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#1
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What is the max towing weight (max weight of the glider) for the PA-18 150 hp and 180hp?
Where can I find information on this (on the net). Thanks! Robert ASW 28-18E |
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On Sunday, April 22, 2012 3:06:13 PM UTC-4, Robert Danewid wrote:
What is the max towing weight (max weight of the glider) for the PA-18 150 hp and 180hp? Where can I find information on this (on the net). Thanks! Robert ASW 28-18E I have never seen any Piper limitations published. The tow hook installed is likely the limiting factor. FWIW UH |
#3
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On Apr 22, 1:06*pm, Robert Danewid wrote:
What is the max towing weight (max weight of the glider) for the PA-18 150 hp and 180hp? Where can I find information on this (on the net). Thanks! Robert ASW 28-18E As long as a Tost hook is installed, there are practically no limits. There are two 180 HP PA-18's operating out of Boulder, CO where density altitudes can reach 9,000'. They routinely tow fully loaded 2- seaters. The PA-18-150 has significantly less performance which is why none are used in Colorado. While information on hooks is available on-line, towing performance probably isn't. I recall the late Dave Johnson, who developed the STC for the 180HP Cub, saying a 180 HP Lyc. O-360 is only a few pounds heavier than the original O-320. He went on to say it seems like the extra 30HP provides a lot more performance than one would expect. The Schweizer tow plane hook has a limit of 1200 pounds which is inadequate for heavier gliders but the Tost hook limit is 2570 Lb which easily handles any glider. For that and a lot of other reasons, the Schweizer hook should be retired. |
#4
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Thanks
My problem is that some one has found a supplement named S1A-77 to the Flight Manual of a 180 hp PA 18 that says that max glider weigth is 600 kg. Can any one send me or direct me to that supplement. It does not make sense...... We have been towing gliders 600 kg with PA 18 150/180 since the early 80ies. Robert |
#5
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At first blush I'd say that information was not from the USA. I don't recall ever seeing any US aviation restriction stated in kilos, but I could be wrong. Just a thought.
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#6
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On Apr 22, 4:43*pm, Robert Danewid wrote:
Thanks My problem is that some one has found a supplement named S1A-77 to the Flight Manual of a 180 hp PA 18 that says that max glider weigth is 600 kg. Can any one send me or direct me to that supplement. It does not make sense...... We have been towing gliders 600 kg with PA 18 150/180 since the early 80ies. Robert OK, having nothing else to do this afternoon, I did some research. The 600kg number suggested a European sourced supplement. US STC's would likely be in SAE units. It appears there is a MOGAS STC issued in Switzerland to Wenger & Kaufmann for PA-18-180-M and PA-18-150 glider tugs. In pursuit of the STC the glider tow performance (takeoff roll, climb rate) was measured with a 600kg glider in tow. Since that is the heaviest glider tested, that became the limit for the STC. This may or may not the source of S1A-77 but it shows how it can happen. There are LOTS of different STC's for PA-18 around the world. This is a bit if a diversion but most recent European 2-seaters specify 600kg (Actually, 600 daN) weak links for aero tow. If these gliders are operated in strict compliance with their Approved Flight Manuals as required by FAR 91.9, 600kg would be the max load on the tug. I have been assuming (possibly in error) that you are in the US. |
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On 23 Apr, 03:08, Bill D wrote:
On Apr 22, 4:43*pm, Robert Danewid wrote: Thanks My problem is that some one has found a supplement named S1A-77 to the Flight Manual of a 180 hp PA 18 that says that max glider weigth is 600 kg. Can any one send me or direct me to that supplement. It does not make sense...... We have been towing gliders 600 kg with PA 18 150/180 since the early 80ies. Robert OK, having nothing else to do this afternoon, I did some research. The 600kg number suggested a European sourced supplement. *US STC's would likely be in SAE units. It appears there is a MOGAS STC issued in Switzerland to Wenger & Kaufmann for PA-18-180-M and PA-18-150 glider tugs. *In pursuit of the STC the glider tow performance (takeoff roll, climb rate) was measured with a 600kg glider in tow. *Since that is the heaviest glider tested, that became the limit for the STC. *This may or may not the source of S1A-77 but it shows how it can happen. *There are LOTS of different STC's for PA-18 around the world. This is a bit if a diversion but most recent European 2-seaters specify 600kg (Actually, 600 daN) weak links for aero tow. *If these gliders are operated in strict compliance with their Approved Flight Manuals as required by FAR 91.9, 600kg would be the max load on the tug. I have been assuming (possibly in error) that you are in the US. I am in Sweden Thanks for your info Robert |
