement can be expected to come from the final NTSB report on this crash. Bob W. Some years ago I witnessed a fatal spin-in following a launch failure. It was a winch launch, the cable broke at about 150 feet agl. There was plenty of room to land ahead on the airfield but the glider started a turn to the left, flying obviously rather slowly. It completed about two thirds of a 360 degree turn and then spun, went down into some trees a few yards from the airfield boundary on ground about 20 feet lower than the airfield. I was one of those that extracted the badly injured pilot from the wreckage (he died in the ambulance before it left the airfield). In the UK it is almost universal practice to set QFE not QNH on glider altimeters (most gliding sites are less than 1,000 feet amsl), I noticed that the altimeter in the wrecked glider was reading about plus 260 feet. Later investigation showed that the millibar sub-scale setting was consistent with the pressure on the previous day on which the glider had flown. It seemed highly likely to me that the pilot had omitted to reset the altimeter before take-off and, when the launch failed, saw over 400 feet on the altimeter and reacted to that. It sounds like this pilot lacked even basic airmanship skills. Quibbling over altimeter settings and low turns is beside the point. The real question is why he was allowed to fly at all. |
#8
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On Saturday, May 3, 2014 9:27:10 PM UTC-7, Waveguru wrote:
Premature termination of the tow at 100ft. Did not complete the turn back to the runway. It is so disheartening to me..... that the industry hasn't picked up my technique of teaching about requiring students to be speaking aloud during the departure climb -- "I can land here (xxxxxx) , I can land there (xxxxxx ) , I can turn for a downwind landing (meaning sufficient altitude and within-limits tailwind component), I can make an abbreviated pattern into wind, I can make a full pattern." Meaning - they can land straight ahead somewhere on the remaining airport. they can land somewhere ahead or aside/outside the premises in the 'best available' place, they know they have enough to land downwind ( if appropriate - sometimes you would never choose DW), they can make a teensy, tight short pattern onto the upwind end of the airfield. they can make a pretty leisurely, semi-normal landing into wind on the airfield. The simplistic rote teaching of requiring students to say aloud -- 200 feet -- That doesn't get them 'ahead of the glider' and actively looking, thinking, assessing where they can go during each moment of the departure climb. IF pilots were taught to think that way, I believe, we would eliminate these PTTT turn/stall accidents almost entirely. Folks might land in less than wonderful places, but it would be a landing, not an example of gravity in control. Arriving in a comparatively level and comparatively slow descent rate is hugely more survivable than what we see in these types of accidents. If any CFIGs would like to discuss their airfield, their trainings ships and tugs, and their departure options, I would be happy to assist them in understanding and incorporating this training protocol. With great regret for the loss of another pilot, Cindy Brickner Caracole Soaring (760) 373-1019 cell phone |
#9
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Why is anyone aero towing with a tow hook that will back release? To me it is a basic safety issue. It is not just this latest tragic accident, I have seen more wild gyrations and damages brought on by aero towing with a C.G.. hook than with a nose hook that does not back release. There are, I think, very few glider models that cannot be retro fitted with a forward hook that does not back release. To those who admire the so called "Zuni hook", well I have one on my desk right now, it is a poor piece of engineering.
In Germany regulations have been enacted setting currency standards that one must meet before using a C.G. hook for aero tow. It would be interesting to analyze damage claims on aero launches, sorted by nose, E-85 or similar, tow hooks against back releasing C.G. hooks. But then maybe I should not make a big issue of it as I am in the glider repair business. Robert Mudd Moriarty, NM |
#10
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On 5/6/2014 10:41 PM, Robert M wrote:
Why is anyone aero towing with a tow hook that will back release? Excellent question. In the U.S., looking back in time (e.g. the Schweizer fleet), historical inertia? In any event, I've never owned a glider that did NOT have a back-releasable, non-CG hook on it, and except for my club's G-103s, never piloted one either. Bob W. |
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