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#21
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Piper 235 tail skin
Jay Honeck wrote:
New thinking at Piper, as reflected in newer manuals, says to replace and not patch the skins. I would think they have discovered important reasons to make that change. Yeah, they discovered that they could charge $1600 for a $12 piece of pressed aluminum. AND likely avoid liability by ensuring a repaired crack does not show up at a crash site. |
#22
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Piper 235 tail skin
"Mike Spera" wrote AND likely avoid liability by ensuring a repaired crack does not show up at a crash site. Sounds good, if it means I am not arriving at the crash site a few milliseconds before the cracked spar. Really, guys and gals; do you want to go flying around with a spar that is stop drilled? Not me. -- Jim in NC |
#23
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Piper 235 tail skin
Morgans wrote:
"Mike Spera" wrote AND likely avoid liability by ensuring a repaired crack does not show up at a crash site. Sounds good, if it means I am not arriving at the crash site a few milliseconds before the cracked spar. Really, guys and gals; do you want to go flying around with a spar that is stop drilled? Not me. Well, we're talking about cracked *skins* here, not spars. See the thread title. I believe Piper's ability to charge $1600 for a $12 part, coupled with potential liability, is exactly what drove this policy change. Happy Flying! Scott Skylane |
#24
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Piper 235 tail skin
On Wed, 05 Mar 2008 20:39:40 -0900, Scott Skylane
wrote: Morgans wrote: "Mike Spera" wrote AND likely avoid liability by ensuring a repaired crack does not show up at a crash site. Sounds good, if it means I am not arriving at the crash site a few milliseconds before the cracked spar. Really, guys and gals; do you want to go flying around with a spar that is stop drilled? Not me. Well, we're talking about cracked *skins* here, not spars. See the thread title. I believe Piper's ability to charge $1600 for a $12 part, coupled with potential liability, is exactly what drove this policy change. If you can find a DER who disagrees with Piper's engineering that calls for replacement instead of repair could you repair it and do a 337 under the DERs signoff? |
#25
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Piper 235 tail skin
: That's strange. When my IA showed me his current manual (on CD), it had
: the prohibition. As I recall, it was worded the same as described in Dave's : post above. : John Galban=====N4BQ (PA28-180) : -- : Message posted via AviationKB.com : http://www.aviationkb.com/Uwe/Forums...ation/200803/1 Might want to check that P/N on the manual. Yours is a hershey-bar -180, right? I was starting to think that only the taper-wings had the prohibition in there. -Cory -- ************************************************** *********************** * Cory Papenfuss, Ph.D., PPSEL-IA * * Electrical Engineering * * Virginia Polytechnic Institute and State University * ************************************************** *********************** |
#26
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Piper 235 tail skin
: Well, we're talking about cracked *skins* here, not spars. See the
: thread title. I believe Piper's ability to charge $1600 for a $12 part, : coupled with potential liability, is exactly what drove this policy change. : If you can find a DER who disagrees with Piper's engineering that : calls for replacement instead of repair could you repair it and do a : 337 under the DERs signoff? Piper *themselves* disagree with Piper. I challenge you to find NTSB reports of *properly* executed skin patches being a factor in a crash. So long as the dynamic balance of the control surface is within range, the repair is done according to AC43 (or in Piper's case, THEIR OWN SERVICE MANUAL!), it's perfectly safe. I agree that the only reasons for the changes are - Limiting liability wherever possible. - Charging insane prices for replacement skins. Think about it... why in the hell would they encourage a $100 repair on a plane they sold 40 years ago if they could play the legally-cautious and $1600 financially-beneficial route of mandating skin replacements? -Cory -- ************************************************** *********************** * Cory Papenfuss, Ph.D., PPSEL-IA * * Electrical Engineering * * Virginia Polytechnic Institute and State University * ************************************************** *********************** |
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