If the seat was built to plans (you really need a set of plans if the plane did not come with them), then it has a seat fitting with 3 positions to adjust the seat travel...is it at the aft position ? Like Dan said I would stay away from the push pull tube until all other areas have been reviewed and found to be correct. As far as the pitot static system, if you have a Mode C transponder that requires the 24 month inspection I would just have a test box hooked up and have the entire pitot static system checked. It will tell you within minutes if you have a leak. Otherwise you will spend hours trying to track down a possible problem. You can also blow up a party balloon and place it over the pitot tube (attach it with a quick tie). Note the speed on the AS indicator. There is an allowable bleed down rate (I think it is in AC-13 ?). As far as the static system, not sure how you would do the tail installed static. If the static port were on the side of the AC you can attach a suction cup over the port and place modeling clay around the edge of the cup to help seal and hold the cup in place. Then with a large syringe attached to the suction cup with a piece of surgical tubing you pull some vacuum, crimp off the hose and note the altimeter. Again there is a bleed down rate (I think it is in AC-13 ?) for the altimeter and VSI.
Again I would check the stab rigging by making a template from the plans and taping it to the side of the AC. I would start here before tearing the AC apart ! If the rig is off then I would go to the stops by the walking beam and check them. Also while in there where the stops are I would check to see if there is any interference from wires, sheet metal any type of fittings the builder may have installed. If all is good here, then I would look inside the tail to see if the stab. balance beam is hitting anything ?
RB
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