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Hi folks,
I ran into a little problem today. Working on a 100hour just a month before the annual is due -- my mechanic and I lifted the back seat to look at the cabling underneath. Lo and behold -- we found a "tear" in an aluminum bulkhead under the back seat. The bulkhead is under the back of the rear seat and doesn't appear to be structural as it is thin aluminum. But there is a steel brace coming in from the flap area of the wing and rivited to the lower outside corner of the aluminum bulkhead. However on mine, just next to the steel brace on the baggage door side -- there is a inch long tear up from the bottom of the bulkhead and a small buckle in the aluminum brace above the tear. Its like there was a terrific upwards stress on the bottom corner of the bulkhead where the steel is rivited and it tore the aluminum bulkhead upwards. Has anyone run into this problem before? I'd love to hear what had to be done to repair/replace the damage. Maybe someone knows of a 337 that had been done to repair similar damage??? It would sure help my mechanic who is a little unsure of where to start in the repair process. Thanks guys... Chuck N7398W |
#2
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If you are a member of the Cherokee Pilots Association, asking this question
on their "Cherokee Chat" web page would net you quite a few good responses. See www.Piperowner.com . Sounds like you've got some pretty major damage there. Is any of it noted in the logbooks? (I'll bet I know the answer to *that* question...) -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#3
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C wrote:
Working on a 100hour just a month before the annual is due -- my mechanic and I lifted the back seat to look at the cabling underneath. Lo and behold -- we found a "tear" in an aluminum bulkhead under the back seat. The bulkhead is under the back of the rear seat and doesn't appear to be structural as it is thin aluminum. But there is a steel brace coming in from the flap area of the wing and rivited to the lower outside corner of the aluminum bulkhead. I'd be carefull jumping to the conclusion that's it isn't structural. That steel plate is the rear wing attach fitting. And I believe the bulkhead that it's attached to is considered the "rear spar carry through" (like a "mini" spar). Cherokee's have a large center spar, but also have a front and rear attach point and carry through. The front carry through is behind where your heels sit when you're in the pilot's seat (under the plastic trim pieces). The rear one is where you describe. However on mine, just next to the steel brace on the baggage door side -- there is a inch long tear up from the bottom of the bulkhead and a small buckle in the aluminum brace above the tear. Its like there was a terrific upwards stress on the bottom corner of the bulkhead where the steel is rivited and it tore the aluminum bulkhead upwards. There was a person on the Cherokee Chat (see Jay Honeck's post) a few weeks ago that had very similar crack and he posted pictures. I hope this isn't the beginning of a trend, or we'll be seeing an AD soon. You're correct in assuming a "terrific upward stress", although I would have hoped that a hard landing or bad turbulence wouldn't have caused such damage. You'll want to make sure you have a very competant mechanic fix this. Wing departure, or severe twist, while in flight would really suck. You might want to show this to your local FSDO, too. I hate to encourage and AD, but this could be a problem we might not want to ignore. --- Jay -- __!__ Jay and Teresa Masino ___(_)___ http://www2.ari.net/jmasino ! ! ! http://www.oceancityairport.com http://www.oc-adolfos.com |
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#6
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Quite often hard landing damage such as this is prohibitively expensive to
repair. I suspect you'll find yet more damage inside the wings around the landing gear attach points. People have tried unsuccessfully to make bush airplanes out of Cherokees. Usually the airframe just gets bulldozed off the side of some Alaska runway after a few months. Karl |
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xyzzy wrote:
attachments don't work on the newsgroups. You'll need to put it on a website if you want us to be able to see it Attachments work, some ISPs don't allow or filter them, I received it just fine... You can view it he http://www.whodat.net/cherokee180/damage.jpg Shame mine doesn't filter excessive quotation... ![]() |
#9
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kage wrote:
: Quite often hard landing damage such as this is prohibitively expensive to : repair. I suspect you'll find yet more damage inside the wings around the : landing gear attach points. People have tried unsuccessfully to make bush : airplanes out of Cherokees. Usually the airframe just gets bulldozed off the : side of some Alaska runway after a few months. : Karl Not everyone wants or needs a bush plane. -- Aaron C. |
#10
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C wrote:
: Hi folks, : I ran into a little problem today. problem snipped This is probably due to someone torqueing the wing forward or aft at some point. The wing flexes around the main spar and pulls or pushes on the rear attatch fitting. This causes a crack in the spar carry through right where yours is. The wing is 12' long, so even a small torque applied at the tip gets "amplified" by the long lever arm. The front attatch fitting is there really to hold on the leading edge "glove" and doesn't take much force. The main spar and rear attatch take all of the loads. Hard landings cause cracks in the wing lower skins at the most inboard point just in front of the main spar, which is covered by the long metal fairing when assembled. Ripples on the lower aft wing skins also show up. If this was done during a hard landing it was really a doozie. My Cherokee 180 had similar damage on the left wing rear attatch fitting. It was apparently damaged in 1969 when the left wing hit a runway light. It was repaired without logs or 337's and went unnoticed until I bought it in 2000. The mechanic that did the pre-buy found it. He said that it was repaired just fine and not to worry unduly. Since the plane had 31 years and 5600 hours since the repair I think it is just fine, too. I don't believe that there was a crack in the spar carry through on my plane, though. The repair on my airplane involved cutting out the baggage compartment floor about 6" aft of the rear spar carry through. The rear spar carry through was replaced, picking up the rivets in the steel plate. A scab patch was put on the outside of the fuselage. The baggage comp. floor was replaced with a doubler on the inside along the cut line. It all was beautifully done. If I can ever get over to the airport again, which may not be for 2-3 more weeks, I can take some pictures if you wish. -- Aaron Coolidge |
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