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Am in temp hiatus in my lessons due to financial shortages but I understood
from my instructor that it was just around the corner, lesson immediately after stalls. Let's see - lesson 13 in the FTM Aeroplane, 4th edition. http://www.tc.gc.ca/civilaviation/ge...13747/menu.htm however it's not in the flight test standards. Lesson 13 in the online version of the flight training syllabus talks about incipient spins and recoveries but the downloadable PDF file still calls for full spin training. Wonder what the real story is. "David Megginson" wrote in message ... "Steve House" writes: Unless you're training for the PPL here in Canada, where spins and recovery are part of the required syllabus at about lesson 11. Transport Canada removed spin training from the syllabus in the late 1990's (I don't know the exact year). It was not part of my PPL training in 2002. As far as I understand (*not* confirmed from an official source), there were two problems with spin training: 1. The stall/spin accident rate was slightly higher in Canada than the U.S., despite the fact that all Canadian PPL holders had spin training and most U.S. PPL holders did not. 2. There were occasional training fatalities during spin training, including one where the rudder in a 152 jumped its stop and jammed past full deflection. Given #1, there was no justification for the deaths in #2 (even if they were fairly rare). All the best, David |
#2
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![]() "Rich Stowell" wrote in message om... We need to be very careful here -- just because an airplane is approved for operation in the Utility Category does NOT mean it is certified for intentional spins! That is correct, but if it's not approved in the utility category it is almost certainly NOT approved for spins. Furhter, there may be further restrictions on the spinning than just the utility category loading. For example, the Cherokees prohibit anything from being in the baggage compartment while spinning. |
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#4
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"Ron Natalie" wrote in message om...
"Ron Natalie" wrote in message m... "John Galban" wrote in message om... I've flown and spun 150/160s that were approved for spins in the Utility Category. Let me be more exact. The PA-28-150 and PA-28-160 are NOT certficated in the utility category, hence no spins. The PA-28-151 and PA-28-161 are certificated in the utility category. snip BTW - I checked my logbook and you were absolutely correct. Turns out the planes I mentioned above were 150 and 160 hp versions of the -140. John Galban=====N4BQ (PA28-180) |
#5
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Ron Natalie wrote:
: I've flown and spun 150/160s that were approved for spins in the : Utility Category. : Let me be more exact. The PA-28-150 and PA-28-160 are NOT : certficated in the utility category, hence no spins. The PA-28-151 : and PA-28-161 are certificated in the utility category. Hrmm... sounds illegal to me then? : The PA-28-140, -180, -181 are certificated in the utility category : For those models that are certificated with for utility category operations. : 1. You have to get the CG in the utility envelope. Of course. : 2. You have to not have the 2150 gross weight increase.on the -140. Probably not too many of them left. : 3. There is a serial number limit on the -180 for utility category operations. Probably the old (non-clamshell cowling) version? : 4. You can only use the two front seats. Of course Mine need not legally apply since the engine upgrade expressly says Normal only. Thanks for the info though... I would think it's pretty much a legal issue. The important thing would be to keep it loaded in the Utility CG range. Other than that there's no real difference between the airframes. -Cory -- ************************************************** *********************** * The prime directive of Linux: * * - learn what you don't know, * * - teach what you do. * * (Just my 20 USm$) * ************************************************** *********************** |
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#8
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#9
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David Megginson wrote in message ...
Either Piper spin-tested the other models and found them unsatisfactory, or else the test pilots wouldn't even try spinning them in the first place (because of engineering predictions). Neither thought makes me too comfortable. Piper spin tested the "stretched" models. They had to as part of the certification testing. That's a whole different ballgame than approval for intentional spins. Oddly enough, the original stretched models were not restricted from intentional spins when they 1st came out. Spin approval was rescinded for those models a few years later by AD. John Galban=====N4BQ (PA28-180) |
#10
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G.R. Patterson III wrote:
I would think it's pretty much a legal issue. I don't think so. Two CFIs were killed near Solberg a few years ago when a spin went flat. I think they were flying a Cherokee. I've spun (with utility loading) a '68 PA28-180 that wasn't placarded against it. It didn't spin well. By that I mean it was _really_ uninterested in entering a spin; stick back full stall (well, mush) and full rudder made it want to spiral. A jab of throttle was needed to convince it to wallow over and spin. Recovery was normal and uneventful. Some PA28's (notably later ones) are placarded against spins, I suspect because some CG loadings may make recovery -er- difficult. |
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