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#1
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I was trying to remember just what that AD was about. I remember reading it
a couple years ago, but do not know why. Wasn't there something in the AD about the switch malfunctioning and actually leaving one or both mags hot when the switch was turned to off in addition to the key comeing out? Seems like I also remember an inspection and lubrication requirement. Maybe I was just dreaming. Jim "Robert M. Gary" wrote in message ups.com... You may actually have an AD that requires you to replace the mag switch. I had to replace mine two years ago after a shop showed me an AD that says it must be replaced if the key can be removed in flight. I have no idea why the hell such an AD exists. -Robert |
#2
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There also was a part of that AD that required an operational test in
which the key is forcefully (no torque spec but plenty aggressively) turned CCW beyond OFF to see if the engine keeps running. Some aircraft including our 172M, would relight again. A new switch wasn't that expensive about 5 years ago (like $100). It came as part of a kit replacing all of the locks in the airframe. The tumbler setup and key etc was more robust that the Cessna OEM key. |
#3
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AH!! That's where I read it... when studying for my CFI ride in a 182RG.
Thanks! Jim "nrp" wrote in message ps.com... There also was a part of that AD that required an operational test in which the key is forcefully (no torque spec but plenty aggressively) turned CCW beyond OFF to see if the engine keeps running. Some aircraft including our 172M, would relight again. A new switch wasn't that expensive about 5 years ago (like $100). It came as part of a kit replacing all of the locks in the airframe. The tumbler setup and key etc was more robust that the Cessna OEM key. |
#4
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![]() Jim Burns wrote: I was trying to remember just what that AD was about. I remember reading it a couple years ago, but do not know why. Wasn't there something in the AD about the switch malfunctioning and actually leaving one or both mags hot when the switch was turned to off in addition to the key comeing out? Seems like I also remember an inspection and lubrication requirement. Maybe I was just dreaming. You remembered pretty accurately. The switch test involved turning off the engine via the mags and making sure they both grounded. If not, it's replacement time. If the key came out in any position other than "off", it's also replacement time. On Sunday I was doing a BFR in a rental. During the engine out glide, the instructor reached over and switched the mags off and pulled the key out. He thought it would rattle/distract me. I had a really good laugh when he couldn't get it back in. He was starting to look kind of worried passing through 1000 AGL. John Galban=====N4BQ (PA28-180) |
#5
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#6
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![]() Mark Hansen wrote: I thought that actually shutting off the engine during a simulated engine out situation was really frowned upon? It probably is frowned upon by some. IMHO, If you really want to shut the engine off during a glide, you should use the mixture. With only the ignition off, the fuel/air mixture is still cycling through the cylinders and soaking your plugs. John Galban=====N4BQ (PA28-180) |
#7
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On Sunday I was doing a BFR in a rental. During the engine out
glide, the instructor reached over and switched the mags off and pulled the key out. He thought it would rattle/distract me. I had a really good laugh when he couldn't get it back in. He was starting to look kind of worried passing through 1000 AGL. Anyone who did that to me would not be able to get out of the plane unassisted. -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#8
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![]() Jay Honeck wrote: Anyone who did that to me would not be able to get out of the plane unassisted. In some other situation I might have been ****ed. But on this flight, he was the PIC (my BFR was expired), plus I was 1,000 ft. AGL, right next to an automotive proving ground. There were several miles of usable runway right under me. Landing there safely would have been easier than at an airport. John Galban=====N4BQ (PA28-180) |
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