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Suggestions to alleviate troubles with the stabilizer adjusting mechanism.
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Immediate changes necessary in the bungee installation.
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To provide tail position light visibility for compliance with CAR 03. 538.
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All planes with effective serial numbers 1623 and up have the redesigned trim system installed. All planes shipped by rail will be shipped as follows.
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Wing aileron bellcrank brackets failing due to parking or staking out the airplane with the tail into the wind without securing the controls.
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Reinforce the upper end of the tie strap on the landing gear with a 4130 steel plate.
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How to correct air leaks, which permit entrance of engine fumes into the cockpit, in the area of the fuselage right main landing gear fittings.
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A synthetic liner used as a hose connection in the Engine Oil Breather System has been found to separate from the hose structure, interfering with proper engine ventilation and leading to oil leaks.
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There is now available a kit number 752-186 to install the auxiliary fuel line in the Piper Pacer "115", "125" and "135".
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Subject: Typical and maximum number of exposed strut threads as permitted for rigging on Piper aircraft. Applicability: Piper J-3, J-4, J-5, and PA-11 through PA-22 Download PDF: Lift-Strut-Fork-Extension.pdf Piper Strut Thread (Typical ...