#8
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Can't agree that most recent European 2 seaters specify 600kg weaklinks for aerotow. The Duo Discus for example is 50% or so higher and the DG 1000 is higher again at 1100 DaN Having said all that here in New Zealand there are some operations that use PA-18 180s and they variously tow Duos and ASH 25s so they are well capable of handling the bigger ships subject to density altitude considerations Colin Last edited by Ventus_a : April 23rd 12 at 10:31 PM. |
#9
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On Apr 23, 3:20*pm, Ventus_a
wrote: Bill D;813718 Wrote: On Apr 22, 4:43*pm, Robert Danewid wrote:- Thanks My problem is that some one has found a supplement named S1A-77 to the Flight Manual of a 180 hp PA 18 that says that max glider weigth is 600 kg. Can any one send me or direct me to that supplement. It does not make sense...... We have been towing gliders 600 kg with PA 18 150/180 since the early 80ies. Robert- OK, having nothing else to do this afternoon, I did some research. The 600kg number suggested a European sourced supplement. *US STC's would likely be in SAE units. It appears there is a MOGAS STC issued in Switzerland to Wenger & Kaufmann for PA-18-180-M and PA-18-150 glider tugs. *In pursuit of the STC the glider tow performance (takeoff roll, climb rate) was measured with a 600kg glider in tow. *Since that is the heaviest glider tested, that became the limit for the STC. *This may or may not the source of S1A-77 but it shows how it can happen. *There are LOTS of different STC's for PA-18 around the world. This is a bit if a diversion but most recent European 2-seaters specify 600kg (Actually, 600 daN) weak links for aero tow. *If these gliders are operated in strict compliance with their Approved Flight Manuals as required by FAR 91.9, 600kg would be the max load on the tug. I have been assuming (possibly in error) that you are in the US. Can't agree that most recent European 2 seaters specify 600kg weaklinks for aerotow. *The Duo Discus for example is 50% or so higher and the DG 1000 is higher again at 1100 DaN Having said all that here in New Zealand there are some operations that use PA-18 180s and they variously tow Duos and ASH 25s so they are well capable of handling the bigger ships subject to density altitude considerations Colin +-------------------------------------------------------------------+ |Filename: Weak links.jpg * * * * * * * * * * * * * * * * * * * * * | |Download:http://www.aviationbanter.com/attachment.php?attachmentid=55283| |Filename: Weak links 2.jpg * * * * * * * * * * * * * * * * * * * * | |Download:http://www.aviationbanter.com/attachment.php?attachmentid=55284| +-------------------------------------------------------------------+ -- Ventus_a From the DG-1000 manual page 2.10: "6000 N + 600 N (1323 lbs. + 132 lbs.) for tow behind slow tow planes" Which I think would include a PA-18. The Duo allows a 700 daN weak link but that's not 50% higher. |
#10
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I did a lot of the fly off time for Dave Johnson when he was
developing his original STC for the first 180hp Cubs. The climb performance over a stock 150hp Cub was amazing. With the 150hp Cubs, we could not tow the 2-32's out of the Black Forest Gliderport (elevation 7200') when the temperature got much over 70ºF. With the 180hp, there really was no limitation on glider weights or density altitude for our ops requirements. We even towed a few gliders out of Leadville (10,000') several times, and flew fully loaded 2-32's out of Aspen, Gunnison, Durango, and several other high altitude airports without problems during Dave's annual glider caravans around the state of Colorado. That was something we couldn't do with the 150 Cub. One particularly rememberable tow was into the wave near Pikes Peak, when the wave wasn't really working. For whatever reason, the 2-32 pilot wouldn't release, and the tow was continued until I waved him off at 18,000' (Old days, Positive Control Airspace began at FL240 then). Steve PS |
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