Checkout_my_Six
Touchdown! Greaser!
then you'd have 10 and a half......
You think that maybe I can’t unzip and count 11?
Piper has turned SBs and related into a revenue stream. Gotta pay for them.Thank you. Ironic that piper.com doesn't have the SB available.
The taper wings have an inspection plate access to the area specified in the SB. The plate is a little outboard of the one shown in the SB.
SB 1006 is probably how it was found. Removal of fuel tank, and inspect spar. There's a guy on another forum who performed the inspection, and hadda replace a wing due to the corrosion found.I'll ask the obvious question. If those two (or two hundred, as some say) were found without cutting into the wing, how were they found and why can't the AD simply require the inspection, whether by cutting into the wing for inspection covers or by borescope or other non-intrusive methods?
Jim
If you adopt this proposed procedure I **URGE** you not to specify that we use the "Acme Model 1234AA-X" inspectoscope
You could offer to pay for the SB work, and purchase the airplane, if the wing turns out to be OK. Otherwise, the owner is on the hook.Thx Tom, will make sure the ads are complied with.
The issue is, without this being an ad, the seller would never want to comply with the sb because he maybe stuck with a grounded and unsellable plane if corrosion was detected.
From a buyer's point of view, if it's not done, I would have to buy the plane first, then comply with SB and hope for the best
Don't worry, I sent a letter to the FAA a couple days ago.So -181's dropped through the cracks? Maybe we should just stay quiet and let sleeping dogs lie.
So -181's dropped through the cracks? Maybe we should just stay quiet and let sleeping dogs lie.
IIRC, all the taper-wing models have inspection holes in the necessary places, and the spar is accessible through the main wheel well on the retractables. So only the fixed-gear, Hershey-bar-wing models are affected.So -181's dropped through the cracks?
That docket is still open until Nov 2019 and is the same time frame as Docket No. FAA-2018-1046 which addresses the spar cap cracks. If I was a betting man...NPRM FAA-2017-1059
Usually due to a bad alloy, not related to external forces.wing spar failures. very serious inter granular corrosion of the wing attach fitting, this is a cast milling
Does that mean they are still accepting comments? I’ve got a new one I’d like to add.That docket is still open until Nov 2019 and is the same time frame as Docket No. FAA-2018-1046 which addresses the spar cap cracks. If I was a betting man...
As best as I can tell the comment period closed on Dec 22, 2017 11:59 PM ET. But here is link to the docket and it gives the contact info for the agency/person overseeing this docket.Does that mean they are still accepting comments?